Centre National d'Etudes Spatiales

France

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Type PI
        Brevet 359
        Marque 41
Juridiction
        International 234
        États-Unis 121
        Canada 24
        Europe 21
Date
Nouveautés (dernières 4 semaines) 1
2025 avril 1
2025 mars 2
2025 (AACJ) 3
2024 16
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Classe IPC
G01S 19/22 - Problèmes liés aux multitrajets 16
H04B 7/185 - Stations spatiales ou aériennes 13
B64G 1/40 - Aménagements ou adaptations des systèmes de propulsion 11
B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage 11
B64G 1/10 - Satellites artificielsSystèmes de tels satellitesVéhicules interplanétaires 10
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Classe NICE
42 - Services scientifiques, technologiques et industriels, recherche et conception 36
41 - Éducation, divertissements, activités sportives et culturelles 33
09 - Appareils et instruments scientifiques et électriques 32
35 - Publicité; Affaires commerciales 29
38 - Services de télécommunications 22
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Statut
En Instance 22
Enregistré / En vigueur 378
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1.

AEROSTAT FOR CARRYING OUT TRANSPORT AND/OR OBSERVATION MISSIONS ON A PLANET WITH AN ATMOSPHERE

      
Numéro d'application FR2024051374
Numéro de publication 2025/083371
Statut Délivré - en vigueur
Date de dépôt 2024-10-18
Date de publication 2025-04-24
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Nicot, Jean-Marc

Abrégé

The present invention relates to an aerostat (1) for carrying out transport and/or observation missions on a planet with an atmosphere, the aerostat comprising: an inflatable body (2) designed to be pressurised by a gas lighter than the atmosphere, a payload (3) configured to have at least one scientific instrument installed on-board, and a solar energy generator (7) arranged between the inflatable body (2) and the payload (3).

Classes IPC  ?

  • B64B 1/40 - Ballons
  • B64D 27/353 - Aménagements pour la production, la distribution, la récupération ou le stockage d'énergie électrique à bord utilisant des cellules solaires

2.

FIBRE-OPTIC INTERFEROMETER BASED ON A MONOFREQUENCY LASER SOURCE AND INTERFEROMETRY METHOD CORRECTED FOR PARASITIC REFLECTIONS

      
Numéro d'application 18576958
Statut En instance
Date de dépôt 2022-07-07
Date de la première publication 2025-03-27
Propriétaire
  • EXAIL (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Ducloux, Eric

Abrégé

This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency f p = 1 2 ⁢ τ . This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency f p = 1 2 ⁢ τ . According to the invention, the laser source is a monofrequency laser source and the light generator includes modulation means designed to modulate the source beam at a modulation frequency equal to This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency f p = 1 2 ⁢ τ . According to the invention, the laser source is a monofrequency laser source and the light generator includes modulation means designed to modulate the source beam at a modulation frequency equal to 2 ⁢ f p 2 ⁢ n + 1 This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency f p = 1 2 ⁢ τ . According to the invention, the laser source is a monofrequency laser source and the light generator includes modulation means designed to modulate the source beam at a modulation frequency equal to 2 ⁢ f p 2 ⁢ n + 1 where n is an integer greater than or equal to 1, and the photodetector and the electronic signal-processing system are configured to acquire and process a signal representative of the interference beam at a demodulation frequency equal to This relates to an interferometer including a light generator, a fibre-optic coil, an optical coupler/splitter, a photodetector and an electronic signal-processing system. The light generator includes a laser source able to emit a source beam split into two secondary beams passing through the coil with a travel time τ defining a natural frequency f p = 1 2 ⁢ τ . According to the invention, the laser source is a monofrequency laser source and the light generator includes modulation means designed to modulate the source beam at a modulation frequency equal to 2 ⁢ f p 2 ⁢ n + 1 where n is an integer greater than or equal to 1, and the photodetector and the electronic signal-processing system are configured to acquire and process a signal representative of the interference beam at a demodulation frequency equal to f p 2 ⁢ n + 1 .

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique

3.

METHOD AND SYSTEM FOR GUIDING A USER HOLDING IN ONE HAND AN ULTRASOUND OBSERVATION PROBE TOWARDS A PRE-RECORDED ACOUSTIC WINDOW

      
Numéro d'application 18722399
Statut En instance
Date de dépôt 2022-12-14
Date de la première publication 2025-03-13
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • MEDES-INST MEDECINE PHYSIOLOGIE SPATIALE (France)
Inventeur(s)
  • Arbeille, Philippe
  • Chaput, Didier
  • Derache, François
  • Faucoz, Orphée
  • Thevenon, Aristée

Abrégé

A method for guiding a user holding in one hand a probe for ultrasound observation a patient, including: placing a support on the body surface; acquiring at least one image; determining the reference frame; determining coordinates of at least one vertex of a polygon placed in a first plane transverse to the recorded direction of the probe; displaying the at least one image; projecting on the at least one displayed image; determining the current position and the current direction of the probe in the reference frame; projecting, on the at least one displayed image, the at least one vertex; bringing the probe to a new current position and a new current direction, the new current position and the new current direction coinciding with the recorded position and the recorded direction.

Classes IPC  ?

  • A61B 8/00 - Diagnostic utilisant des ondes ultrasonores, sonores ou infrasonores

4.

CNES CENTRE NATIONAL D'ÉTUDES SPATIALES

      
Numéro d'application 1827622
Statut Enregistrée
Date de dépôt 2024-06-12
Date d'enregistrement 2024-06-12
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 11 - Appareils de contrôle de l'environnement
  • 14 - Métaux précieux et leurs alliages; bijouterie; horlogerie
  • 16 - Papier, carton et produits en ces matières
  • 18 - Cuir et imitations du cuir
  • 20 - Meubles et produits décoratifs
  • 21 - Ustensiles, récipients, matériaux pour le ménage; verre; porcelaine; faience
  • 25 - Vêtements; chaussures; chapellerie
  • 28 - Jeux, jouets, articles de sport

Produits et services

Mouse pads, decorative magnets, batteries, charging stations [chargers], laptop bags. Electric lamps. Watches, cuff links, brooches, key rings. Posters, books, notebooks, pens, name badge holders [office requisites]. Umbrellas, backpacks, tote bags. Plastic exhibition or display models. Tableware, mugs, glasses [receptacles], drinking bottles for sports. Clothing, namely, polo shirts, tee-shirts, jackets, caps, socks, neckties, shirts. Games, toys, models [toys].

5.

IMPROVED AEROSTATIC ASSEMBLY

      
Numéro d'application FR2024050674
Numéro de publication 2024/246457
Statut Délivré - en vigueur
Date de dépôt 2024-05-24
Date de publication 2024-12-05
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Vargas, André
  • Duvel, Jean-Philippe

Abrégé

The invention relates to an aerostatic assembly (1) comprising: - two nacelles (2, 3), namely an aerial nacelle (2) and a marine nacelle (3), wherein the aerial nacelle (2) comprises a balloon (5) in a deflated state, a gas cartridge (6) for filling it, a first connection means (7) connecting the balloon (5) to the aerial nacelle (2), an atmospheric measurement device (8) and a transmission device (12) and the marine nacelle (3) comprises at least one device (9) for powering the atmospheric measurement device and the transmission device; - a second connection means (10) connecting the two nacelles (2, 3), the aerostatic assembly (1) being configured to trigger the filling of the balloon (5) via the gas cartridge (6) and the unlocking of locking/unlocking means (4) when a water landing is detected by water-landing detection means (8) in order to separate the nacelles (2, 3) so that they are connected together only by the second connection means (10).

Classes IPC  ?

  • B64B 1/40 - Ballons
  • B64B 1/62 - Commande de la pression du gaz, du chauffage, refroidissement ou libération du gaz
  • G01W 1/08 - Adaptations de ballons, de fusées ou d'aéronefs à des fins météorologiquesRadiosondes
  • B64B 1/50 - Ballons captifs
  • B63B 22/00 - Coffres d'amarrage ou bouées

6.

CNES

      
Numéro de série 98820454
Statut En instance
Date de dépôt 2024-10-25
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Wholesale or retail store services featuring downloadable electronic publications, printed products, instructional or teaching material except apparatus, posters, books, writing instruments, bags, small bags Space shuttles; vehicles for air and space travel, namely,solid-propellant rocket, space vehicles, namely, rockets,launch vehicles for satellite carrying space shuttles and in general for space transportation systems, all these goods being in connection with space activity Arranging seminars and practical training courses in the field of space travel; arranging symposiums, colloquiums and conferences for cultural or educational purposes; publication of electronic books and journals on-line; publication of texts other than advertising texts, all these services being in connection with aeronautics and space travel Technical project studies particularly in the fields of air and space travel; computer programming; engineering services, professional consultancy in the field of aeronautics and space; research and development of electronic and computer systems in the fields of computing and telecommunications for use in air and space travel; professional consultancy and project development unrelated to business dealings, namely, technical design of space ships rockets, satellites and any spatial devices; materials testing in technical laboratories; tests on the adaptability to the air and space travel environment of products from the radar industry, the optical industry, the spacecraft industry, the navigation satellite industry; research in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology and geology, and tests onthe adaptability to the space travel environment of products stemming from this research; development of global satellite navigation systems; scientific research into basic technologies; research in the field of robotic exploration of other planets. research in connection with preparatory programs with a view to future launches of rockets, satellites and space shuttles; research for the development of space technology; scientific research for earth observation, for exploration and human transportation, for human space travel or for space engineering; research into space technology; scientific services, namely, testing of new products for others, research missions and scientific coordination; development and publication of web pages for displaying scientific information in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology, geology and satellite technology research; research for fine-tuning technology and developing products; materials testing in an orbital environment; research on the adaptability of various components to the space environment, all these services being in connection with the field of space travel

7.

METHOD FOR MEASURING AND/OR COMPENSATING FOR AN ABERRATION IN AN IMAGE ACQUIRED BY AN OPTICAL INSTRUMENT COMPRISING A MULTISPECTRAL DETECTOR ARRAY

      
Numéro d'application FR2024050389
Numéro de publication 2024/200963
Statut Délivré - en vigueur
Date de dépôt 2024-03-27
Date de publication 2024-10-03
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Cucchetti, Edoardo
  • Latry, Christophe
  • Lucas, Sylvain

Abrégé

The invention relates to a method (100) for measuring an aberration in an image acquired by a detector array and a plurality of spectral filter arrays, the method comprising the following steps: acquiring (101) a known point source; determining (102) an initial value (VIP) of the parameters of a model of an impulse response; sampling (103); calculating (104) a cost according to a distance between the calculated impulse response and the observed impulse response; calculating (105) an overall cost (CG) for all of the spectral bands; estimating (102bis) a value (VEP) of each parameter; sampling (103bis); calculating (104bis) the cost; calculating (105bis) the overall cost (NCG); comparing (106) the overall cost (NCG) with the overall cost (CG); repeating (107).

Classes IPC  ?

  • H04N 25/61 - Traitement du bruit, p. ex. détection, correction, réduction ou élimination du bruit le bruit provenant uniquement de l'objectif, p. ex. l'éblouissement, l'ombrage, le vignettage ou le "cos4"
  • G01M 11/02 - Test des propriétés optiques

8.

GEODES

      
Numéro d'application 019070932
Statut En instance
Date de dépôt 2024-08-23
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 38 - Services de télécommunications
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Data software platforms relating to the field of space; Digital recording media; Electronicdata storage; Magnetic data carriers, recording discs; Computers, telecommunication apparatus enabling connection to databases or an internet network; Computer software featuring online downloadable computer programs on the internet and the world wide web; Electronic databases relating to the field of space; Data input and output terminals; Computer software for managing data and files and database software; Data processing apparatus relating to the field of space; apparatus for the transmission and communication of data; Databases relating to the field of space. Rental of access time to data processing servers and to computerised or telematic database servers, in connection with the aeronautics and space fields, including the Internet; Rental of access time to telecommunications servers, including the Internet, to servers for texts, electronic documents, databases, graphics and audiovisual information, in connection with the field of space; Rental of access time to servers for computer programs in connection with the field of space; Rental of access time to computer and communications networks in connection with the field of space; Rental of access time to a computerised or telematic database server, in connection with the field of space; Transmission of electronic mail; Providing chatrooms in virtual environments, Including real-time multimedia and collective communication on computer networks. Software as a service [SaaS]; Data platforms relating to the field of space as software as a service (SaaS); Computer rental; Design of graphics, drawings and text for formatting Web pages on the Internet; providing online information From computer or data transmission databases or the internet, in relation to the following fields: Space engineering; Computer software design, Upgrading of computer software, rental of computer software, Maintenance of computer software, Technical consultancy services relating to information technology, Computer rental, Computer programming, Advice and consultancy relating to computers, Providing of temporary use of computer programs for use with and on the internet and the world wide web.

9.

HYPERSPECTRAL IMAGING OPTICAL SYSTEM

      
Numéro d'application EP2024050148
Numéro de publication 2024/149666
Statut Délivré - en vigueur
Date de dépôt 2024-01-04
Date de publication 2024-07-18
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Butel, Guillaume
  • Israbian, Claude
  • Tetaz, Nicolas
  • Francesconi, Benjamin
  • Imbert, Christian
  • Coste, Vincent

Abrégé

PFim,tim,t nRii PFim,tim,t λii SFii iPFo,Olo,Ol nlii nFOVii nSFii nPii i ) of the detector distinct from the others.

Classes IPC  ?

  • G01J 3/02 - SpectrométrieSpectrophotométrieMonochromateursMesure de la couleur Parties constitutives
  • G01J 3/28 - Étude du spectre

10.

CNES CENTRE NATIONAL D'ÉTUDES SPATIALES

      
Numéro de série 79411988
Statut En instance
Date de dépôt 2024-06-12
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 25 - Vêtements; chaussures; chapellerie
  • 28 - Jeux, jouets, articles de sport
  • 09 - Appareils et instruments scientifiques et électriques
  • 11 - Appareils de contrôle de l'environnement
  • 14 - Métaux précieux et leurs alliages; bijouterie; horlogerie
  • 16 - Papier, carton et produits en ces matières
  • 18 - Cuir et imitations du cuir
  • 20 - Meubles et produits décoratifs
  • 21 - Ustensiles, récipients, matériaux pour le ménage; verre; porcelaine; faience

Produits et services

Clothing, namely, polo shirts, tee-shirts, jackets, caps, socks, neckties, shirts Games, toys, models [toys] Mouse pads, decorative magnets, batteries, charging stations [chargers], laptop bags Electric lamps Watches, cuff links, brooches, key rings Posters, books, notebooks, pens, name badge holders [office requisites] Umbrellas, backpacks, tote bags Plastic exhibition or display models Tableware, mugs, glasses [receptacles], drinking bottles for sports

11.

FIBER OPTIC DOSIMETER FOR SPACE ENVIRONMENT AND DOSIMETRY PROCESS

      
Numéro d'application 18512596
Statut En instance
Date de dépôt 2023-11-17
Date de la première publication 2024-05-23
Propriétaire
  • EXAIL (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • UNIVERSITÉ JEAN MONNET SAINT ETIENNE (France)
Inventeur(s)
  • Cheiney, Pierrick
  • Robin, Thierry
  • Melin, Gilles
  • Balcon, Nicolas
  • Mekki, Julien
  • Girard, Sylvain

Abrégé

This relates to a dosimeter including a light source capable of generating a light beam, an optical coupler-splitter, a radio-sensitive optical fiber, a first photodetector arranged to record a power measurement of the light beam transmitted through the radio-sensitive optical fiber, a reference optical arm, a second photodetector arranged to record a reference power measurement of the light beam transmitted through the reference optical arm, and an electronic system configured to extract a differential radiation induced attenuation measurement in the radio-sensitive optical fiber with respect to the reference optical arm. The light beam is non-polarized or depolarized, or, respectively, the light beam is polarized and the radio-sensitive optical fiber is a polarization-maintaining fiber.

Classes IPC  ?

12.

METHOD FOR REDUCING THE KERR EFFECT IN AN INTERFEROMETRY MEASURING DEVICE, AND INTERFEROMETRY MEASURING DEVICE CONFIGURED TO IMPLEMENT THIS METHOD

      
Numéro d'application 18548849
Statut En instance
Date de dépôt 2022-03-03
Date de la première publication 2024-05-23
Propriétaire
  • EXAIL (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Ducloux, Eric
  • Lhomme, Louis
  • Grossard, Nicolas
  • Hauden, Jérôme

Abrégé

Disclosed is a method for reducing the Kerr effect in an interferometry measuring device including a generator configured to emit an input periodic light signal, and a Sagnac interferometer in which two counterpropagating signals travel and combine so as to form a periodic output signal having at least two power values, the method including: determining a phase shift between the two counterpropagating signals a first time, and cancelling out the phase shift; and then determining a phase shift between the two counterpropagating signals a second time; and adjusting the ratio between the average powers of the counterpropagating signals so as to cancel out the value of the phase shift determined in the second determination. Also disclosed is an interferometry measuring device configured to implement such method.

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique

13.

GENERATOR FOR GENERATING AN ANTI-KERR-EFFECT MODULATED LIGHT SIGNAL, INTERFEROMETRY MEASURING DEVICE COMPRISING SUCH A GENERATOR, AND METHOD FOR MODULATING A LIGHT SIGNAL

      
Numéro d'application 18548842
Statut En instance
Date de dépôt 2022-03-03
Date de la première publication 2024-05-16
Propriétaire
  • EXAIL (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Ducloux, Eric
  • Ollivier, Christophe

Abrégé

Disclosed is a generator for generating an anti-Kerr modulated light signal, including a primary light source having four longitudinal modes or fewer and configured to generate a light signal and a modulator configured to modulate the power of the light signal by way of a square-wave or rectangular-wave control signal the duty cycle of which is less than or equal to 50%, and which are adapted such that the modulated light signal is periodic and has: —at a first point of the signal, a first power value equal to the product of its average power and a gain between 1.6 and 2.4; —at a second point of the signal, a second, non-zero power value, that is different from the first power value. Also disclosed is a modulation method and to a measuring device.

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique
  • G02F 1/01 - Dispositifs ou dispositions pour la commande de l'intensité, de la couleur, de la phase, de la polarisation ou de la direction de la lumière arrivant d'une source lumineuse indépendante, p. ex. commutation, ouverture de porte ou modulationOptique non linéaire pour la commande de l'intensité, de la phase, de la polarisation ou de la couleur
  • G02F 1/21 - Dispositifs ou dispositions pour la commande de l'intensité, de la couleur, de la phase, de la polarisation ou de la direction de la lumière arrivant d'une source lumineuse indépendante, p. ex. commutation, ouverture de porte ou modulationOptique non linéaire pour la commande de l'intensité, de la phase, de la polarisation ou de la couleur par interférence

14.

DEVICE FOR MEASURING AIR MOISTURE CONTENT

      
Numéro d'application FR2023051760
Numéro de publication 2024/100364
Statut Délivré - en vigueur
Date de dépôt 2023-11-09
Date de publication 2024-05-16
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • UNIVERSITE D'ORLEANS (France)
Inventeur(s) Chartier, Michel

Abrégé

The present invention relates to a device (1) for measuring air moisture content, the device comprising: a first piezoelectric sensor (2) comprising a quartz disk (4), a second piezoelectric sensor (6) comprising a quartz disk (8), a resonance frequency measuring device (18) configured to measure a change in resonance frequency of the quartz disk (4) of the first piezoelectric sensor (2) and a temperature sensor (20) configured to measure the temperature of the quartz disk (8) of the second piezoelectric sensor (6), the temperature sensor (20) being attached to a central portion (80) of the second quartz disk (8).

Classes IPC  ?

  • G01N 29/02 - Analyse de fluides
  • G01N 29/036 - Analyse de fluides en mesurant la fréquence ou la résonance des ondes acoustiques
  • G01N 29/22 - Recherche ou analyse des matériaux par l'emploi d'ondes ultrasonores, sonores ou infrasonoresVisualisation de l'intérieur d'objets par transmission d'ondes ultrasonores ou sonores à travers l'objet Détails
  • G01N 29/24 - Sondes
  • G01N 29/32 - Dispositions pour supprimer des influences indésirables, p. ex. des variations de température ou de pression

15.

FLEXIBLE DEVICE FOR TRANSFERRING HEAT BY CIRCULATING A TWO-PHASE FLUID

      
Numéro d'application FR2023051621
Numéro de publication 2024/084165
Statut Délivré - en vigueur
Date de dépôt 2023-10-17
Date de publication 2024-04-25
Propriétaire
  • AIRBUS DEFENCE AND SPACE SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Coquard, Typhaine
  • Fourgeaud, Laura
  • Simon, Coraline

Abrégé

The invention relates to a two-phase heat transfer device (1) capable of operating in a space environment, the device comprising: - a cavity (10) containing a two-phase fluid in the liquid-vapour equilibrium state; - a flexible portion (30) and two interface parts (40), one of the interface parts, the flexible portion and the other interface part being successively connected to one another, the device being characterised in that the flexible portion comprises a sealed flexible sheath (31) inside which at least one flexible internal liquid circulation duct (32) extends, which duct is surrounded by a space (33) for circulating the vapour.

Classes IPC  ?

  • F28D 15/02 - Appareils échangeurs de chaleur dans lesquels l'agent intermédiaire de transfert de chaleur en tubes fermés passe dans ou à travers les parois des canalisations dans lesquels l'agent se condense et s'évapore, p. ex. tubes caloporteurs

16.

QUASI-OPTICAL BEAMFORMER COMPRISING TWO REFLECTORS

      
Numéro d'application 18379605
Statut En instance
Date de dépôt 2023-10-12
Date de la première publication 2024-04-18
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D’ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • UNIVERSITE DE RENNES (France)
  • NANTES UNIVERSITE (France)
  • CENTRALESUPELEC (France)
  • INSA DE RENNES (France)
Inventeur(s)
  • Fraysse, Jean-Philippe
  • Lassauce, Léonin
  • Tubau, Ségolène
  • Ettorre, Mauro
  • Legay, Hervé

Abrégé

A quasi-optical beamformer includes a plurality N> 1 of power feeds (PF), each of the i∈[1; N] power feeds (PF) being configured to emit a respective radio-frequency beam denoted Ri, a radio-frequency transmission line (LT) fed at a first end by the power feeds and comprising at a second end a plurality of network ports (PR) that are configured to collect radio-frequency radiation, the transmission line (LT) comprising a radio-frequency waveguide (GO) that comprises at least two metal plates (PM) that are stacked so as to guide the radio-frequency beams Ri, i∈[1; N] towards the network ports (PR), the transmission line (LT) extending along a central main axis denoted axis x, a first reflector (M1) having a first centre (C1) centred on the axis x and a first effective radius of curvature and being configured to reflect the guided radio-frequency beams Ri, i∈[1; N], a second reflector (M2) having a second effective radius of curvature and being configured to reflect the radio-frequency beams (RFi) reflected by the first reflector so as to direct them towards the network ports so as to form output radio-frequency beams (RSi), the first and second effective radii of curvature and an arrangement of the power feeds (PF) with respect to the first reflector being configured so that: each of the output radio-frequency beams (RSi) is a plane wave, and a transverse amplitude distribution Ai, on the network ports (PR), of each output radio-frequency beam (RSi), is substantially identical.

Classes IPC  ?

  • H01Q 19/06 - Combinaisons d'éléments actifs primaires d'antennes avec des dispositifs secondaires, p. ex. avec des dispositifs quasi optiques, pour donner à une antenne une caractéristique directionnelle désirée utilisant des dispositifs de réfraction ou de diffraction, p. ex. lentilles
  • H01Q 9/04 - Antennes résonnantes
  • H01Q 23/00 - Antennes comportant des circuits ou des éléments de circuit actifs qui leur sont intégrés ou liés
  • H04B 7/06 - Systèmes de diversitéSystèmes à plusieurs antennes, c.-à-d. émission ou réception utilisant plusieurs antennes utilisant plusieurs antennes indépendantes espacées à la station d'émission

17.

QUASI-OPTICAL BEAMFORMER COMPRISING TWO REFLECTORS

      
Numéro de document 03216531
Statut En instance
Date de dépôt 2023-10-13
Date de disponibilité au public 2024-04-13
Propriétaire
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRALESUPELEC (France)
  • NANTES UNIVERSITE (France)
  • INSA DE RENNES (France)
  • THALES (France)
  • UNIVERSITE DE RENNES (France)
Inventeur(s)
  • Fraysse, Jean-Philippe
  • Lassauce, Leonin
  • Tubau, Segolene
  • Ettorre, Mauro
  • Legay, Herve

Abrégé

Quasi-optical beamformer (1) comprising.-a plurality N > 1 of powei feeds (PF), each of the i c [1;N] power feeds (PF) being configured to emit a respective radio-frequency beam denoted Ri,- a radio-frequency transmission line (LT) fed at a first end by the power feeds and comprising at a second end a plurality of network ports (PR) that are configured to collect radio-frequency radiation, the transmission line (LT) comprising a radio-frequency waveguide (GO) that comprises at least two metal plates (PM) that are stacked so as to guide the radio-frequency beams Ri, i c [1; IV] towards the network ports (PR), the lransmission line (LT) extending along a cenlral main axis denoted axis x,- a first reflector (M1) having a first centre (C1) centred on the axis x and a first effective radius of curvature and being configured to reflect the guided radio-frequency beams Roi c [1; N],- a second reflector (M2) having a second effective radius of curvature and being configured to reflect the radio-frequency beams (RF) reflected by the first reflector so as to direct them towards the network ports so as to form output radio-frequency beams (RSi), the first and second effective radii of curvature and an arrangement of the power feeds (PF) with respect to the first reflector being configured so that- each of the output radio-frequency beams (RS,) is a plane wave, and- a transverse amplitude distribution Ai, on the network ports (PR), of each output radio-frequency beam (RS), is substantially identical

Classes IPC  ?

  • H01Q 15/14 - Surfaces réfléchissantesStructures équivalentes
  • H01Q 19/17 - Combinaisons d'éléments actifs primaires d'antennes avec des dispositifs secondaires, p. ex. avec des dispositifs quasi optiques, pour donner à une antenne une caractéristique directionnelle désirée utilisant des surfaces réfléchissantes où les surfaces sont concaves la source rayonnante primaire comprenant plusieurs éléments rayonnants
  • H05K 1/02 - Circuits imprimés Détails

18.

ANGULAR POSITIONING MODULE FOR AN OPTICAL BENCH

      
Numéro d'application FR2023051075
Numéro de publication 2024/052603
Statut Délivré - en vigueur
Date de dépôt 2023-07-11
Date de publication 2024-03-14
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • UNIVERSITE PAUL SABATIER TOULOUSE III (France)
  • ANTOINE CAILLEAU (ASTROMECCA) (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Cailleau, Antoine
  • Klotz, Alain

Abrégé

The invention relates to an angular positioning module (1) for a positioning system for an optical bench, the angular positioning module (1) comprising: a fixed frame (5); a rotating shaft (7); a rotary motor (11); a transmission device (17) being provided with a pulley (19) mounted on the output rod (13) of the rotary motor (11) so as to be coupled in rotation therewith, with a wheel (21) mounted on the rotating shaft (7) so as to be coupled in rotation therewith, and with a cable wound on the one hand around the pulley (19) and on the other hand around the wheel (21) such that the pulley (19) and the wheel (21) are connected by two separate strands of the cable, the rotation of the pulley (19) causing the winding of a first strand and the simultaneous unwinding of a separate second strand around the pulley (19), and vice versa.

Classes IPC  ?

  • G02B 7/00 - Montures, moyens de réglage ou raccords étanches à la lumière pour éléments optiques
  • F16H 19/06 - Transmissions comportant essentiellement et uniquement des engrenages ou des organes de friction et qui ne peuvent transmettre un mouvement rotatif indéfini pour convertir un mouvement rotatif en mouvement alternatif et vice versa comportant un organe flexible sans fin

19.

COMPUTER-IMPLEMENTED METHOD FOR AUTOMATICALLY DETERMINING A TARGET ARCHITECTURE

      
Numéro d'application 18501224
Statut En instance
Date de dépôt 2023-11-03
Date de la première publication 2024-02-22
Propriétaire Centre National d'Études Spatiales (France)
Inventeur(s)
  • Manni, Florent
  • Coggiola, Clément
  • Galizzi, Julien

Abrégé

A computer-implemented method for automatically determining a target architecture from a set of target architectures in order to implement an algorithm. The method includes selecting a language associated with a compiler of the language to produce a source code for the algorithm, the compiler including at least one compilation optimization option. Compiling source code for the algorithm according to at least one compilation optimization option to produce an object code. The method includes measuring at least one performance score of the produced object code, the at least one performance score being measured according to a metric.

Classes IPC  ?

20.

METHOD AND DEVICE FOR DETERMINING A POINTING LAW FOR A SATELLITE BY DETERMINING A SPACE-TIME DISTRIBUTION

      
Numéro d'application FR2023050910
Numéro de publication 2023/247882
Statut Délivré - en vigueur
Date de dépôt 2023-06-20
Date de publication 2023-12-28
Propriétaire
  • AIRBUS DEFENCE AND SPACE SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Wenger, Thibaut
  • Picard, Mathieu
  • Tourneur, Cyrille

Abrégé

The present disclosure relates to a method for determining at least one pointing law, in a time window, for an observation instrument of at least one EO satellite (20) searching for EO space objects (50), the determination method comprising: - determining, from a list of space objects, space objects that are observable from the at least one satellite in an observation window, the duration of which is equal to or greater than the duration of the time window; - determining, in the time window and in a given satellite reference frame, referred to as the observation reference frame, a space-time distribution of the space objects that are observable in the observation window from the at least one satellite; - determining a pointing law for the observation instrument, in the time window and in the observation reference frame, according to the space-time distribution.

Classes IPC  ?

  • B64G 3/00 - Observation ou poursuite des véhicules astronautiques
  • B64G 1/10 - Satellites artificielsSystèmes de tels satellitesVéhicules interplanétaires
  • B64G 1/68 - Aménagements ou adaptations d'appareils ou d'instruments, non prévus ailleurs des détecteurs de météoroïdes ou de débris spatiaux
  • H04N 23/695 - Commande de la direction de la caméra pour modifier le champ de vision, p. ex. par un panoramique, une inclinaison ou en fonction du suivi des objets

21.

THERMOREGULATED SPACE EQUIPMENT HAVING THERMALLY INSULATING MECHANICAL SUPPORT

      
Numéro d'application FR2023050680
Numéro de publication 2023/222966
Statut Délivré - en vigueur
Date de dépôt 2023-05-12
Date de publication 2023-11-23
Propriétaire
  • AIRBUS DEFENCE AND SPACE SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Langlet, Floriane
  • Carponcin, Delphine

Abrégé

The invention relates to thermoregulated space equipment (10) which comprises at least one mechanical support structure (1) comprising a first metal portion (2) for interfacing with the equipment, which first metal portion is rigidly connected to at least one second metal portion (3) for interfacing with a space platform (20), characterised in that the mechanical support structure further comprises at least one metal mesh (4) which forms a mechanical connection between the first and second interface portions, the mechanical support structure also comprising at least one mechanically rigid and thermally insulating block of material (5) which continuously and rigidly connects the first and second interface portions and fills the metal mesh.

Classes IPC  ?

  • B64G 1/50 - Aménagements ou adaptations des dispositifs de contrôle de l'environnement ou des conditions de vie pour la commande de la température
  • B64G 1/66 - Aménagements ou adaptations d'appareils ou d'instruments, non prévus ailleurs
  • B64G 1/58 - Protection thermique, p. ex. boucliers thermiques

22.

SUBSTRATE FOR AN ELECTRONIC CHIP

      
Numéro d'application 18246933
Statut En instance
Date de dépôt 2021-10-18
Date de la première publication 2023-11-16
Propriétaire
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • Institut Polytechnique de Grenoble (France)
  • UNIVERSITE GRENOBLE ALPES (France)
  • Université de Chambéry - Université Savoie Mont Blanc (France)
Inventeur(s)
  • Febvre, Pascal
  • Yilmaz, Ugur

Abrégé

The present description concerns a support (108) for an electronic die (110), comprising: a first printed circuit board (300); a first conductive region (310), intended to receive the die, located on a first surface (108i) of the first board; and a second conductive region (320), intended to receive a thermal connector (200), located on a second surface (108s) of the first board, opposite to the first surface, the first region being connected to the second region by at least one through conductive via (330), located vertically in line with the first region.

Classes IPC  ?

  • H05K 1/02 - Circuits imprimés Détails
  • H01L 23/00 - Détails de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide
  • H05K 1/14 - Association structurale de plusieurs circuits imprimés

23.

METHOD FOR PERFORMING NON-LOCAL DEMOSAICING OF AN IMAGE, AND ASSOCIATED DEVICE

      
Numéro d'application EP2023060515
Numéro de publication 2023/208783
Statut Délivré - en vigueur
Date de dépôt 2023-04-21
Date de publication 2023-11-02
Propriétaire
  • AIRBUS DEFENCE AND SPACE SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Guillaume, Laurent
  • Thiebaut, Carole
  • Nguyen, Thien Anh

Abrégé

The invention provides a demosaicing method applied to an initial image to obtain a demosaiced image allowing improved demosaicing by virtue of the fact that it comprises: applying a stabilization transform to stabilize noise variance, and, for each reference patch: • determining (310) a set of similar patches • determining (320) a covariance matrix of said set of similar patches and • for each similar patch, computing estimates of interpolated spectral bands, depending on a block decomposition of the covariance matrix (340) depending on phasing, determining interpolated spectral bands by aggregating (350) the estimates of the interpolated spectral bands, and performing an inverse transform on the stabilization transform.

Classes IPC  ?

  • G06T 3/40 - Changement d'échelle d’images complètes ou de parties d’image, p. ex. agrandissement ou rétrécissement

24.

METHOD FOR SELECTING LOAD CASES BY DIMENSIONALITY REDUCTION FOR DIMENSIONING A REUSABLE SPACE LAUNCHER SYSTEM

      
Numéro d'application FR2023050344
Numéro de publication 2023/198972
Statut Délivré - en vigueur
Date de dépôt 2023-03-14
Date de publication 2023-10-19
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Garcia Martinez, Adrian

Abrégé

The invention relates to a method (100) for dimensioning a space launcher (LS), the space launcher (LS) comprising at least one module (M1, M2, M3), the at least one module (M1, M2, M3) comprising a structure (ST1, ST2, ST3), the method (100) comprising the following steps: - determining (101) a set of load cases to be taken into account for dimensioning the at least one module (M1, M2, M3) of the launcher (LS), a load case being defined as a combination of mechanical force components that are simultaneously applied to the structure (ST1, ST2, ST3) of the at least one module (M1, M2, M3), each combination comprising a number N of mechanical force components, the set of load cases being defined in an N-dimensional space; - projecting (102) the set into an n-dimensional hyperplane, n being smaller than N; - determining (103) a projection sheath in the hyperplane, the sheath defining a load case subset; - using (104) the load case subset to dimension the at least one module (M1, M2, M3).

Classes IPC  ?

  • B64G 1/00 - Véhicules spatiaux
  • G06F 30/15 - Conception de véhicules, d’aéronefs ou d’embarcations

25.

METHOD FOR MODELLING A DYNAMIC SYSTEM BY MEANS OF A NEURAL NETWORK, AND CORRESPONDING DEVICE

      
Numéro d'application FR2023050475
Numéro de publication 2023/194680
Statut Délivré - en vigueur
Date de dépôt 2023-04-03
Date de publication 2023-10-12
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Canart, Christian

Abrégé

Method (100) for simulating a dynamic system comprising the steps of modelling (1011) one component and another component by means of one neural network (V) and of another neural network (T1, T2), each comprising an input layer, which is configured to receive values of physical parameters (X1VV, X2VV, X3VV), (Y1VV, Y2VV, Y3VV), and values of physical parameters (Y1T1T1, Y2T1T1, Y3T1T1) (X1T2T2, X2T2T2, X3T2T1T1T2T2T2) of the other neural network (T1, T2) when the component and the other component have a common dynamic interface, so that the neural network (V) and the other neural network (T1, T2) form an interconnected network of neural networks (T1, V, T2), to model a dynamic behaviour of the dynamic system, comprising said component and said other component, and of simulating (102) the dynamic behaviour of the dynamic system.

Classes IPC  ?

  • G06F 30/27 - Optimisation, vérification ou simulation de l’objet conçu utilisant l’apprentissage automatique, p. ex. l’intelligence artificielle, les réseaux neuronaux, les machines à support de vecteur [MSV] ou l’apprentissage d’un modèle
  • G06F 113/08 - Fluides
  • G06F 113/14 - Tuyaux

26.

METHOD FOR AUTONOMOUS ORBIT CONTROL AND SATELLITE CONFIGURED TO IMPLEMENT THE METHOD

      
Numéro d'application FR2023050274
Numéro de publication 2023/180646
Statut Délivré - en vigueur
Date de dépôt 2023-03-01
Date de publication 2023-09-28
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Thomassin, Jérôme

Abrégé

The invention relates to a method (100) for controlling the orbit of a satellite, which method comprises: - determining (102) a manoeuvre plan (PMA) comprising at least one previous manoeuvre (PM1) of the previous manoeuvre plan (PPMA), if the at least one previous manoeuvre (PM1 = MA1) is implemented on a date corresponding to a previous fixed part (PPF) and the prediction horizon (HP), the manoeuvre plan (PMA) comprising at least one manoeuvre (MA2, MA3) implemented during a part of the prediction horizon; - identifying (103) a collision risk; - determining (104) a new manoeuvre plan (NPMA) comprising a previous manoeuvre (PM1, PM2, PM3) of the previous manoeuvre plan (PPMA), if the previous manoeuvre is implemented within the previous prediction horizon (PHP) and the prediction horizon (HP) of the new manoeuvre plan (NPMA), and comprising a new manoeuvre (NMA4), implemented over a new part of the prediction horizon (HP).

Classes IPC  ?

  • B64G 1/24 - Appareils de guidage ou de commande, p. ex. de commande d'assiette
  • B64G 1/52 - Dispositifs de protection, de sécurité ou de sauvetageMoyens de survie

27.

METHOD FOR MEASURING AT LEAST ONE PHYSICAL INTERFACIAL PROPERTY

      
Numéro d'application EP2023052708
Numéro de publication 2023/152051
Statut Délivré - en vigueur
Date de dépôt 2023-02-03
Date de publication 2023-08-17
Propriétaire
  • UNIVERSITE D'AIX MARSEILLE (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Medale, Marc
  • Brutin, David

Abrégé

0122 are, respectively, the density of the liquid and of the surrounding fluid.

Classes IPC  ?

  • G01N 13/02 - Recherche de la tension superficielle des liquides

28.

METHOD FOR CONTROLLING A MOTORISED SYRINGE

      
Numéro d'application EP2023052706
Numéro de publication 2023/152050
Statut Délivré - en vigueur
Date de dépôt 2023-02-03
Date de publication 2023-08-17
Propriétaire
  • UNIVERSITE D'AIX MARSEILLE (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Medale, Marc
  • Brutin, David

Abrégé

iiiiiii.

Classes IPC  ?

  • G01F 11/02 - Appareils qu'il faut actionner de l'extérieur, adaptés à chaque opération répétée et identique, pour mesurer et séparer le volume prédéterminé d'un fluide ou d'un matériau solide fluent à partir d'une alimentation ou d'un récipient sans tenir compte du poids, et pour fournir ce volume avec chambres de mesure qui se dilatent ou se contractent au cours du mesurage
  • A61M 5/19 - Seringues avec plusieurs compartiments
  • A61M 5/20 - Seringues automatiques, p. ex. avec tige de piston actionnée automatiquement, avec injection automatique de l'aiguille, à remplissage automatique
  • B01L 3/02 - BurettesPipettes
  • B05C 17/005 - Outils à main ou appareils utilisant des outils tenus à la main pour appliquer ou étaler des liquides ou d'autres matériaux fluides sur des surfaces, pour enlever partiellement des liquides ou d'autres matériaux fluides des surfaces pour décharger par pression des matériaux à travers un orifice d'évacuation
  • B05C 17/01 - Outils à main ou appareils utilisant des outils tenus à la main pour appliquer ou étaler des liquides ou d'autres matériaux fluides sur des surfaces, pour enlever partiellement des liquides ou d'autres matériaux fluides des surfaces pour décharger par pression des matériaux à travers un orifice d'évacuation avec un piston actionné mécaniquement, électriquement ou analogue
  • B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
  • B05C 11/10 - Stockage, débit ou réglage du liquide ou d'un autre matériau fluideRécupération de l'excès de liquide ou d'un autre matériau fluide
  • G01F 11/30 - Appareils qu'il faut actionner de l'extérieur, adaptés à chaque opération répétée et identique, pour mesurer et séparer le volume prédéterminé d'un fluide ou d'un matériau solide fluent à partir d'une alimentation ou d'un récipient sans tenir compte du poids, et pour fournir ce volume avec des chambres de mesure fixes ayant un volume constant au cours du mesurage avec des soupapes d'admission et de décharge du type à levée ou à boisseau coulissant

29.

RADIOFREQUENCY ANTENNA FOR A SATELLITE

      
Numéro d'application 17981059
Statut En instance
Date de dépôt 2022-11-04
Date de la première publication 2023-07-13
Propriétaire Centre National d'Études Spatiales (France)
Inventeur(s)
  • Sodki, Mehdi
  • Blanc, Ornella

Abrégé

A radiofrequency antenna is adapted to be mounted on a spacecraft. The radiofrequency antenna includes four helical strands of a super elastic shape memory alloy and is configured to move from a deployed configuration to a constrained stacking configuration and to return autonomously to the deployed configuration.

Classes IPC  ?

  • H01Q 11/08 - Antennes hélicoïdales
  • H01Q 1/36 - Forme structurale pour éléments rayonnants, p. ex. cône, spirale, parapluie
  • H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons

30.

METHOD AND SYSTEM FOR GUIDING A USER, HOLDING IN ONE HAND AN ULTRASONIC OBSERVATION PROBE, TOWARDS A PRE-RECORDED ACOUSTIC WINDOW

      
Numéro d'application FR2022052359
Numéro de publication 2023/118702
Statut Délivré - en vigueur
Date de dépôt 2022-12-14
Date de publication 2023-06-29
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • MEDES-INST MEDECINE PHYSIOLOGIE SPATIALE (France)
Inventeur(s)
  • Chaput, Didier
  • Derache, François
  • Faucoz, Orphée
  • Thevenon, Aristée

Abrégé

Method (100) for guiding a user holding in one hand (4) a probe (1) configured for ultrasonic observation of a body (5) of a patient, the method comprising the following steps: placing (101) a support at a point on the surface of the body, in order to maintain an object (3) comprising markers in a predetermined position and orientation with respect to a reference frame; acquiring (102) at least one image; determining (103) the reference frame from the markers identifiable by processing of the at least one image, the recorded position (PE) and the recorded direction (DE) of the probe (1) being defined in the reference frame; determining (104) coordinates of at least one vertex of a polygon (P) placed in a first plane transverse to the recorded direction (DE) of the probe; displaying (105) the at least one image on the display device; projecting (106) the at least one vertex of a polygon (P) onto the at least one displayed image; determining (107) the actual position (PA) and the actual direction (DA) of the probe (1) in the reference frame, based on the markers identifiable on the at least one image; determining (108) coordinates in the reference frame of at least one vertex of the polygon (P) placed in a second plane transverse to the actual direction of the probe; projecting (109) the at least one vertex onto the at least one displayed image; bringing (110) the probe into a new actual position and a new actual direction, the new actual position and the new actual direction coinciding with the recorded position (PE) and the recorded direction (DE).

Classes IPC  ?

  • A61B 8/00 - Diagnostic utilisant des ondes ultrasonores, sonores ou infrasonores
  • A61B 8/08 - Applications cliniques

31.

METHOD FOR ASSEMBLING A FIRST METAL PART WITH A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL, AND PIECE MADE FROM SUCH AN ASSEMBLY

      
Numéro d'application 17999332
Statut En instance
Date de dépôt 2021-05-10
Date de la première publication 2023-06-29
Propriétaire
  • ARIANEGROUP SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Du Tertre, Alban
  • Guichard, Didier

Abrégé

The invention relates to a method for assembling a first metal part with a second part made of an organic matrix composite material, the first part having a first connecting portion and the second part having a second connecting portion, the method comprising the steps of: causing the first connecting portion and the second connecting portion to overlap, a through-hole of the second connecting portion opening onto the first connecting portion, forming a protective layer on the side wall of the through-hole, forming a seal between the protective layer and the first connecting portion, and forming, by additive manufacturing using cold gas spray deposition of metal powder, a fastening element which extends into the through-hole, is fastened to the first connecting portion and encloses the second connecting portion.

Classes IPC  ?

  • B29C 65/00 - Assemblage d'éléments préformésAppareils à cet effet
  • B29C 65/56 - Assemblage d'éléments préformésAppareils à cet effet en utilisant des moyens mécaniques
  • B22F 5/00 - Fabrication de pièces ou d'objets à partir de poudres métalliques caractérisée par la forme particulière du produit à réaliser
  • B22F 10/25 - Dépôt direct de particules métalliques, p. ex. dépôt direct de métal [DMD] ou mise en forme par laser [LENS]
  • F02K 9/34 - CartersChambres de combustionLeurs chemises

32.

TECH in SPACE cnes

      
Numéro d'application 018885792
Statut Enregistrée
Date de dépôt 2023-06-08
Date d'enregistrement 2023-12-12
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 16 - Papier, carton et produits en ces matières
  • 25 - Vêtements; chaussures; chapellerie
  • 28 - Jeux, jouets, articles de sport
  • 35 - Publicité; Affaires commerciales
  • 38 - Services de télécommunications
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Scientific apparatus and instruments (other than for medical purposes), Photographic, cinematographic apparatus and instruments; Apparatus for recording, transmission or reproduction of sound or image; Magnetic data carriers, recording discs; Coin-operated mechanisms; Data processing equipment; Computers, telecommunication apparatus enabling connection to databases or an internet network; Software, including the following products: Software relating to space, computer software including online downloadable computer programs on the internet and the world wide web; Fire extinguishers. Printed brochures; Posters; Newspapers; Albums; Books; Picturebooks; Colouring books; Educational books; Geographical maps; Wall charts; Postcards. Clothing; Footwear; Headgear; Shirts; Leather dresses; Belts [clothing]; Furs [clothing]; Gloves [clothing]; Scarves; Neckties; Hosiery; Socks; Slippers; Sports shoes; Underwear. Games; Toys; Toys for pets; Baby gyms; Controllers for game consoles; Playground balls; Playing cards; Table-top games; Scooters [toys]; Sailboards; Sailboards; Rackets; Toy models; Toy figures; Toy robots. Direct mail advertising; Arranging newspaper subscriptions for others; Business management and organization consultancy; Computerized file management; Traffic optimisation for websites; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Commercial intermediation services. Webcasting services, Electronic communications services, Transmission of information, text, messages, data and content via the internet, by computer and via other communications means, wirelessly and via mobile telephony networks, providing of online forums, discussion forums, journals, personal online journals (blogs) for access and transmission of messages, comments and multimedia content between users; Providing access to databases; Radio broadcasting; Television broadcasting; Teleconferencing services; Videoconferencing services; Electronic messaging; Online providing (transmission) of information using a computer or data transmission database or the Internet; Instant electronic messaging services. Teaching; Training; Entertainment services; Sporting and cultural activities; Entertainment information; Education information; Publication of books; Providing films, not downloadable, via video-on-demand services; Production of cinematographic films; Photography; Organization of competitions [education or entertainment]; Arranging and conducting of colloquiums; Arranging and conducting of conferences; Arranging and conducting of congresses; Arranging of exhibitions for cultural or educational purposes; Game services provided online from a computer network; Gambling services; Online publication of electronic books and journals. Rental of access time to data processing servers and to computerised or telematic database servers, in connection with the aeronautics and space fields, including the Internet; Rental of access time to telecommunication servers including the internet, to servers of text, electronic documents, databases, graphics and audiovisual information, in relation to the following fields: Space; Rental of access time to servers of computer programs, in relation to the following fields: Space; Computer rental; Design of graphics, drawings and text for formatting Web pages on the Internet; providing online information From computer or data transmission databases or the internet, in relation to the following fields: Space engineering; Rental of access time to computer and communications networks, in relation to the following fields: Space; Computer software design, Updating of computer software, Rental of computer software, Maintenance of computer software, Technical consultancy services relating to information technology, Computer rental, Computer programming, Advice and consultancy relating to computers, Leasing access time to a computer or data transmission database, in relation to the following fields: Space; Providing of virtual facilities, namely: Real-time multimedia and collective communication on computer networks, via discussion forums; Engineering services, Professional consultations, in relation to the following fields: Space engineering; Provision of electronic mail facilities; Providing of temporary use of computer programs for use with and on the internet and the world wide web.

33.

DEPLOYMENT DEVICE FOR NANO-SATELLITE

      
Numéro d'application 17986149
Statut En instance
Date de dépôt 2022-11-14
Date de la première publication 2023-05-11
Propriétaire
  • Centre National d'Études Spatiales (France)
  • MECANO I.D. (France)
Inventeur(s)
  • Deslandes, Olivier
  • Sicre, Jacques
  • Bonnes, Lionel

Abrégé

The present disclosure concerns a device for deploying a nanosatellite including a main structure mounted on a launching vehicle, a support frame carrying the nanosatellite, and a locking/unlocking structure. The locking/unlocking structure includes a first clamping element complementary to a second clamping element of the support frame, and an elastically deformable actuating element to allow, in a locking position, constrain the first clamping element to the second clamping element to retain the support frame to the main structure, and in an unlocking position, release the first clamping element from the second clamping element to release the support frame from the main structure causing it to be ejected.

Classes IPC  ?

  • B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage

34.

Guyaspace Experience CSG

      
Numéro d'application 018862412
Statut Enregistrée
Date de dépôt 2023-04-14
Date d'enregistrement 2023-09-26
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 16 - Papier, carton et produits en ces matières
  • 28 - Jeux, jouets, articles de sport
  • 35 - Publicité; Affaires commerciales
  • 41 - Éducation, divertissements, activités sportives et culturelles

Produits et services

Telepresence robots for guiding museum visitors; Electronic pocket diaries; Electronic agendas; Decorative magnets; Videotapes; Directional compasses; Digital photo frames; Encoded key cards; Identity cards, magnetic; Memory cards for video game machines; Video game cartridges; Headphones; Video cassettes; Stick computers; Transparencies [photography]; Cinematographic film, exposed; Films, exposed; Data gloves; Holograms; Cosmographic instruments; Optical lenses; Electronic book readers; Computer game software, recorded; Downloadable game software; 3D spectacles; Magnifying glasses [optics]; Sunglasses; Smartglasses; Computers; Notebook computers; Laptop computers; Smartphones; Lens hoods; Electronic key fobs being remote control apparatus; Prisms [optics]; Satellites for scientific purposes; Tablet computers; Mobile telephones; Telescopes; Visors for helmets; Viewfinders, photographic. Printed brochures; Posters; Newspapers; Albums; Books; Picturebooks; Colouring books; Educational books; Geographical maps; Wall charts; Postcards; Almanacs; Atlases; Souvenir banknotes; Tickets; Copybooks; Calendars; Catalogues; Pencils; Envelopes [stationery]; Bunting of paper; Gums [adhesives] for stationery or household purposes; Colouring pictures; Booklets; Manuals [handbooks]; Periodicals; Pencil holders; Portraits; Index books; Sealing stamps; Stamps [seals]; Drawing sets. Balls for games; Playing cards; Kites; Flying discs [toys]; Drones [toys]; Toy figures; Table-top games; Toys; Trading card games; Board games; Arcade video game machines; Toy models; Puppets; Masks [playthings]; Plush toys; Toy pistols; Dolls; Jigsaw puzzles. Direct mail advertising; Arranging newspaper subscriptions for others; Business management and organization consultancy; Computerized file management; Traffic optimisation for websites; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Commercial intermediation services; Compilation of information into computer databases; Distribution of samples; Reception services for visitors [office functions]; Retail services in relation to the following goods: Electronic agendas, Notebook computers, Decorative magnets, videotapes, Directional compasses, Digital photo frames, encoded key cards, Magnetic identity cards, memory cards for video game machines, video game cartridges, Headphones, videocassettes, USB keys, photographic transparencies, Cinematographic film, exposed, Exposed films, Virtual reality gloves, Holograms, Cosmographic instruments, optical lenses, Electronic readers, Computer game software for computers, downloadable games software, 3D spectacles, Magnifying glasses (optics), Sunglasses, smartglasses, Computers, netbook computers, handheld computers, Smartphones, Lens hoods, electronic key fobs being remote control apparatus, Prisms (optics), Satellites for scientific purposes, computer tablets, Mobile telephones, Telescopes, visors for helmets, photographic viewfinders, Play balloons, Playing cards, Kites, Flying discs [toys], drones (toys), figurines being toys, Board games, Toys, tracing cards for games, Board games, Arcade video game machines, Models (toys), hand puppets, Masks (playthings), Plush toys, toy pistols, Dolls, Jigsaw puzzles. Providing museum facilities; Presenting museum exhibitions; Cultural services provided by museums; Museum curator services; Entertainment services provided by museums; Providing museum facilities [presentation, exhibitions]; Education provided by museums; Teaching provided by museums; Conducting of guided museum tours, For educational purposes; cultural, educational or entertainment services provided by museums; cultural, educational or entertainment services provided by museums; Teaching; Training; Entertainment services; Sporting and cultural activities; Entertainment information; Education information; Publication of books; Providing films, not downloadable, via video-on-demand services; Production of cinematographic films; Photography; Organization of competitions [education or entertainment]; Arranging and conducting of colloquiums; Arranging and conducting of conferences; Arranging and conducting of congresses; Arranging of exhibitions for cultural or educational purposes; Game services provided online from a computer network; Gambling services; Online publication of electronic books and journals.

35.

GUYASPACE

      
Numéro d'application 018862375
Statut Enregistrée
Date de dépôt 2023-04-14
Date d'enregistrement 2023-09-26
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 16 - Papier, carton et produits en ces matières
  • 28 - Jeux, jouets, articles de sport
  • 35 - Publicité; Affaires commerciales
  • 41 - Éducation, divertissements, activités sportives et culturelles

Produits et services

Telepresence robots for guiding museum visitors; Electronic pocket diaries; Electronic agendas; Decorative magnets; Videotapes; Directional compasses; Digital photo frames; Encoded key cards; Identity cards, magnetic; Memory cards for video game machines; Video game cartridges; Headphones; Video cassettes; Stick computers; Transparencies [photography]; Cinematographic film, exposed; Films, exposed; Data gloves; Holograms; Cosmographic instruments; Optical lenses; Electronic book readers; Computer game software, recorded; Downloadable game software; 3D spectacles; Magnifying glasses [optics]; Sunglasses; Smartglasses; Computers; Notebook computers; Laptop computers; Smartphones; Lens hoods; Electronic key fobs being remote control apparatus; Prisms [optics]; Satellites for scientific purposes; Tablet computers; Mobile telephones; Telescopes; Visors for helmets; Viewfinders, photographic. Printed brochures; Posters; Newspapers; Albums; Books; Picturebooks; Colouring books; Educational books; Geographical maps; Wall charts; Postcards; Almanacs; Atlases; Souvenir banknotes; Tickets; Copybooks; Calendars; Catalogues; Pencils; Envelopes [stationery]; Bunting of paper; Gums [adhesives] for stationery or household purposes; Colouring pictures; Booklets; Manuals [handbooks]; Periodicals; Pencil holders; Portraits; Index books; Sealing stamps; Stamps [seals]; Drawing sets. Balls for games; Playing cards; Kites; Flying discs [toys]; Drones [toys]; Toy figures; Table-top games; Toys; Trading card games; Board games; Arcade video game machines; Toy models; Puppets; Masks [playthings]; Plush toys; Toy pistols; Dolls; Jigsaw puzzles. Direct mail advertising; Arranging newspaper subscriptions for others; Business management and organization consultancy; Computerized file management; Traffic optimisation for websites; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Commercial intermediation services; Compilation of information into computer databases; Distribution of samples; Reception services for visitors [office functions]; Retail services in relation to the following goods: Electronic agendas, Notebook computers, Decorative magnets, videotapes, Directional compasses, Digital photo frames, encoded key cards, Magnetic identity cards, memory cards for video game machines, video game cartridges, Headphones, videocassettes, USB keys, photographic transparencies, Cinematographic film, exposed, Exposed films, Virtual reality gloves, Holograms, Cosmographic instruments, optical lenses, Electronic readers, Computer game software for computers, downloadable games software, 3D spectacles, Magnifying glasses (optics), Sunglasses, smartglasses, Computers, netbook computers, handheld computers, Smartphones, Lens hoods, electronic key fobs being remote control apparatus, Prisms (optics), Satellites for scientific purposes, computer tablets, Mobile telephones, Telescopes, visors for helmets, photographic viewfinders, Play balloons, Playing cards, Kites, Flying discs [toys], drones (toys), figurines being toys, Board games, Toys, tracing cards for games, Board games, Arcade video game machines, Models (toys), hand puppets, Masks (playthings), Plush toys, toy pistols, Dolls, Jigsaw puzzles. Providing museum facilities; Presenting museum exhibitions; Cultural services provided by museums; Museum curator services; Entertainment services provided by museums; Providing museum facilities [presentation, exhibitions]; Education provided by museums; Teaching provided by museums; Conducting of guided museum tours, For educational purposes; cultural, educational or entertainment services provided by museums; cultural, educational or entertainment services provided by museums; Teaching; Training; Entertainment services; Sporting and cultural activities; Entertainment information; Education information; Publication of books; Providing films, not downloadable, via video-on-demand services; Production of cinematographic films; Photography; Organization of competitions [education or entertainment]; Arranging and conducting of colloquiums; Arranging and conducting of conferences; Arranging and conducting of congresses; Arranging of exhibitions for cultural or educational purposes; Game services provided online from a computer network; Gambling services; Online publication of electronic books and journals.

36.

Method for constructing a high-resolution merged signal or image from a low-resolution plurality of signals or a low-resolution plurality of images

      
Numéro d'application 18079700
Numéro de brevet 12133001
Statut Délivré - en vigueur
Date de dépôt 2022-12-12
Date de la première publication 2023-04-06
Date d'octroi 2024-10-29
Propriétaire
  • UNIVERSITE PARIS CITE (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • Centre National d'Études Spatiales (France)
Inventeur(s)
  • Abergel, Rémy
  • Almansa, Andrés
  • Blanchet, Gwendoline
  • Latry, Christophe
  • Moisan, Lionel

Abrégé

A method for constructing a high-resolution merged signal from low-resolution signals acquired by an acquisition device includes acquisition of low-resolution signals (BR), measurement and/or estimation of acquisition parameters, pre-merging of the signals as a function of the low-resolution signals and of the parameters, filtering of the pre-merged signal, transmission of the filtered pre-merged signal and of the parameters, calculation of an estimate of the pre-merged signal by an inverse filtering of the filtered pre-merged signal, and determination, according to a variational method, of the high-resolution merged signal from the estimate of the pre-merged signal and of the parameters, a resolution of the merged signal is greater than a resolution of each signal.

Classes IPC  ?

  • H04N 23/80 - Chaînes de traitement de la caméraLeurs composants
  • H04N 5/265 - Mélange
  • H04N 7/18 - Systèmes de télévision en circuit fermé [CCTV], c.-à-d. systèmes dans lesquels le signal vidéo n'est pas diffusé

37.

METHOD FOR MANUFACTURING A MULTI-MATERIAL PART BY ADDITIVE MANUFACTURING, USING THE TECHNIQUE OF POWDER BED SELECTIVE LASER MELTING OR SELECTIVE LASER SINTERING

      
Numéro d'application 17793199
Statut En instance
Date de dépôt 2021-01-22
Date de la première publication 2023-02-23
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • UNIVERSITE PAUL SABATIER TOULOUSE III (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Veron, Frédéric
  • Vendier, Olivier
  • Tailhades, Philippe
  • Baco-Carles, Valérie
  • Kiryukhina, Kateryna

Abrégé

A process for manufacturing a multi-material part by additive manufacturing, includes the following steps: a) a step of providing a pre-treated metal powder comprising grains and an oxidized and porous layer on a surface of the grains; b) a selective laser powder-bed fusion step comprising implementation of steps i) and ii) as follows: i) a step of forming a layer from the pre-treated metal powder; ii) a step of melting by laser the layer, the melting step being carried out under a reactive atmosphere and comprising changing parameters of application of the laser so that at least a first region of the layer is converted so as to lower the electrical conductivity thereof, thus forming a dielectric, and so that at least a second region of the layer is densified without converting it, the at least a first region being formed when the parameters of application of the laser allow a first energy density to be applied to the first region and/or the laser beam to be kept for a first dwell time on the first region, the at least a second region being formed when the parameters of application of the laser allow a second energy density to be applied to the second region and/or the laser beam to be kept for a second dwell time on the second region, and the first energy density being higher than the second energy density and/or the first dwell time being longer than the second dwell time. A part obtained using the process is also provided.

Classes IPC  ?

  • B22F 12/40 - Moyens de rayonnement
  • B22F 10/28 - Fusion sur lit de poudre, p. ex. fusion sélective par laser [FSL] ou fusion par faisceau d’électrons [EBM]
  • B22F 1/145 - Traitement chimique, p. ex. passivation ou décarburation
  • B22F 1/16 - Particules métalliques revêtues d'un non-métal
  • C22C 1/10 - Alliages contenant des composants non métalliques
  • B33Y 10/00 - Procédés de fabrication additive
  • B33Y 70/10 - Composites de différents types de matériaux, p. ex. mélanges de céramiques et de polymères ou mélanges de métaux et de biomatériaux
  • B33Y 40/10 - Prétraitement

38.

FIBRE-OPTIC INTERFEROMETER BASED ON A MONOFREQUENCY LASER SOURCE AND INTERFEROMETRY METHOD CORRECTED FOR PARASITIC REFLECTIONS

      
Numéro d'application EP2022068942
Numéro de publication 2023/280992
Statut Délivré - en vigueur
Date de dépôt 2022-07-07
Date de publication 2023-01-12
Propriétaire
  • IXBLUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Ducloux, Eric

Abrégé

ττ defining a natural frequency (A). According to the invention, the laser source (8) is a monofrequency laser source and the light generator (1) comprises modulation means (7, 9) designed to modulate the source beam (10) at a modulation frequency equal to (B), where n is an integer greater than or equal to 1, and the photodetector (5) and the electronic signal-processing system (6) are configured to acquire and process a signal representative of the interference beam (15) at a demodulation frequency equal to (C).

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique

39.

SUBSTRATE COATED WITH A LUBRICANT COATING

      
Numéro d'application FR2022050999
Numéro de publication 2022/254130
Statut Délivré - en vigueur
Date de dépôt 2022-05-25
Date de publication 2022-12-08
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE LYON (France)
  • LUXEMBOURG INSTITUTE OF SCIENCE AND TECHNOLOGY (LIST) (Luxembourg)
Inventeur(s)
  • Chemin, Jean-Baptiste
  • Choquet, Patrick
  • Colas, Guillaume
  • Saulot, Aurélien
  • Yann, Michel

Abrégé

The invention relates to a substrate coated with a coating consisting of molybdenum (Mo) atoms, sulfur (S) atoms, tantalum (Ta) atoms and oxygen (O) atoms present in the form of one or more compounds chosen from the compounds of formula (I): [Chem 16] MowSxTayOz (I) in which w is equal to 0 or 1; x ranges from 0 to 2; y ranges from 0 to 1 and z ranges from 0 to 3; said coating comprising at least 5 at.% of oxygen and said coating having a dense compact microstructure.

Classes IPC  ?

  • C23C 14/00 - Revêtement par évaporation sous vide, pulvérisation cathodique ou implantation d'ions du matériau composant le revêtement
  • C23C 14/06 - Revêtement par évaporation sous vide, pulvérisation cathodique ou implantation d'ions du matériau composant le revêtement caractérisé par le matériau de revêtement
  • C23C 14/08 - Oxydes
  • C23C 14/34 - Pulvérisation cathodique
  • C23C 14/35 - Pulvérisation cathodique par application d'un champ magnétique, p. ex. pulvérisation au moyen d'un magnétron

40.

SPACECRAFT FOR ELECTRICITY DISTRIBUTION, AND ASSOCIATED METHOD

      
Numéro d'application FR2022050901
Numéro de publication 2022/238660
Statut Délivré - en vigueur
Date de dépôt 2022-05-11
Date de publication 2022-11-17
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • SAFRAN AIRCRAFT ENGINES (France)
  • THALES (France)
Inventeur(s)
  • Bultel, Pascal
  • Durand, Gautier
  • Thiry, Nicolas
  • Ansart, Marie
  • Bouhours, Gilles
  • Duchemin, Olivier
  • Marchandise, Frédéric

Abrégé

The invention relates to a spacecraft (1) for the distribution of electrical energy to client craft (2) at points situated in free space, in orbit and/or on a celestial body, the spacecraft (1) comprising a main structure (10) equipped with an electric thruster (10A), with a chemical thruster (10B) and with a solar generator (10C), a first fuel container (11) for fuel intended for the electric thruster (10A), and a second fuel container (12) for fuel intended for the chemical thruster (10B), the spacecraft (1) being able to be modulated such that: the main structure (10) can be coupled/decoupled alternatively to/from the first container (11) or the second container (12), the first container (11) and the second container (12) being able to be coupled/decoupled to/from one another, the solar generator (10C) being intended to be deployed or retracted.

Classes IPC  ?

  • B64G 1/10 - Satellites artificielsSystèmes de tels satellitesVéhicules interplanétaires
  • B64G 1/40 - Aménagements ou adaptations des systèmes de propulsion
  • B64G 1/42 - Aménagements ou adaptations des systèmes fournissant l'énergie
  • B64G 1/62 - Systèmes de retour sur terreDispositifs de freinage ou d'atterrissage
  • B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage
  • B64G 1/16 - Voitures extra-terrestres

41.

COMPUTER-IMPLEMENTED METHOD FOR AUTOMATICALLY DETERMINING A TARGET ARCHITECTURE

      
Numéro d'application FR2022050776
Numéro de publication 2022/234209
Statut Délivré - en vigueur
Date de dépôt 2022-04-25
Date de publication 2022-11-10
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Manni, Florent
  • Coggiola, Clément
  • Galizzi, Julien

Abrégé

The invention relates to a computer-implemented method (100) for automatically determining a target architecture from a set of target architectures in order to implement an algorithm, the method comprising the following steps: selecting (101) a language to produce a source code for the algorithm, the language being associated with a compiler of the language, the compiler comprising at least one compilation optimisation option; compiling (102) the source code for the algorithm according to the at least one compilation optimisation option to produce an object code; measuring (103) at least one performance score of the produced object code, the at least one performance score being measured according to a metric; determining (105) the target architecture after calculating (104) an affinity function from the at least one performance score of the object code produced by the at least one compilation optimisation option and from at least one reference score of a reference object code produced by compiling a reference source code produced for a reference algorithm in the selected language, the reference algorithm being associated with the target architecture.

Classes IPC  ?

  • G06F 8/41 - Compilation
  • G06F 8/77 - Métriques logicielles
  • G06F 11/34 - Enregistrement ou évaluation statistique de l'activité du calculateur, p. ex. des interruptions ou des opérations d'entrée–sortie

42.

Ion propulsion device

      
Numéro d'application 17762303
Numéro de brevet 11993402
Statut Délivré - en vigueur
Date de dépôt 2020-09-22
Date de la première publication 2022-11-03
Date d'octroi 2024-05-28
Propriétaire
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • UNIVERSITE PARIS-SACLAY (France)
Inventeur(s)
  • Gierak, Jacques
  • Boniface, Claude
  • Lepesant, Mathieu

Abrégé

An ion propulsion device including emission modules in an emission plane, each module having an insulating support, an emission electrode on the support, and a conductive liquid with a microfluidic channel depositing conductive liquid on the electrode; an extraction electrode common to the emission modules and facing the modules; and a control unit, in which each module is configured to emit an ion beam when an electric field is applied to the liquid; each control unit controls an ion emission current emitted by applying a potential difference between each emission electrode and the extraction electrode; the emission electrodes are spaced apart by a linear distance that is greater than a distance between two adjacent emission electrodes separated by an empty space; and a length of the insulating support between the electrodes is greater than a propagation distance of an electric leakage current by charge jumping along the support between the electrodes.

Classes IPC  ?

  • B64G 1/40 - Aménagements ou adaptations des systèmes de propulsion
  • H01J 27/26 - Sources d'ionsCanons à ions utilisant l'ionisation de surface, p. ex. sources d'ions à effet de champ, sources d'ions thermo-ioniques

43.

METHOD FOR CONTROLLING AN ELECTROMAGNETIC ACTUATOR OF AN EXPANSION VALVE, AND ACTUATOR AND EXPANSION VALVE CONFIGURED TO IMPLEMENT SAID METHOD

      
Numéro d'application FR2022050372
Numéro de publication 2022/200710
Statut Délivré - en vigueur
Date de dépôt 2022-03-02
Date de publication 2022-09-29
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CONCEPTION DE SYSTEMES ET TECHNOLOGIE MECANIQUE (CSTM) (France)
  • INSTITUT CATHOLIQUE D'ARTS ET METIERS (ICAM) (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Deschaux, Flavien
  • Ariba, Yassine
  • De Seze, Damien
  • Gouaisbaut, Frédéric
  • Dugue, François

Abrégé

The invention relates to an electronically controlled expansion valve (1) having a controlled valve (10) inserted between a source (2) at a first pressure (P1) and an outlet (3) at a second pressure (P2), a pressure sensor (9) designed to measure the second pressure and a computer (7) designed to control the valve (10) so as to bring about a pressure drop between the source and the outlet, making it possible to feedback-control the second pressure (P2) to a setpoint pressure (Pref), the valve (10) comprising an actuator (14) for driving a member (13) for restricting a passage section (11) for the fluid, between the source (2) and the fluid outlet (3), so as to vary the passage section, the restriction (11) being implemented by means of a passage orifice (12) for the fluid and a shut-off member (13) placed on the axis of the orifice and designed such that an axial movement of the shut-off member (13) brings about a variation in the passage section (11) for the fluid, the expansion valve (1) having a position sensor (19) for the shut-off member (13), characterized in that the computer (7) uses a first control law (LC1) to make the position (X1) of the shut-off member (13) converge towards a setpoint position (Yr), the setpoint position (Yr) being determined via a second control layer (LC2) for making the second pressure (P2) converge towards the setpoint pressure (Pref), on the basis of a model (MD) of a flow rate (Dcol) through the expansion valve (1), the second control law (LC2) also being determined on the basis of a model (MP) of the second pressure (P2) as a function of the flow rate (Dcol) through the expansion valve and a consumption flow rate (Ds) downstream of the fluid outlet (3).

Classes IPC  ?

  • G05D 16/20 - Commande de la pression d'un fluide caractérisée par l'utilisation de moyens électriques

44.

GENERATOR FOR GENERATING AN ANTI-KERR-EFFECT MODULATED LIGHT SIGNAL, INTERFEROMETRY MEASURING DEVICE COMPRISING SUCH A GENERATOR, AND METHOD FOR MODULATING A LIGHT SIGNAL

      
Numéro d'application EP2022055460
Numéro de publication 2022/184855
Statut Délivré - en vigueur
Date de dépôt 2022-03-03
Date de publication 2022-09-09
Propriétaire
  • IXBLUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Ducloux, Eric
  • Ollivier, Christophe

Abrégé

MesMesMes). The invention also relates to a modulation method and to a measuring device.

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique
  • G01R 15/24 - Adaptations fournissant une isolation en tension ou en courant, p. ex. adaptations pour les réseaux à haute tension ou à courant fort utilisant des dispositifs modulateurs de lumière

45.

METHOD FOR REDUCING THE KERR EFFECT IN AN INTERFEROMETRY MEASURING DEVICE, AND INTERFEROMETRY MEASURING DEVICE CONFIGURED TO IMPLEMENT THIS METHOD

      
Numéro d'application EP2022055467
Numéro de publication 2022/184860
Statut Délivré - en vigueur
Date de dépôt 2022-03-03
Date de publication 2022-09-09
Propriétaire
  • IXBLUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Ducloux, Eric
  • Lhomme, Louis
  • Grossard, Nicolas
  • Hauden, Jérôme

Abrégé

The invention relates to a method for reducing the Kerr effect in an interferometry measuring device (1) comprising a generator configured to emit an input periodic light signal (3), and a Sagnac interferometer (4) in which two counterpropagating signals (15, 16) travel and combine so as to form a periodic output signal (11) having at least two power values, the method comprising a. determining a phase shift between the two counterpropagating signals (15, 16) a first time and cancelling out the phase shift, and then b. determining a phase shift between the two counterpropagating signals (15, 16) a second time, c. adjusting the ratio between the average powers of the counterpropagating signals (15, 16) so as to cancel out the value of the phase shift determined in the second determination. The invention also relates to an interferometry measuring device configured to implement the method according to the invention.

Classes IPC  ?

  • G01C 19/72 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées à faisceaux lumineux tournant dans des directions opposées dans un anneau passif, p. ex. gyromètres à laser à fibre optique

46.

AEROSTAT INTENDED TO PERFORM MISSIONS FOR TRANSPORTING A PAYLOAD

      
Numéro d'application FR2021052412
Numéro de publication 2022/144516
Statut Délivré - en vigueur
Date de dépôt 2021-12-21
Date de publication 2022-07-07
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Nicot, Jean-Marc

Abrégé

The present invention relates to an aerostat (1) comprising: - an inflatable body (2) configured to be pressurised by a gas lighter than the atmosphere, - a payload support member (3) configured to support a payload, the support member being arranged under the inflatable body and being connected to the inflatable body, - a solar energy generator (7) arranged under the support member and connected to the support member, the solar energy generator being retractable between a first position referred to as the storage position, and a second position referred to as the use position, the solar energy generator comprising a plurality of photovoltaic panels (72) which are retractable between the storage position, in which the photovoltaic panels are grouped and extend horizontally below one another in horizontal planes (P), and the use position, in which the photovoltaic panels are deployed and extend vertically below one another in the same vertical plane (V).

Classes IPC  ?

  • B64B 1/40 - Ballons
  • B64B 1/48 - Ballons associés à des appareils provoquant l'éclatement pour permettre à la charge emportée d'être larguée par parachute

47.

METHOD FOR ACQUIRING AND ANALYSING A SCENE BY IMAGE DIFFERENCE

      
Numéro d'application FR2021052023
Numéro de publication 2022/123133
Statut Délivré - en vigueur
Date de dépôt 2021-11-16
Date de publication 2022-06-16
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Bourcier, Frédéric
  • Infante, Fulvio
  • Thin, Guillaume

Abrégé

Disclosed is a method (100) for acquiring and analysing a scene (4) by image difference, the method (100) comprising the steps of acquiring (101) a first image of the scene (4), the first image being formed by ambient light reflected or scattered by the scene; excitation (102) of the scene by an excitation source (1), the excitation (102) triggering an emission of light from at least part of the scene, during an emission time period; acquiring (103) a second image of the scene, the acquiring (103) of the second image being synchronised with the excitation (102) so that the acquisition of the second image is carried out during the emission time, the second image being formed by the emission of light from the scene added to the reflected or scattered ambient light; calculating a second image (104) adjusted with respect to the first image in order to compensate a relative movement of the scene with respect to the sensor (2), calculating (105) a differential image, the differential image being a difference between the first image and the second, adjusted image.

Classes IPC  ?

  • H04N 5/232 - Dispositifs pour la commande des caméras de télévision, p.ex. commande à distance
  • G06T 7/254 - Analyse du mouvement impliquant de la soustraction d’images
  • H04N 5/225 - Caméras de télévision

48.

SUBSTRATE FOR AN ELECTRONIC CHIP

      
Numéro d'application EP2021078761
Numéro de publication 2022/084224
Statut Délivré - en vigueur
Date de dépôt 2021-10-18
Date de publication 2022-04-28
Propriétaire
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • INSTITUT POLYTECHNIQUE DE GRENOBLE (France)
  • UNIVERSITE GRENOBLE ALPES (France)
  • UNIVERSITE DE CHAMBERY - UNIVERSITE SAVOIE MONT BLANC (France)
Inventeur(s)
  • Febvre, Pascal
  • Yilmaz, Ugur

Abrégé

The present description relates to a substrate (108) for an electronic chip (110), comprising: a first printed circuit board (300); a first conductive region (310), intended to receive the chip and located on a first face (108i) of the first board; and a second conductive region (320), intended to receive a thermal connector (200) and located on a second face (108s) of the first board, opposite the first face, the first region being connected to the second region by at least one conductive through-via (330) located plumb with the first region.

Classes IPC  ?

  • H05K 1/02 - Circuits imprimés Détails
  • H01L 23/367 - Refroidissement facilité par la forme du dispositif
  • H01L 23/44 - Dispositions pour le refroidissement, le chauffage, la ventilation ou la compensation de la température le dispositif complet étant totalement immergé dans un fluide autre que l'air
  • H01L 23/13 - Supports, p. ex. substrats isolants non amovibles caractérisés par leur forme
  • H01L 23/498 - Connexions électriques sur des substrats isolants

49.

TECH THE MOON

      
Numéro d'application 1645460
Statut Enregistrée
Date de dépôt 2021-12-20
Date d'enregistrement 2021-12-20
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Provision of advice and providing information in the fields of organization and management of commercial affairs in the aeronautical and space sector; services provided by consultants and provision of advice in the field of company strategy; providing information and providing advice in relation to economic activities in the aeronautical and space fields for commercial purposes; business management; business administration; business management and organization consultancy; computer file management; collection and systematization of data in a central file; organization of exhibitions for commercial or advertising purposes; online advertising on a computer network; public relations; promotion and communication services in the aeronautical and space fields, information agencies in relation to commercial activities in the aeronautical and space fields; economic research services for commercial purposes. Provision of investment advice; advisory services in relation to financial grants; financial advisory services in relation to joint ventures; advice, information, research and consulting relating to finance and investment. Providing coaching services and educational programs in the field of commercial growth, business management and business development in the aeronautical and space fields; education services, namely, continuing education programs in the field of business, commercial growth, business management, business development, and business start-ups accessible via the Internet in the aeronautical and space fields; educational services, namely, developing, arranging, and conducting educational conferences and programs and providing courses of instruction in the fields of business, business acceleration and investments in the aeronautical and space fields; educational services, namely, developing, arranging, and conducting educational conferences and programs, as well as providing courses of instruction in the field of business and/or commercial growth, business management, commercial development for the purpose of connecting creators with other entrepreneurs, experts, consultants, alumni, investors, community managers and companies for growing their company in the aeronautical and space fields. Scientific information services in the aeronautical and space field; provision of technical advice in connection with the aeronautical and space fields; engineering research services; technological research in connection with the aeronautical and space fields; scientific research and analysis; technical research projects and studies; research in the field of physics; scientific research and development; industrial research and analysis services; research for development of new products; research and development services in connection with physics; industrial research, testing and analysis services; provision of information relating to technological research; research, development, analysis and consultant services in the field of engineering; provision of information regarding studies, technical projects and research on the use of natural energy; evaluations and research conducted by engineers; design and development of computers and software; research and development of new products for others; technical project studies particularly in the fields of air and space travel; computer programming; conversion of data or documents from physical to electronic media; developing standards and means for standardization (engineering); research and development of electronic and computer systems in the fields of computing and telecommunications for aeronautics and space; technical research on implementing standards and standardization; services involving standardization, namely developing (design) technical standards for manufactured goods and for telecommunication services; research on quality control and performance evaluation; professional scientific consultations and drawing up technological projects unrelated to business matters; engineering works (not for building purposes); design of graphics, drawings and text for creating web pages on the Internet; materials testing in technical laboratories; tests on the adaptability to the air and space travel environment of products from the radar industry, the optical industry, the spacecraft industry, the navigation satellite industry; research in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology and geology, and tests on the adaptability to the space travel environment of products stemming from this research; development of global satellite navigation systems; scientific research into basic technologies; research in the field of robotic exploration of other planets; research in connection with preparatory programs with a view to future launches of rockets, satellites and space shuttles; research for the development of space technology; scientific research for observing the Earth, for human exploration and transportation, for human space travel or for space engineering; research into space technology; scientific services, including testing for others, research missions and scientific coordination; development of Web pages for displaying scientific information in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology, geology and satellite technology research; research for fine-tuning technology and developping products; materials testing in an orbital environment; research on the adaptability of various components to the space environment; computer rental.

50.

RECEIVER OF RADIONAVIGATION SIGNALS COMPRISING A COMPUTER OF A CORRELATION POWER INDICATOR

      
Numéro d'application FR2021051079
Numéro de publication 2021/255386
Statut Délivré - en vigueur
Date de dépôt 2021-06-16
Date de publication 2021-12-23
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • M3 SYSTEMS (France)
Inventeur(s)
  • Lestarquit, Laurent
  • Jardak, Nabil

Abrégé

Receiver (10) of radionavigation signals, comprising a radiofrequency stage (E1); a generator (E2) of a carrier-replica signal (Srep(t)); a mixer (47) for mixing the carrier-replica signal (Srep(t)) with a digitised GNSS signal (Sr(t)); a loop (E4) for automatically controlling code position, comprising a generator (E4a) of code-replica signals; a plurality of correlators (E4c) able to compute a correlation function between the main code-replica signal (SCR(L)(t)) and the baseband signal Sbb(t) in order to produce a main correlation (50); a computer (E4d) of a correlation-power indicator, which is configured to determine correlation powers and to determine a maximum correlation power; a correction computer (E4e) configured to determine an adjusted code frequency; the loop (E4) for automatically controlling code position comprising an output that delivers at least the main correlation (50).

Classes IPC  ?

  • G01S 19/25 - Acquisition ou poursuite des signaux émis par le système faisant intervenir des données d'assistance reçues en provenance d'un élément coopérant, p. ex. un GPS assisté
  • G01S 19/30 - Acquisition ou poursuite des signaux émis par le système lié au code

51.

TECH THE MOON

      
Numéro d'application 216724500
Statut En instance
Date de dépôt 2021-12-20
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

(1) Prestation de conseil et mise à disposition d'informations dans le domaines de l'organisation et de la direction des affaires commerciales dans le secteur aéronautique et spatial; services de conseillers et prestation de conseils dans le domaine de la stratégie d'entreprises; mise à disposition d'informations et prestation de conseils en rapport avec des activités économiques dans les domaines aéronautique et spatial à des fins commerciales; direction des affaires; administration des affaires; conseils en organisation et direction des affaires; gestion de fichiers informatiques; recueil et systématisation de données dans un fichier central; organisation d'expositions à buts commerciaux ou de publicité; publicité en ligne sur un réseau informatique; relations publiques; services de promotion et de communication dans les domaines aéronautique et spatial, agences d'informations en rapport avec des activités commerciales dans les domaines aéronautique et spatial; services de recherches en matière économique à des fins commerciales. (2) Prestation de conseils en investissement; services de conseil en rapport avec les subventions financières; services de conseils financiers en rapport avec des coentreprises; prestation de conseils, services d'information, de conseillers et de recherche en matière de finance et d'investissements. (3) Prestation de services d'encadrement et programmes éducatif dans le domaine de la croissance commerciale, de la gestion d'affaires et du développement d'affaires dans les domaines aéronautique et spatial; services d'éducation, à savoir programmes de formation continue dans le domaine des affaires, de la croissance commerciale, de la gestion d'affaires, du développement d'affaires et des jeunes entreprises (start-ups) accessibles par le biais d'Internet dans les domaines aéronautique et spatial; services éducatifs, à savoir développement, mise en place et animation de programmes et de conférences pédagogiques et mise à disposition de cours d'enseignement dans les domaines des affaires, de l'accélération d'affaires et des investissements dans les domaines aéronautique et spatial; services éducatifs, à savoir développement, mise en place et animation de programmes et de conférences pédagogiques, ainsi que mise à disposition de cours d'enseignement dans le domaine des affaires et/ou de la croissance commerciale, de la gestion d'affaires, du développement commercial dans le but de connecter des créateurs avec d'autres entrepreneurs, experts, conseillers, anciens élèves, investisseurs, responsables communautaires et entreprises pour la croissance de leur entreprise dans les domaines aéronautique et spatial. (4) Services d'information scientifiques dans le domaine aéronautique et spatial; fourniture de conseils techniques en rapport avec les domaines aéronautique et spatial; recherches en ingénierie; recherches technologiques en rapport avec les domaines aéronautique et spatial; analyses et recherches scientifiques; études et projets de recherches techniques; recherches dans le domaine de la physique; recherches et développement scientifiques; recherches et analyses industrielles; recherches pour le développement de nouveaux produits; services de recherches et développement en rapport avec la physique; services de recherches, d'essais et d'analyses industriels; mise à disposition d'informations en matière de recherches technologiques; services de recherches, de développement, d'analyse et de conseillers dans le domaine de l'ingénierie; mise à disposition d'informations concernant des études de projets techniques et des recherches relatives à l'utilisation d'énergies naturelles; évaluations et recherches menées par des ingénieurs; conception et développement d'ordinateurs et de logiciels; recherches et développement de nouveaux produits pour des tiers; études de projets techniques en particulier en matière d'aéronautique et spatiale; programmation d'ordinateurs; conversion de données ou de documents d'un support physique vers un support électronique; développement de normes et moyens de normalisation (ingénierie); recherches et développement de systèmes électroniques et informatiques dans les domaines de l'informatique et des télécommunications pour l'aéronautique et le spatial; recherches techniques sur la mise en place de normes et la normalisation; services de normalisation, à savoir développement (conception) de normes techniques pour produits manufacturés et pour services de télécommunications; recherches sur le contrôle de la qualité et l'évaluation de la performance; consultations professionnelles scientifiques et élaboration de projets technologiques sans rapport avec les affaires; travaux d'ingénierie (pas pour la construction); services de conception de graphismes, dessins et textes pour la réalisation de pages Web sur le réseau Internet; essais de matériaux dans un laboratoire technique; essais sur l'adaptabilité en milieu aéronautique et spatial des produits de l'industrie du radar, de l'industrie optique, de l'industrie des engins spatiaux, de l'industrie des satellites de navigation; recherches dans les domaines des sciences, de l'astronomie, de la technologie, de l'aéronautique, de l'océanographie, de la météorologie et de la géologie, et essais sur l'adaptabilité en milieu spatial des produits issus de ces recherches; développement de systèmes de navigation satellitaire mondiaux; recherches scientifiques sur les technologies fondamentales; recherches en matière d'exploration robotisée de différentes planètes; recherches en matière de programmes de préparations en vue de futurs lancements de fusées, de satellites et de navettes spatiales; recherches pour le développement de technologies spatiales; recherche scientifique pour l'observation de la terre, pour l'exploration et le transport des hommes, pour les voyages des hommes dans l'espace ou pour l'ingénierie spatiale; recherches sur la technologie spatiale; services scientifiques, y compris les tests pour des tiers, les missions de recherche et la coordination scientifique; développement de pages Web pour faire figurer des informations scientifiques dans les domaines de la science, de l'astronomie, de la technologie, de l'aéronautique, de l'océanographie, de la météorologie, de la géologie et de la recherche sur la technologie satellitaire; recherches pour affiner des technologies et développer des produits; essais de matériaux en milieu orbital; recherches sur l'adaptabilité de différents composants en milieu spatial; services de location d'ordinateurs.

52.

TECH THE MOON

      
Numéro de série 97181293
Statut Enregistrée
Date de dépôt 2021-12-20
Date d'enregistrement 2024-05-07
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Proving consultancy and information in the fields of Business organization and Business management in the aeronautical and space sectors; Providing of consultancy and advice in the field of business strategy; Providing of business information and advice relating to economic activities in the aeronautical and space fields; Conducting business surveys; Business administration; Business management and organization consultancy; Computerized file management; Collection and systematic ordering of data in a central file for business purposes; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Public relations consultancy; Promotion and communication, namely, sales promotion, promoting the goods and services of others, consultancy regarding advertising communication strategies in the aeronautical and space fields, commercial information agencies relating to commercial activities in the aeronautical and space fields; Providing business research relating to economics, for commercial purposes Providing investment advice; Financial consultancy relating to financial subsidies in the field of in the aeronautical and space fields ; Financial consultancy relating to joint ventures; Providing of advice, information, consultancy and financial research relating to finance and investments Educational services, namely, providing coaching and educational programs featuring Business growth, Management of business and Business development, In the aeronautical and space fields; Educational services, namely, continuous training programs in the field of business, business growth, business management, business development and start-up development accessible via the internet in the aeronautical and space fields; Educational services, namely, the development, implementation and conducting of pedagogical programs and conferences and the providing of instructional courses in the fields of business, business acceleration and investments in the aeronautical and space fields; Educational services, namely, the development, implementation and conducting of pedagogical programs and conferences, as well as the providing of instructional courses in the field of business and business growth, business management, business development with the purpose of connecting creators with other entrepreneurs, experts, advisors, alumni, investors, community leaders and companies for the growth of their company in the aeronautical and space fields Scientific information services in the aeronautical and space fields; Providing technical advice relating to the aeronautical and space fields; Engineering research in the aeronautical and space fields; Technological research relating to the aeronautical and space fields; Scientific research and analysis in the aeronautical and space fields; Technical research projects and studies in the aeronautical and space fields; Research in the field of physics; Scientific research and development; Industrial analysis and research services in the aeronautical and space fields; Research to develop new products; Research and development services relating to physics; Industrial research, testing and analysis in the aeronautical and space fields; Provision of information relating to technological research in the aeronautical and space fields; Research, development, analysis and consultancy in the field of civil, mechanical engineering; Provision of information concerning scientific, engineering research and technical project studies relating to the use of natural energy; Evaluations and research conducted by engineers in the aeronautical and space fields; Design and development of computer hardware and software; Research and development of new products for others; Technical research project studies, in particular in connection with aeronautics and space; Computer programming; Conversion of data or documents from physical to electronic media; Development of voluntary standards and standardization means for engineering, namely services of start-up incubator ; Research and development of electronic and computer systems in the fields of computing and telecommunications for the aeronautics and space sectors; Technical research relating to the establishment of standards and standardization in the aeronautical and space fields; Standardization, namely, development and design of voluntary technical standards for manufactured goods in the aeronautical and space fields and for telecommunications; Research relating to quality control and performance evaluation in the aeronautical and space fields; Professional scientific consultancy and development of technology projects featuring aeronautical and space projects not relating to business; Engineering, not for construction purposes; Design of graphics, drawings and text for formatting Web pages on the Internet; Testing of materials in a technical laboratory; Testing of materials relating to adaptability, in the aeronautics and space sectors, of goods from the radar, optical, space engines and satellite navigation industries; Research in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology and geology in the field of video surveillance equipment, and testing of materials relating to adaptability, in the space sector, of goods derived from this research; Development of global satellite navigation systems; Scientific research into core technologies in the aeronautical and space fields; Research into the robotic exploration of other planets; Scientific research into programs for preparing for future launches of rockets, satellites and space shuttles; Research for the development of space technology; Scientific research for Earth observation, for human exploration and transport, for human travel into space or for space engineering; Research relating to space technology; Scientific services, including tests for others, research missions and scientific coordination, namely, scientific research, in the aeronautical and space fields; Development of web pages for others for presenting scientific information in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology, geology and satellite technology research; Research for refining technologies in the aeronautical and space fields and developing new products; Testing of materials in orbit; Research into the adaptability of different components in the aeronautical and space fields in space; Computer rental

53.

METHOD FOR CONSTRUCTING A HIGH-RESOLUTION MIXED SIGNAL OR IMAGE FROM A PLURALITY OF LOW-RESOLUTION SIGNALS OR A PLURALITY OF LOW-RESOLUTION IMAGES

      
Numéro d'application FR2021051041
Numéro de publication 2021/250356
Statut Délivré - en vigueur
Date de dépôt 2021-06-10
Date de publication 2021-12-16
Propriétaire
  • UNIVERSITE DE PARIS (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Abergel, Rémy
  • Almansa, Andrés
  • Blanchet, Gwendoline
  • Latry, Christophe
  • Moisan, Lionel

Abrégé

Method (100) for constructing a high-resolution (HR) mixed signal from low-resolution (BR) signals acquired by an acquisition device (10), comprising the following steps: acquiring (101) low-resolution signals (BR); measuring and/or estimating (101') acquisition parameters (PA); pre-mixing (101a) the signals according to the low-resolution signals and the parameters (PA); filtering (101b) the pre-mixed signal; transmitting (102) the filtered pre-mixed signal and the parameters (PA); calculating (103) an estimate of the pre-mixed signal by inversely filtering the pre-mixed filtered signal; determining (104), according to a variational method, the high resolution mixed signal from the estimate of the pre-mixed signal and the parameters, a resolution of the mixed signal being greater than a resolution of each signal.

Classes IPC  ?

  • G06T 5/00 - Amélioration ou restauration d'image
  • G06T 5/50 - Amélioration ou restauration d'image utilisant plusieurs images, p. ex. moyenne ou soustraction

54.

AEROSTAT INTENDED TO PERFORM MISSIONS FOR TRANSPORTING A PAYLOAD

      
Numéro d'application FR2021051012
Numéro de publication 2021/245363
Statut Délivré - en vigueur
Date de dépôt 2021-06-04
Date de publication 2021-12-09
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Behar, Jean-Baptiste

Abrégé

The present invention relates to an aerostat (1) comprising: - an inflatable body (2) having a cylindrical shape comprising a first pole (22) and a second pole (24), - a triangular sail (4) arranged under the inflatable body and comprising a first vertex (42) and a second vertex (44) such that a first side (46) of the sail extends in contact with the inflatable body, the sail comprising a third free vertex (48) with a payload (5) attached thereto, - a fastening device (7) comprising a first strand (70) and a second strand (72), the fastening device being connected to a cable (6) configured to keep the aerostat connected to a surface of the planet with an atmosphere.

Classes IPC  ?

  • B64B 1/52 - Attache des agrès de remorque
  • B64B 1/58 - Disposition ou structure des ballonnetsRemplissage
  • B64B 1/24 - Disposition des installations de propulsion

55.

STRUCTURE FOR ASSEMBLING A PIECE COMPRISING A FIRST METAL PART AND A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL

      
Numéro d'application FR2021050812
Numéro de publication 2021/234245
Statut Délivré - en vigueur
Date de dépôt 2021-05-11
Date de publication 2021-11-25
Propriétaire
  • ARIANEGROUP SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Fontaine, Arnaud
  • Du Tertre, Alban
  • Guichard, Didier

Abrégé

The invention relates to a piece comprising a first metal part (12) and a second part (14) made of an organic matrix composite material, in which the first part (12) has a first connecting portion (12A) and the second part (14) has a second connecting portion (14A), the second connecting portion (14A) having at least one blind hole (14B1, 14B2), the second connecting portion (14A) being totally or partially sandwiched between the first connecting portion (12A) and a metal fastening element (16), the fastening element (16) being fixed to the first part (12) on a portion (12D) other than the first connecting portion (12A) and extending into the at least one blind hole (14B1, 14B2), whereby the first part (12) and the second part (14) are fixed to one another.

Classes IPC  ?

  • B29C 65/64 - Assemblage d'un élément en matière autre que plastique avec un élément en matière plastique, p. ex. à force
  • F02K 9/00 - Moteurs-fusées, c.-à-d. ensembles fonctionnels portant à la fois le combustible et son oxydantLeur commande
  • B22F 10/25 - Dépôt direct de particules métalliques, p. ex. dépôt direct de métal [DMD] ou mise en forme par laser [LENS]
  • B22F 7/08 - Fabrication de couches composites, de pièces ou d'objets à base de poudres métalliques, par frittage avec ou sans compactage de pièces ou objets composés de parties différentes, p. ex. pour former des outils à embouts rapportés avec une ou plusieurs parties non faites à partir de poudre
  • B33Y 80/00 - Produits obtenus par fabrication additive
  • B29K 105/06 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts

56.

METHOD FOR ASSEMBLING A FIRST METAL PART WITH A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL, AND PIECE MADE FROM SUCH AN ASSEMBLY

      
Numéro d'application FR2021050804
Numéro de publication 2021/234242
Statut Délivré - en vigueur
Date de dépôt 2021-05-10
Date de publication 2021-11-25
Propriétaire
  • ARIANEGROUP SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Du Tertre, Alban
  • Guichard, Didier

Abrégé

The invention relates to a method for assembling a first metal part (12) with a second part (14) made of an organic matrix composite material, the first part (12) having a first connecting portion (12A) and the second part (14) having a second connecting portion (14B), the method comprising the steps of: - causing the first connecting portion and the second connecting portion to overlap, a through-hole (14B) of the second connecting portion opening onto the first connecting portion, - forming a protective layer (18) on the side wall (14B3) of the through-hole, - forming a seal (19A) between the protective layer and the first connecting portion, and - forming, by additive manufacturing using spray deposition of metal powder driven by a cold gas, a fastening element (20) which extends into the through-hole, is fastened to the first connecting portion and encloses the second connecting portion.

Classes IPC  ?

  • B29C 65/64 - Assemblage d'un élément en matière autre que plastique avec un élément en matière plastique, p. ex. à force
  • B22F 10/25 - Dépôt direct de particules métalliques, p. ex. dépôt direct de métal [DMD] ou mise en forme par laser [LENS]
  • B22F 7/08 - Fabrication de couches composites, de pièces ou d'objets à base de poudres métalliques, par frittage avec ou sans compactage de pièces ou objets composés de parties différentes, p. ex. pour former des outils à embouts rapportés avec une ou plusieurs parties non faites à partir de poudre
  • B33Y 10/00 - Procédés de fabrication additive
  • B33Y 80/00 - Produits obtenus par fabrication additive
  • F02K 9/00 - Moteurs-fusées, c.-à-d. ensembles fonctionnels portant à la fois le combustible et son oxydantLeur commande
  • B29K 105/06 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts

57.

STRUCTURE FOR ASSEMBLING A PIECE COMPRISING A FIRST METAL PART AND A SECOND PART MADE OF AN ORGANIC MATRIX COMPOSITE MATERIAL

      
Numéro d'application FR2021050811
Numéro de publication 2021/234244
Statut Délivré - en vigueur
Date de dépôt 2021-05-11
Date de publication 2021-11-25
Propriétaire
  • ARIANEGROUP SAS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Du Tertre, Alban
  • Guichard, Didier

Abrégé

The invention relates to a piece comprising a first metal part (12) and a second part (14) made of an organic matrix composite material, in which the first part (12) has a first connecting portion (12A) and the second part (14) has a second connecting portion (14A), the second connecting portion (14A) having at least one through-hole (14B), the second connecting portion (14A) being totally or partially sandwiched between the first connecting portion (12A) and a metal fastening element (16), the fastening element (16) being fixed to the first part (12), on the one hand, on the first connecting portion (12D) via the through-hole (14B) of the second connecting portion (14A) and, on the other hand, on a portion (12D) other than the first connecting portion (12A), whereby the first part (12) and the second part (14) are fixed to one another.

Classes IPC  ?

  • B29C 65/64 - Assemblage d'un élément en matière autre que plastique avec un élément en matière plastique, p. ex. à force
  • F02K 9/00 - Moteurs-fusées, c.-à-d. ensembles fonctionnels portant à la fois le combustible et son oxydantLeur commande
  • B22F 10/25 - Dépôt direct de particules métalliques, p. ex. dépôt direct de métal [DMD] ou mise en forme par laser [LENS]
  • B22F 7/08 - Fabrication de couches composites, de pièces ou d'objets à base de poudres métalliques, par frittage avec ou sans compactage de pièces ou objets composés de parties différentes, p. ex. pour former des outils à embouts rapportés avec une ou plusieurs parties non faites à partir de poudre
  • B33Y 80/00 - Produits obtenus par fabrication additive
  • B29K 105/06 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts

58.

IMPROVED DEPLOYMENT DEVICE FOR NANO-SATELLITE

      
Numéro d'application FR2021050818
Numéro de publication 2021/229178
Statut Délivré - en vigueur
Date de dépôt 2021-05-11
Date de publication 2021-11-18
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • MECANO I.D. (France)
Inventeur(s)
  • Deslandes, Olivier
  • Sicre, Jacques
  • Bonnes, Lionel

Abrégé

The invention relates to a deployment device (1) for a nano-satellite (5) comprising a main structure (2) mounted on a launcher, a support frame (3) carrying the nano-satellite (5), a locking/unlocking structure (4), the deployment device (1) being characterised in that the locking/unlocking structure (4) comprises a first clamping element (41) complementary to a second clamping element (42) of the support frame (3), and an actuating element (43) that is elastically deformable such that: in a locked position, it constrains the first clamping element (41) against the second clamping element (42) in order to hold the support frame (3) to the main structure (2) and, in an unlocked position, it releases the first clamping element (41) from the second clamping element (42) so as to release the support frame (3) from the main structure (2) in order for it to be ejected.

Classes IPC  ?

  • B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage

59.

RADIOFREQUENCY ANTENNA FOR A SATELLITE

      
Numéro d'application FR2021050762
Numéro de publication 2021/224572
Statut Délivré - en vigueur
Date de dépôt 2021-05-03
Date de publication 2021-11-11
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Sodki, Mehdi
  • Blanc, Ornella

Abrégé

The present invention relates to a radiofrequency antenna (1) which is adapted to be mounted on a spacecraft, wherein the antenna (1) comprises four helical strands (10) of a superelastic shape memory alloy and is configured to move from a deployed configuration to a constrained stacking configuration and to return autonomously to the deployed configuration.

Classes IPC  ?

  • H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
  • H01Q 1/36 - Forme structurale pour éléments rayonnants, p. ex. cône, spirale, parapluie
  • H01Q 11/08 - Antennes hélicoïdales

60.

LOW-SHOCK AND REUSABLE RETENTION AND RELEASE DEVICE

      
Numéro d'application FR2021050668
Numéro de publication 2021/209724
Statut Délivré - en vigueur
Date de dépôt 2021-04-15
Date de publication 2021-10-21
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Sicre, Jacques

Abrégé

A device (1, 1', 1'') for retaining and releasing a bar (2, 2''), the device (1, 1', 1'') comprising a clamping component (3, 3'), a retaining and releasing component (4) and at least one unclamping component (5, 5'), the retaining and releasing component (4) comprising a plurality of segments (41, 42, 43, 44, 41', 42', 43', 44', 41'', 42''), each comprising a first bearing surface (71, 72) configured to bear on part of the bar (2) when the plurality of segments (41, 42, 43, 44, 41', 42', 43', 44', 41'', 42'') is in a retention configuration under the effect of a clamping pressure generated by the clamping component (3, 3'), the plurality of segments (41, 42, 43, 44, 41', 42', 43', 44', 41'', 42'') comprising a second bearing surface (8, 8') configured to bear on an end of the at least one unclamping component (5, 5'), the at least one unclamping component (5, 5') being produced from a first single effect shape memory material, with each end of the at least one unclamping component (5, 5') exerting an unclamping pressure compensating the clamping pressure, so as to place the retaining and releasing component (4) in a configuration in which the part of the arm (2, 2'') is released.

Classes IPC  ?

  • F16B 1/00 - Dispositifs pour assembler des éléments structuraux ou parties de machines ou bien pour empêcher tout mouvement relatif entre eux
  • B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage
  • B64G 1/22 - Parties de véhicules spatiaux ou équipements spécialement destinés à être fixés dans ou sur ces véhicules

61.

SAPPHIRE MICROREACTORS

      
Numéro d'application FR2021050604
Numéro de publication 2021/205115
Statut Délivré - en vigueur
Date de dépôt 2021-04-07
Date de publication 2021-10-14
Propriétaire
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Marre, Samuel
  • Lecoutre, Carole
  • Garrabos, Yves
  • Fauveau, Cyrielle
  • Cario, Anaïs
  • Nguyen, Olivier

Abrégé

The present invention concerns the field of microreaction devices and of micro-process engineering. It particularly involves devices having micro-channels (internal chambers with micrometric to submicrometric dimensions) for conveying chemical or biochemical mixtures and/or reactions. More specifically, such devices are optimised to achieve high temperature and pressure stresses (i.e. 500°C and 500 bar). For observation and analysis purposes, the microreaction devices have a wide range of transparency in terms of wavelengths. The subject matter of the present invention relates to a microfluid or microreactor device made of transparent sapphire, preferably in the wavelength range ranging from 150 to 6500 nm, and to its manufacturing method and to its use.

Classes IPC  ?

  • B01J 19/00 - Procédés chimiques, physiques ou physico-chimiques en généralAppareils appropriés

62.

TANK FOR CRYOGENIC PROPELLANTS

      
Numéro d'application FR2021050266
Numéro de publication 2021/165607
Statut Délivré - en vigueur
Date de dépôt 2021-02-16
Date de publication 2021-08-26
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CMP COMPOSITES (France)
Inventeur(s)
  • Oswald, Jean
  • Benabes, Jérôme
  • Guerin, Yannick
  • Lavaud, Antoine

Abrégé

The invention relates to a composite tank (100) for receiving and storing a cryogenic propellant, the composite tank (100) comprising: a sealing envelope (1) delimiting a storage chamber for the cryogenic propellant, the sealing envelope (1) comprising a first composite material, and a reinforcement layer (2) configured to at least partially cover the sealing envelope (1), the reinforcement layer (2) comprising a second composite material.

Classes IPC  ?

  • F17C 1/16 - Récipients sous pression, p. ex. bouteilles de gaz, réservoirs de gaz, cartouches échangeables en matériaux plastiques

63.

TECH THE MOON

      
Numéro d'application 018533649
Statut Enregistrée
Date de dépôt 2021-08-17
Date d'enregistrement 2022-01-15
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Consultancy and providing of information in the field of business organisation and management in the aeronautical and space sector; Providing of consultancy and advice in the field of company strategy; Providing of information and advice relating to economic activities in the aeronautical and space fields; Conducting business; Business administration; Business management and organization consultancy; Computerized file management; Collection and systematic ordering of data in a central file; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Public relations services; Promotion and communication in the aeronautical and space fields, information agencies relating to commercial activities in the aeronautical and space fields; Providing research, Relating to economics, commercial purposes. Providing investment advice; Consultancy relating to financial subsidies; Financial consultancy relating to joint ventures; Providing of advice, information, consultancy and research relating to finance and investments. Providing of coaching and educational programmes, In relation to the following fields: Business growth, Management of business and Business development, In the aeronautical and space fields; Educational services, namely continuous training programmes in the field of business, business growth, business management, business development and start-up development accessible via the internet in the aeronautical and space fields; Educational services, namely the development, implementation and conducting of pedagogical programmes and conferences and the providing of instructional courses in the fields of business, business acceleration and investments in the aeronautical and space fields; Education, namely development, implementation, conducting of pedagogical programmes and conferences, as well as providing of instructional courses in the field of business and/or business growth, business management, business development in order to connect creators with other entrepreneurs, experts, advisors, alumni, investors, community leaders and companies for the growth of their company in the aeronautical and space fields; Training; Coaching [training]; Continuous training; Organisation of training; Training; Providing of training in the aeronautical and space fields; Computer-assisted training courses; Training; Provision of online training; Providing of training programmes; Arranging of training symposiums; Arranging and conducting of workshops [training]; Publishing of webpages featuring scientific information In relation to the following fields: Provision of teaching classes, Astronomy, technology, Aeronautics, Research relating to space technology. Scientific information services in the aeronautical and space fields; Providing technical advice relating to the aeronautical and space fields; Engineering research; Technological research relating to the aeronautical and space fields; Scientific research and analysis; Technical research projects and studies; Research in the field of physics; Scientific research and development; Industrial analysis and research services; Research to develop new products; Research and development relating to physics; Industrial research, testing and analysis; Provision of information relating to technological research; Research, development, analysis and consultancy in the field of engineering; Provision of information concerning research and technical project studies relating to the use of natural energy; Evaluations and research conducted by engineers; Design and development of computer hardware and software; Research and development of new products for others; Technical project studies, in particular in connection with aeronautics and space; Computer programming; Conversion of data or documents from physical to electronic media; Development of standards and standardisation means (engineering); Research and development of electronic and computer systems in the fields of computing and telecommunications for the aeronautics and space sectors; Technical research relating to the establishment of standards and standardisation; Standardisation, namely development (design) of technical standards for manufactured goods and for telecommunications; Research relating to quality control and performance evaluation; Professional scientific consultancy and development of technology projects not relating to business; Engineering (not for construction purposes); Design of graphics, drawings and text for formatting Web pages on the Internet; Testing of materials in a technical laboratory; Testing relating to adaptability, in the aeronautics and space sectors, of goods from the radar, optical, space engines and satellite navigation industries; Research in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology and geology, and testing relating to adaptability, in the space sector, of goods derived from this research; Development of global satellite navigation systems; Scientific research into core technologies; Research into the robotic exploration of other planets; Research into programmes for preparing for future launches of rockets, satellites and space shuttles; Research for the development of space technology; Scientific research for Earth observation, for human exploration and transport, for human travel into space or for space engineering; Research relating to space technology; Scientific services, Including tests for others, research missions and scientific coordination; Development of web pages for presenting scientific information in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology, geology and satellite technology research; Research for refining technologies and developing goods; Testing of materials in orbit; Research into the adaptability of different components in space; Computer rental.

64.

METHOD AND DEVICE FOR OPTICAL DETECTION

      
Numéro d'application FR2021050165
Numéro de publication 2021/156560
Statut Délivré - en vigueur
Date de dépôt 2021-01-29
Date de publication 2021-08-12
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Montel, Johan

Abrégé

Method (100) for optical detection of an object by an image sensor, the object and the image sensor being movable relative to each other, the image sensor being configured to receive a measurement of a movement speed of the sensor, which speed is measured in a frame of reference that is fixed relative to the object, the method comprising the following steps: defining (101) an area in an image plane of the sensor which comprises a central point; calculating a movement speed (102) from a virtual image point in the image plane, the virtual image point being a virtual image of a virtual object point formed on the image plane at the central point of the area, the movement speed being calculated on the basis of the movement speed of the image sensor; determining (103) an integration time which is an increasing function of the movement speed; acquiring (104) a raw image on the basis of the integration time; calculating a reference image (105) as a function of an estimated movement of the image point during the integration time; calculating a corrected image (106); selecting (107) pixels in the corrected image.

Classes IPC  ?

  • G01S 5/16 - Localisation par coordination de plusieurs déterminations de direction ou de ligne de positionLocalisation par coordination de plusieurs déterminations de distance utilisant des ondes électromagnétiques autres que les ondes radio
  • G06T 7/20 - Analyse du mouvement
  • G06T 7/70 - Détermination de la position ou de l'orientation des objets ou des caméras
  • G01S 3/786 - Systèmes pour déterminer une direction ou une déviation par rapport à une direction prédéterminée utilisant le réglage d'une orientation des caractéristiques de directivité d'un détecteur ou d'un système de détecteurs afin d'obtenir une valeur désirée du signal provenant de ce détecteur ou de ce système de détecteurs la valeur désirée étant maintenue automatiquement

65.

METHOD FOR MANUFACTURING A MULTI-MATERIAL PART BY ADDITIVE MANUFACTURING, USING THE TECHNIQUE OF POWDER BED SELECTIVE LASER MELTING OR SELECTIVE LASER SINTERING

      
Numéro de document 03165810
Statut En instance
Date de dépôt 2021-01-22
Date de disponibilité au public 2021-07-29
Propriétaire
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (CNRS) (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • UNIVERSITE PAUL SABATIER TOULOUSE III (France)
  • THALES (France)
Inventeur(s)
  • Veron, Frederic
  • Vendier, Olivier
  • Tailhades, Philippe
  • Baco-Carles, Valerie
  • Kiryukhina, Kateryna

Abrégé

The invention relates to a process for manufacturing a multi-material part by additive manufacturing, comprising the following steps: a) a step of providing a pre-treated metal powder comprising grains and an oxidized and porous layer on a surface of said grains; b) a selective laser powder-bed fusion step comprising implementation of steps i) and ii) as follows: i) a step of forming a layer from the pre-treated metal powder; ii) a step of melting by laser said layer, said melting step being carried out under a reactive atmosphere and comprising changing parameters of application of the laser so that at least a first region of said layer is converted so as to lower the electrical conductivity thereof, thus forming a dielectric, and so that at least a second region of said layer is densified without converting it, the at least a first region being formed when the parameters of application of the laser allow a first energy density to be applied to said first region and/or the laser beam to be kept for a first dwell time on said first region, the at least a second region being formed when the parameters of application of the laser allow a second energy density to be applied to said second region and/or the laser beam to be kept for a second dwell time on said second region, and the first energy density being higher than the second energy density and/or the first dwell time being longer than the second dwell time. The invention also relates to a part obtained using said process.

Classes IPC  ?

  • B22F 1/00 - Poudres métalliquesTraitement des poudres métalliques, p. ex. en vue de faciliter leur mise en œuvre ou d'améliorer leurs propriétés
  • B22F 3/105 - Frittage seul en utilisant un courant électrique, un rayonnement laser ou un plasma
  • B22F 3/11 - Fabrication de pièces ou d'objets poreux
  • B22F 7/06 - Fabrication de couches composites, de pièces ou d'objets à base de poudres métalliques, par frittage avec ou sans compactage de pièces ou objets composés de parties différentes, p. ex. pour former des outils à embouts rapportés
  • B22F 10/28 - Fusion sur lit de poudre, p. ex. fusion sélective par laser [FSL] ou fusion par faisceau d’électrons [EBM]
  • B22F 10/32 - Commande ou régulation des opérations de l’atmosphère, p. ex. de la composition ou de la pression dans une chambre de fabrication
  • B22F 10/34 - Commande ou régulation des opérations des caractéristiques de la poudre, p. ex. densité, oxydation ou fluidité
  • B22F 10/368 - Température ou gradient de température, p. ex. température du bassin de fusion
  • B22F 10/38 - Commande ou régulation des opérations pour obtenir des caractéristiques spécifiques du produit, p. ex. le lissage de la surface, la densité, la porosité ou des structures creuses
  • B33Y 10/00 - Procédés de fabrication additive
  • B33Y 40/10 - Prétraitement
  • B33Y 70/00 - Matériaux spécialement adaptés à la fabrication additive
  • B33Y 70/10 - Composites de différents types de matériaux, p. ex. mélanges de céramiques et de polymères ou mélanges de métaux et de biomatériaux
  • B33Y 80/00 - Produits obtenus par fabrication additive
  • C22C 29/12 - Alliages à base de carbures, oxydes, borures, nitrures ou siliciures, p. ex. cermets, ou d'autres composés métalliques, p. ex. oxynitrures, sulfures à base d'oxydes
  • C22C 29/16 - Alliages à base de carbures, oxydes, borures, nitrures ou siliciures, p. ex. cermets, ou d'autres composés métalliques, p. ex. oxynitrures, sulfures à base de nitrures

66.

METHOD FOR MANUFACTURING A MULTI-MATERIAL PART BY ADDITIVE MANUFACTURING, USING THE TECHNIQUE OF POWDER BED SELECTIVE LASER MELTING OR SELECTIVE LASER SINTERING

      
Numéro d'application EP2021051485
Numéro de publication 2021/148624
Statut Délivré - en vigueur
Date de dépôt 2021-01-22
Date de publication 2021-07-29
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • UNIVERSITE PAUL SABATIER TOULOUSE III (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Veron, Frédéric
  • Vendier, Olivier
  • Tailhades, Philippe
  • Baco-Carles, Valérie
  • Kiryukhina, Kateryna

Abrégé

The invention relates to a method for manufacturing a multi-material part by additive manufacturing, comprising the following steps: a) a step of providing a pretreated metal powder comprising grains and an oxidised and porous layer on the surface of the grains; b) a step of powder bed selective laser melting comprising the implementation of the following steps i) and ii): i) a step of forming a layer from the pretreated metal powder; ii) a step of laser melting of the layer, carried out in a reactive atmosphere and comprising the adaptation of application parameters of the laser in order to transform at least one first zone of the layer in such a way as to reduce its electrical conductivity, thus forming a dielectric, and in order to densify at least one second zone of the layer without transforming it, the at least one first zone being formed when the application parameters of the laser allow a first energy density to be applied to the first zone and/or the laser beam to be held for a first hold time on the first zone, the at least one second zone being formed when the application parameters of the laser allow a second energy density to be applied to the second zone and/or the laser beam to be held for a second hold time on the second zone, and the first energy density being greater than the second energy density and/or the first hold time being greater than the second hold time. The invention also relates to a part obtained by this method.

Classes IPC  ?

  • B22F 3/105 - Frittage seul en utilisant un courant électrique, un rayonnement laser ou un plasma
  • B33Y 10/00 - Procédés de fabrication additive
  • B33Y 70/10 - Composites de différents types de matériaux, p. ex. mélanges de céramiques et de polymères ou mélanges de métaux et de biomatériaux
  • B33Y 70/00 - Matériaux spécialement adaptés à la fabrication additive
  • B33Y 80/00 - Produits obtenus par fabrication additive
  • B33Y 40/10 - Prétraitement
  • B22F 1/00 - Poudres métalliquesTraitement des poudres métalliques, p. ex. en vue de faciliter leur mise en œuvre ou d'améliorer leurs propriétés
  • B22F 1/02 - Traitement particulier des poudres métalliques, p.ex. en vue de faciliter leur mise en œuvre, d'améliorer leurs propriétés; Poudres métalliques en soi, p.ex. mélanges de particules de compositions différentes comportant un enrobage des particules
  • B22F 3/11 - Fabrication de pièces ou d'objets poreux
  • B22F 7/06 - Fabrication de couches composites, de pièces ou d'objets à base de poudres métalliques, par frittage avec ou sans compactage de pièces ou objets composés de parties différentes, p. ex. pour former des outils à embouts rapportés
  • C22C 1/04 - Fabrication des alliages non ferreux par métallurgie des poudres
  • C22C 1/10 - Alliages contenant des composants non métalliques
  • B22F 10/28 - Fusion sur lit de poudre, p. ex. fusion sélective par laser [FSL] ou fusion par faisceau d’électrons [EBM]
  • B22F 10/32 - Commande ou régulation des opérations de l’atmosphère, p. ex. de la composition ou de la pression dans une chambre de fabrication
  • B22F 10/34 - Commande ou régulation des opérations des caractéristiques de la poudre, p. ex. densité, oxydation ou fluidité
  • B22F 10/368 - Température ou gradient de température, p. ex. température du bassin de fusion
  • B22F 10/38 - Commande ou régulation des opérations pour obtenir des caractéristiques spécifiques du produit, p. ex. le lissage de la surface, la densité, la porosité ou des structures creuses
  • C22C 29/12 - Alliages à base de carbures, oxydes, borures, nitrures ou siliciures, p. ex. cermets, ou d'autres composés métalliques, p. ex. oxynitrures, sulfures à base d'oxydes
  • C22C 29/16 - Alliages à base de carbures, oxydes, borures, nitrures ou siliciures, p. ex. cermets, ou d'autres composés métalliques, p. ex. oxynitrures, sulfures à base de nitrures

67.

TECH THE MOON

      
Numéro d'application 018498165
Statut Enregistrée
Date de dépôt 2021-06-21
Date d'enregistrement 2021-12-30
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Consultancy and Providing of information, in relation to the following fields: Business organisation and Business management, In the aeronautical and space sector; Providing of consultancy and advice in the field of company strategy; Providing of information and advice relating to economic activities in the aeronautical and space fields; Conducting business; Business administration; Business management and organization consultancy; Computerized file management; Collection and systematic ordering of data in a central file; Organization of exhibitions for commercial or advertising purposes; Online advertising on a computer network; Public relations services; Promotion and communication in the aeronautical and space fields, information agencies relating to commercial activities in the aeronautical and space fields; Providing research, Relating to economics, commercial purposes. Providing investment advice; Consultancy relating to financial subsidies; Financial consultancy relating to joint ventures; Providing of advice, information, consultancy and research relating to finance and investments. Providing of coaching and educational programmes, In relation to the following fields: Business growth, Management of business and Business development, In the aeronautical and space fields; Educational services, namely continuous training programmes in the field of business, business growth, business management, business development and start-up development accessible via the internet in the aeronautical and space fields; Educational services, namely the development, implementation and conducting of pedagogical programmes and conferences and the providing of instructional courses in the fields of business, business acceleration and investments in the aeronautical and space fields; Educational services, namely the development, implementation and conducting of pedagogical programmes and conferences, as well as the providing of instructional courses in the field of business and/or business growth, business management, business development with the purpose of connecting creators with other entrepreneurs, experts, advisors, alumni, investors, community leaders and companies for the growth of their company in the aeronautical and space fields. Scientific information services in the aeronautical and space fields; Providing technical advice relating to the aeronautical and space fields; Engineering research; Technological research relating to the aeronautical and space fields; Scientific research and analysis; Technical research projects and studies; Research in the field of physics; Scientific research and development; Industrial analysis and research services; Research to develop new products; Research and development relating to physics; Industrial research, testing and analysis; Provision of information relating to technological research; Research, development, analysis and consultancy in the field of engineering; Provision of information concerning research and technical project studies relating to the use of natural energy; Evaluations and research conducted by engineers; Design and development of computer hardware and software; Research and development of new products for others; Technical project studies, in particular in connection with aeronautics and space; Computer programming; Conversion of data or documents from physical to electronic media; Development of standards and standardisation means (engineering); Research and development of electronic and computer systems in the fields of computing and telecommunications for the aeronautics and space sectors; Technical research relating to the establishment of standards and standardisation; Standardisation, namely development (design) of technical standards for manufactured goods and for telecommunications; Research relating to quality control and performance evaluation; Professional scientific consultancy and development of technology projects not relating to business; Engineering (not for construction purposes); Design of graphics, drawings and text for formatting Web pages on the Internet; Testing of materials in a technical laboratory; Testing relating to adaptability, in the aeronautics and space sectors, of goods from the radar, optical, space engines and satellite navigation industries; Research in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology and geology, and testing relating to adaptability, in the space sector, of goods derived from this research; Development of global satellite navigation systems; Scientific research into core technologies; Research into the robotic exploration of other planets; Research into programmes for preparing for future launches of rockets, satellites and space shuttles; Research for the development of space technology; Scientific research for Earth observation, for human exploration and transport, for human travel into space or for space engineering; Research relating to space technology; Scientific services, Including tests for others, research missions and scientific coordination; Development of web pages for presenting scientific information in the fields of science, astronomy, technology, aeronautics, oceanography, meteorology, geology and satellite technology research; Research for refining technologies and developing goods; Testing of materials in orbit; Research into the adaptability of different components in space; Computer rental.

68.

Method and device for measuring atmospheric parameters to estimate the quality of the air and the climate variables

      
Numéro d'application 17185353
Numéro de brevet 11885787
Statut Délivré - en vigueur
Date de dépôt 2021-02-25
Date de la première publication 2021-06-17
Date d'octroi 2024-01-30
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Pequignot, Eric

Abrégé

The present disclosure relates to a method and a device for measuring at least one atmospheric parameter (gas, temperature). The method includes implementing steps of acquiring spectral images in the ultraviolet and/or the visible and/or the infrared range and scanning according to a tomographic principle. The spectral images are acquired using a network of optical systems such as infrared cameras, and are used to estimate the air quality and/or meteorological and/or climate parameters in a geographic area, for example an urban agglomeration.

Classes IPC  ?

  • G01N 33/00 - Recherche ou analyse des matériaux par des méthodes spécifiques non couvertes par les groupes
  • G01N 15/06 - Recherche de la concentration des suspensions de particules
  • G01N 21/31 - CouleurPropriétés spectrales, c.-à-d. comparaison de l'effet du matériau sur la lumière pour plusieurs longueurs d'ondes ou plusieurs bandes de longueurs d'ondes différentes en recherchant l'effet relatif du matériau pour les longueurs d'ondes caractéristiques d'éléments ou de molécules spécifiques, p. ex. spectrométrie d'absorption atomique
  • G01W 1/06 - Instruments pour indiquer des conditions atmosphériques par mesure de plusieurs variables, p. ex. humidité, pression, température, nébulosité ou vitesse du vent donnant l'indication des conditions météorologiques par combinaison des variables mesurées
  • G01N 21/17 - Systèmes dans lesquels la lumière incidente est modifiée suivant les propriétés du matériau examiné

69.

METHOD FOR VIRTUAL SURVEILLANCE OF AT LEAST ONE MOVABLE OBJECT

      
Numéro d'application FR2020052323
Numéro de publication 2021/116583
Statut Délivré - en vigueur
Date de dépôt 2020-12-07
Date de publication 2021-06-17
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Marmet, François-Xavier

Abrégé

Method for virtual surveillance of at least one movable object, the method being carried out by a surveillance unit and comprising, for each of the one or more movable objects, a step (12) of receiving virtual surveillance parameters from a surveillance unit, a step (14) of receiving a current position of the movable object from any one of the surveillance or monitoring units and a step (16) of establishing a virtual authorised zone which is attached to the movable object and defined on a virtual map in accordance with the virtual surveillance parameters, the virtual authorised zone comprising the current position. The method also comprises a step (20) of receiving data concerning the movement of the movable object from any one of the surveillance or monitoring units and finally a step (22) of modifying the virtual authorised zone.

Classes IPC  ?

  • H04W 12/08 - Sécurité d'accès
  • H04W 12/64 - Sécurité dépendant du contexte dépendant de la localisationSécurité dépendant du contexte dépendant de la proximité utilisant des zones géorepérées
  • H04W 4/021 - Services concernant des domaines particuliers, p. ex. services de points d’intérêt, services sur place ou géorepères
  • G08B 21/02 - Alarmes pour assurer la sécurité des personnes

70.

Method for demodulating digital signals using multiple digital demodulators

      
Numéro d'application 17254696
Numéro de brevet 11343127
Statut Délivré - en vigueur
Date de dépôt 2019-06-21
Date de la première publication 2021-06-10
Date d'octroi 2022-05-24
Propriétaire
  • SAFRAN DATA SYSTEMS (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Thomas, Alain
  • Leveau, Jean-Marc
  • Augarde, Stanislas
  • Bouisson, Emmanuel
  • Gay, Adrien

Abrégé

Method for processing a sequence of digital signal samples including a first sub-sequence and a second sub-sequence. Forming a first block of samples comprising the first sub-sequence and a second block of samples comprising header samples followed by the second sub-sequence. Demodulating the first block of samples through a digital demodulator to produce a first block of symbols, and the second block of digital signal samples through a second digital demodulator to produce a second block of symbols. The second demodulator implementing a carrier synchronisation or symbol rate synchronisation starting with the header samples, which comprise samples in a number adapted in such a way that the synchronisation is effective before the second demodulator demodulates the second sub-sequence. Reconstructing a sequence of symbols by concatenating the first symbol block with the second symbol block.

Classes IPC  ?

  • H04L 27/233 - Circuits de démodulationCircuits récepteurs utilisant une démodulation non cohérente
  • H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
  • H04L 7/06 - Commande de vitesse ou de phase au moyen de signaux de synchronisation les signaux de synchronisation différant des signaux d'information en amplitude, polarité ou fréquence
  • H04B 1/30 - Circuits pour récepteurs homodynes ou synchrodynes

71.

Tunable microwave system

      
Numéro d'application 17254496
Numéro de brevet 11335985
Statut Délivré - en vigueur
Date de dépôt 2019-06-17
Date de la première publication 2021-06-03
Date d'octroi 2022-05-17
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Pacaud, Damien
  • Laplanche, Etienne
  • Verdeyme, Serge
  • Tantot, Olivier
  • Delhote, Nicolas
  • Bila, Stéphane
  • Perigaud, Aurélien
  • Carpentier, Ludovic

Abrégé

A tunable microwave system includes at least two elements, each element being chosen from a propagating guide, an evanescent guide, a resonator, and at least one coupling device arranged between the two elements and configured to couple the two elements to each other, the coupling device having a holder having an aperture and having at least one elongate element the shape of which is elongate in a polarization direction contained in a plane of the aperture, the elongate element being securely fastened to the perimeter of the aperture at at least one end, the coupling device being configured to be rotatable about an axis substantially perpendicular to the plane of the aperture so as to modify a value of the polarization direction and so that the coupling between the two elements is dependent on the value of the polarization direction.

Classes IPC  ?

  • H01P 1/165 - Dispositifs auxiliaires pour faire tourner le plan de polarisation
  • H01P 1/17 - Dispositifs auxiliaires pour faire tourner le plan de polarisation pour produire une rotation continue du plan de polarisation, p. ex. une polarisation circulaire
  • H01P 1/06 - Joints mobiles, p. ex. joints rotatifs
  • H01P 1/211 - Filtres du type moule à gaufresStructures crénelées
  • H01P 1/219 - Filtres à mode évanescent
  • H01P 1/12 - Dispositifs commutateurs ou interrupteurs utilisant un vibreur mécanique

72.

METHOD FOR REDUCING ERRORS ASSOCIATED WITH MULTIPLE PATHS

      
Numéro d'application FR2020052173
Numéro de publication 2021/105613
Statut Délivré - en vigueur
Date de dépôt 2020-11-25
Date de publication 2021-06-03
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Marmet, François-Xavier

Abrégé

A method for determining a corrected signal, allowing the errors associated with multiple paths to be reduced, said method comprising a step (12) of receiving a plurality of incident signals originating from a plurality of signal transmission units, such that each incident signal of the plurality of incident signals originates from a signal transmission unit of the plurality of signal transmission units and a step (14) of characterising at least one incident signal as a multiple path signal, a step (18) of determining a correction scale for each of the at least one multiple path type signals, as well as a step (22) of creating a correction table, and a step (24) of determining at least one corrected signal as a function of the correction table.

Classes IPC  ?

  • G01S 19/22 - Problèmes liés aux multitrajets
  • G01S 5/02 - Localisation par coordination de plusieurs déterminations de direction ou de ligne de positionLocalisation par coordination de plusieurs déterminations de distance utilisant les ondes radioélectriques

73.

AI4GEO

      
Numéro d'application 1592588
Statut Enregistrée
Date de dépôt 2021-03-03
Date d'enregistrement 2021-03-03
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 35 - Publicité; Affaires commerciales
  • 36 - Services financiers, assurances et affaires immobilières
  • 38 - Services de télécommunications
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Software (recorded programs); software for creating searchable databases; database and application integration software; apparatus for processing, transmission and storage of database information; all these goods intended for production of 3D geospatial information in an automatic way. Updating and maintenance of 3D geospatial data in computer databases; 3D geospatial data recording; compilation of 3D geospatial information in computer databases; systemization of 3D geospatial information in computer databases. Provision of financial information via computer databases and software packages. Provision of access to 3D geospatial databases; provision of access to online 3D geospatial databases; rental of access time to 3D geospatial databases; electronic exchange of data stored in 3D geospatial databases accessible via telecommunication networks. 3D geospatial database design; 3D geospatial computer database hosting; 3D geospatial computer database development; 3D geospatial database software installation and maintenance; 3D geospatial database software updating.

74.

Microwave waveguide comprising a cavity formed by layers having conductive surfaces and a dielectric strip disposed in the cavity

      
Numéro d'application 16768917
Numéro de brevet 11380972
Statut Délivré - en vigueur
Date de dépôt 2018-12-05
Date de la première publication 2021-05-20
Date d'octroi 2022-07-05
Propriétaire
  • UNIVERSITÉ DE BORDEAUX (France)
  • INSTITUT POLYTECHNIQUE DE BORDEAUX (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Ghiotto, Anthony
  • Parment, Frédéric

Abrégé

This microwave component (10) comprises a waveguide (12) comprising an upper layer, a lower layer, and a central layer (18) intermediate between the upper layer and the lower layer, said layers defining a zone (19) of propagation of an electromagnetic wave, the propagation zone (19) extending along a propagation axis, and comprising a cavity (32) bounded by the upper layer, the lower layer, and, laterally, by two opposite lateral edges (36) of the central layer (18). The waveguide (12) comprises at least one dielectric strip (28) placed in the propagation zone (19), the dielectric strip (28) being defined in one of the upper layer and the lower layer or being placed in the cavity (32) away from the lateral edges (36) of the cavity (32).

Classes IPC  ?

  • H01P 3/12 - Guides d'ondes creux
  • H01P 11/00 - Appareils ou procédés spécialement adaptés à la fabrication de guides d'ondes, résonateurs, lignes ou autres dispositifs du type guide d'ondes

75.

SOL-GEL METHOD FOR MANUFACTURING A PRECURSOR GEL, A XEROGEL AND A POWDER OF YTTRIUM-ALUMINUM GARNET AND USE THEREOF FOR FORMING ARTICLES

      
Numéro d'application FR2020052055
Numéro de publication 2021/094684
Statut Délivré - en vigueur
Date de dépôt 2020-11-10
Date de publication 2021-05-20
Propriétaire
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Rossignol, Sylvie
  • Vardelle, Michel
  • Rémondière, Fabien
  • Singlard, Marc
  • Oriol, Stéphane
  • Fiore, Giuseppe

Abrégé

One subject of the present invention relates to a sol-gel method for manufacturing a wet gel, a xerogel and a powder of yttrium-aluminum garnet. Another subject is an extrusion paste comprising the abovementioned wet gel, xerogel or powder. The invention further relates to the use of a wet gel, a xerogel, a powder of yttrium-aluminum garnet or an extrusion paste comprising a wet gel, a xerogel or a powder of yttrium-aluminum garnet to manufacture an article, preferably by extrusion, microextrusion or filament deposition printing and also to said article.

Classes IPC  ?

  • C01F 17/34 - Aluminates, p. ex. YAlO3 ou Y3-xGdxAl5O12

76.

PROPULSION UNIT FOR ROCKET

      
Numéro d'application FR2020051713
Numéro de publication 2021/069814
Statut Délivré - en vigueur
Date de dépôt 2020-09-30
Date de publication 2021-04-15
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Girard, Nathalie
  • Labarthe, Emilie
  • Bonnal, Christophe
  • Masson, Frédéric

Abrégé

The invention relates to a propulsion unit (1) for a rocket, comprising a tank (2) designed to contain a propellant, an engine comprising a combustion chamber (3) configured to subject the propellant to combustion generating exhaust gases, a supply circuit (4) disposed between the propellant tank (2) and the combustion chamber (3) configured to supply the combustion chamber (3) with propellant and an exhaust gas circuit (8) disposed between the combustion chamber (3) and the propellant tank (2) configured to convey at least part of the exhaust gases from the combustion chamber (3) to the propellant tank (2) in order to pressurise it.

Classes IPC  ?

  • F02K 9/50 - Alimentation en propergols utilisant du fluide pressurisé pour mettre les propergols sous pression
  • F02K 9/46 - Alimentation en propergols utilisant des pompes
  • F02K 9/48 - Alimentation en propergols utilisant des pompes entraînées par une turbine à gaz, elle-même entraînée par les gaz de combustion des propergols
  • F02K 9/56 - Commande
  • F02K 9/60 - Parties de leur structureDétails non prévus ailleurs
  • F02K 9/97 - Tuyères de fusée

77.

METHOD FOR COVERING THE INNER SURFACE OF A TANK

      
Numéro d'application FR2020051786
Numéro de publication 2021/069848
Statut Délivré - en vigueur
Date de dépôt 2020-10-09
Date de publication 2021-04-15
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • CMP COMPOSITES (France)
Inventeur(s)
  • Lavaud, Antoine
  • Guelou, Yann

Abrégé

Method for covering the inner surface (2) of a tank (100), the method comprising the following steps: - a) providing a tank (100) made of a composite material, such as a thermoplastic material or a thermosetting material, the tank being configured to receive a pressurised fluid, - b) spraying a liquid composition (6) comprising a fluoropolymer, a prepolymer and a crosslinking agent of the prepolymer onto the inner surface (2) of the tank (100) so as to form a cover layer (7) covering the inner surface (2), and - c) polymerising the cover layer (7) so as to generate a polymeric binder encapsulating the fluoropolymer and form a fluorinated coating (8) covering at least part of the inner surface (2).

Classes IPC  ?

  • C08F 259/08 - Composés macromoléculaires obtenus par polymérisation de monomères sur des polymères de monomères contenant des halogènes tels que définis dans le groupe sur des polymères contenant du fluor
  • C09D 127/12 - Compositions de revêtement à base d'homopolymères ou de copolymères de composés possédant un ou plusieurs radicaux aliphatiques non saturés, chacun ne contenant qu'une seule liaison double carbone-carbone et l'un au moins étant terminé par un halogèneCompositions de revêtement à base de dérivés de tels polymères non modifiés par un post-traitement chimique contenant des atomes de fluor
  • C08F 299/00 - Composés macromoléculaires obtenus par des interréactions de polymères impliquant uniquement des réactions entre des liaisons non saturées carbone-carbone, en l'absence de monomères non macromoléculaires

78.

METHOD FOR DECREASING ERRORS RELATED TO MULTIPATH PROPAGATION OF A NOISY ACQUIRED SIGNAL

      
Numéro d'application FR2020051709
Numéro de publication 2021/064324
Statut Délivré - en vigueur
Date de dépôt 2020-09-30
Date de publication 2021-04-08
Propriétaire
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • M3 SYSTEMS (France)
Inventeur(s)
  • Marmet, François-Xavier
  • Robert, Thierry
  • Michel, Patrice
  • Jardak, Nabil

Abrégé

Method for decreasing errors related to multipath propagation of a noisy acquired signal, comprising a step of receiving a noisy signal comprising a known signature, a step of decomposing the noisy signal into wavelets, and a step of reconstructing a signal reconstructed from a combination of wavelets selected from the wavelets obtained in the decomposing step. The method also comprises a step of constructing an expected signal from the known signature, a step of estimating the similarity of the reconstructed signal to the expected signal, and a step of estimating the direct signal using the result of the step of estimating the similarity.

Classes IPC  ?

79.

ION PROPULSION DEVICE

      
Numéro d'application EP2020076418
Numéro de publication 2021/063750
Statut Délivré - en vigueur
Date de dépôt 2020-09-22
Date de publication 2021-04-08
Propriétaire
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • UNIVERSITE PARIS-SACLAY (France)
Inventeur(s)
  • Gierak, Jacques
  • Boniface, Claude
  • Lepesant, Mathieu

Abrégé

LLL of the insulating support (17) being chosen so as to maximize the number of emission modules (10) in the emission plane.

Classes IPC  ?

  • F03H 1/00 - Utilisation du plasma pour produire une poussée propulsive par réaction

80.

STAN TOOL

      
Numéro de série 90559899
Statut Enregistrée
Date de dépôt 2021-03-04
Date d'enregistrement 2022-02-15
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 41 - Éducation, divertissements, activités sportives et culturelles
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Downloadable scientific software specifically software for the analysis of transfer functions derived from electrical simulations conducted with other commercial simulation software; recorded computer software, namely, recorded computer programs for extracting, analyzing and viewing data in the field of space exploration, earth observation and aerospace, as well as recorded computer software for use in database and image management and in data and image processing in the field of space activity and earth observation; downloadable computer programs intended to analyze the stability of designs of analogic and/or digital electronic circuits as well as downloadable computer programs for use in computer-aided design of electronic functions in the field of industry, science and research Educational services, namely, providing of training, especially in the field of methods and analysis of the stability of electronic circuits as well as and training in the development of scientific software Research services in the field of analysis of stability of electronic circuits and microwaves and detection of instabilities of electronic circuits and microwaves

81.

Self-assisted fast acquisition and first fix for a standalone GNSS receiver

      
Numéro d'application 16964033
Numéro de brevet 11846713
Statut Délivré - en vigueur
Date de dépôt 2019-01-17
Date de la première publication 2021-02-18
Date d'octroi 2023-12-19
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Marmet, François-Xavier

Abrégé

A Global Navigation Satellite System (GNSS) positioning techniques is provided. A method to improve the time required to compute a position measurement in a GNSS receiver, and the time required to make this position measurement accurate is also provided. The method comprises computing a snapshot PVT (Position Velocity and Time) measurement, and use it to reduce the time required to acquire new signals to compute a conventional PVT measurement. A receiver implementing the method is further provided.

Classes IPC  ?

  • G01S 19/24 - Acquisition ou poursuite des signaux émis par le système
  • G01S 19/25 - Acquisition ou poursuite des signaux émis par le système faisant intervenir des données d'assistance reçues en provenance d'un élément coopérant, p. ex. un GPS assisté

82.

CRYOGENIC COOLER FOR A RADIATION DETECTOR, PARTICULARLY IN A SPACECRAFT

      
Numéro d'application FR2020051123
Numéro de publication 2020/260842
Statut Délivré - en vigueur
Date de dépôt 2020-06-26
Date de publication 2020-12-30
Propriétaire
  • L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L’EXPLOITATION DES PROCEDES GEORGES CLAUDE (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Butterworth, James
  • Chassaing, Clément

Abrégé

The invention mainly relates to a cryogenic cooler comprising a cold region, a heat-transfer fluid circuit, the cold region being positioned in the circuit, an application heat exchanger configured to exchange calories with a device to be cooled, characterised in that the cooler comprises at least one passive non-return valve fluidly connected to the cold region, the heat exchanger comprising at least one first fluid inlet positioned downstream of the non-return valve in the flow direction of the heat-transfer fluid, the heat-transfer fluid circulating from the end of the cold region.

Classes IPC  ?

  • F25B 9/14 - Machines, installations ou systèmes à compression dans lesquels le fluide frigorigène est l'air ou un autre gaz à point d'ébullition peu élevé caractérisés par le cycle utilisé, p. ex. cycle de Stirling
  • F25B 25/00 - Machines, installations ou systèmes utilisant une combinaison des principes de fonctionnement compris dans plusieurs des groupes
  • F25D 19/00 - Disposition ou montage des groupes frigorifiques dans les dispositifs

83.

SHAPE-MEMORY TUBULAR STRUCTURE

      
Numéro d'application FR2020050989
Numéro de publication 2020/249900
Statut Délivré - en vigueur
Date de dépôt 2020-06-10
Date de publication 2020-12-17
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Cadiergues, Laurent
  • Pagnoux, Hélène
  • Veaudecrenne, Ellen
  • Combes, Hélène

Abrégé

The application relates to a tubular composite structure (1) able to deploy by shape-memory effect and having two ends (3, 4), the tubular composite structure (1) able to deploy by shape-memory effect comprising a single heating jacket, formed of braided fibres made of a single electrically resistive material and impregnated with a shape-memory resin (110), and defining an interior space (200) circumscribed by the heating jacket (110), the braided fibres ensuring autonomous deployment of the tubular composite structure and providing structural integrity to the structure in the deployed position.

Classes IPC  ?

  • B29C 70/88 - Façonnage de matières composites, c.-à-d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p. ex. des inserts caractérisées principalement par des propriétés spécifiques, p. ex. électriquement conductrices ou renforcées localement
  • B29C 61/00 - Façonnage par libération de contraintes internesFabrication de préformes ayant des contraintes internesAppareils à cet effet
  • B29C 61/06 - Fabrication de préformes ayant des contraintes internes, p. ex. mémoire plastique
  • H01Q 1/08 - Moyens pour replier tout ou partie des antennes
  • B29C 61/04 - Dilatation thermique
  • H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
  • H01Q 1/14 - SupportsMoyens de montage pour des fils ou autres éléments rayonnants non rigides
  • B29K 105/08 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts de grande longueur, p. ex. ficelles, mèches, mats, tissus ou fils
  • B29L 31/30 - Véhicules, p. ex. bateaux ou avions, ou éléments de leur carrosserie
  • B29L 31/34 - Appareils électriques, p. ex. bougies ou leurs parties constitutives

84.

LDPC coding with differentiated protection

      
Numéro d'application 16897814
Numéro de brevet 11050439
Statut Délivré - en vigueur
Date de dépôt 2020-06-10
Date de la première publication 2020-12-17
Date d'octroi 2021-06-29
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
  • INSTITUT NATIONAL POLYTECHNIQUE DE TOULOUSE (France)
  • TESA TELECOM SPATIALES AERONAUTIQUES (France)
Inventeur(s)
  • Ortega Espluga, Lorenzo
  • Poulliat, Charly
  • Al Bitar, Hanaa
  • Boucheret, Marie-Laure
  • Aubault, Marion

Abrégé

A new unequal-error-protection method that is based on using a particular parity-check-matrix structure for LDPC codes.

Classes IPC  ?

  • G06F 11/00 - Détection d'erreursCorrection d'erreursContrôle de fonctionnement
  • G08C 25/00 - Dispositions pour prévenir ou corriger les erreursDispositions de contrôle
  • G06F 11/30 - Surveillance du fonctionnement
  • H03M 13/00 - Codage, décodage ou conversion de code pour détecter ou corriger des erreursHypothèses de base sur la théorie du codageLimites de codageMéthodes d'évaluation de la probabilité d'erreurModèles de canauxSimulation ou test des codes
  • H04L 1/00 - Dispositions pour détecter ou empêcher les erreurs dans l'information reçue
  • H03M 13/11 - Détection d'erreurs ou correction d'erreurs transmises par redondance dans la représentation des données, c.-à-d. mots de code contenant plus de chiffres que les mots source utilisant un codage par blocs, c.-à-d. un nombre prédéterminé de bits de contrôle ajouté à un nombre prédéterminé de bits d'information utilisant plusieurs bits de parité
  • H03M 13/29 - Codage, décodage ou conversion de code pour détecter ou corriger des erreursHypothèses de base sur la théorie du codageLimites de codageMéthodes d'évaluation de la probabilité d'erreurModèles de canauxSimulation ou test des codes combinant plusieurs codes ou structures de codes, p. ex. codes de produits, codes de produits généralisés, codes concaténés, codes interne et externe
  • H03M 13/35 - Protection inégale ou adaptative contre les erreurs, p. ex. en fournissant un niveau différent de protection selon le poids de l'information d'origine ou en adaptant le codage selon le changement des caractéristiques de la voie de transmission

85.

ABSOLUTE 720° INCLINOMETER ABLE TO OPERATE IN MICROGRAVITY

      
Numéro d'application FR2020050803
Numéro de publication 2020/234529
Statut Délivré - en vigueur
Date de dépôt 2020-05-14
Date de publication 2020-11-26
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Remetean, Emile

Abrégé

The present description relates to a device (7) for recognising the attitude of an object, characterized in that it comprises: a sphere (11) comprising a wall (13) able to let a light flux at least partially pass; a ball (17), moveably mounted inside said sphere (11); an image-acquiring device (19), arranged in said attitude-recognising device (7) to acquire a two-dimensional image of the ball (17) and of the sphere (11); a device (21) for emitting a light flux, arranged in said attitude-recognising device (7) to emit a light flux in the direction of said sphere (11); an image-processing device (23) that is connected to the image-acquiring device (19), controlled by an image-processing algorithm and designed to control the device (21) for emitting a light flux, with a view to collecting said image acquired by said image-acquiring device (19) and to determining, from said image (29), a gravity vector (G) having as origin the centre (Os) of the sphere (11) and as end the centre (OB) of the ball (17).

Classes IPC  ?

  • G01C 9/10 - Mesure de l'inclinaison, p. ex. par clinomètres, par niveaux en utilisant des objets roulants
  • G01C 9/06 - Moyens d'indication ou de lecture électriques ou photo-électriques
  • G01C 21/24 - NavigationInstruments de navigation non prévus dans les groupes spécialement adaptés pour la navigation des cosmonautes
  • B64G 1/10 - Satellites artificielsSystèmes de tels satellitesVéhicules interplanétaires
  • B64G 1/24 - Appareils de guidage ou de commande, p. ex. de commande d'assiette
  • B64G 1/66 - Aménagements ou adaptations d'appareils ou d'instruments, non prévus ailleurs

86.

Dynamic StreetView with view images enhancement

      
Numéro d'application 16958687
Numéro de brevet 12044543
Statut Délivré - en vigueur
Date de dépôt 2018-12-19
Date de la première publication 2020-10-29
Date d'octroi 2024-07-23
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Marmet, François-Xavier

Abrégé

A user computing device, method and computer program to display a view to the user are provided. The invention allows a user to display a number of different views with photorealistic rendering of how the view should look like at a view time, based solely on view position, and descriptors of the view. In an aspect, the invention deduces from view position and view time the view descriptors (weather parameters, traffic parameters . . . ); selects, in a collection of images, an image of the view based on view position; modifies the image to match descriptors of the view (for example, by adding a rain effect if the image in the collection is under sunshine and the view should be displayed under rain). Thus, the invention allows displaying photorealistic images of how a view should look like at any time.

Classes IPC  ?

  • G01C 21/36 - Dispositions d'entrée/sortie pour des calculateurs embarqués
  • G06F 16/29 - Bases de données d’informations géographiques
  • G06Q 30/0241 - Publicités

87.

Relay platform for transmitting positioning signals to rovers with an optimized radiation pattern

      
Numéro d'application 16958688
Numéro de brevet 11543536
Statut Délivré - en vigueur
Date de dépôt 2018-12-14
Date de la première publication 2020-10-29
Date d'octroi 2023-01-03
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Capet, Nicolas
  • Marmet, François-Xavier

Abrégé

An antenna assembly configured to transmit terrestrial positioning signals from a relay platform having a frame of reference, the transmit being in at least a first mode with a radiating pattern having at least a main lobe having a narrow aperture in a plane and a wide aperture in a plane. A relay platform comprising a receiver of a synchronization signal, a transmitter of positioning signals to an area of service comprising a number of rovers, and an antenna assembly configured to produce a radiating pattern adapted to transmit the positioning signals as a function of the environment of the relay platform and the rovers. In a number of embodiments the relay platforms may be organized in a network of platforms, possibly of masters and slaves that receive feed-back from the rovers in the AoS so as to optimize the configuration of the antenna elements dynamically to optimize the QoS of positioning based on a number of selected quality indexes.

Classes IPC  ?

  • H01Q 3/34 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante faisant varier la phase par des moyens électriques
  • G01S 19/11 - Éléments coopérantsInteraction ou communication entre les différents éléments coopérants ou entre les éléments coopérants et les récepteurs fournissant des signaux de positionnement supplémentaires dédiés les éléments coopérants étant des pseudolites ou des répétiteurs de signaux de systèmes de positionnement par satellite à radiophares
  • G01S 1/04 - Radiophares ou systèmes de balisage émettant des signaux ayant une ou des caractéristiques pouvant être détectées par des récepteurs non directionnels et définissant des directions, situations ou lignes de position déterminées par rapport aux émetteurs de radiophareRécepteurs travaillant avec ces systèmes utilisant les ondes radioélectriques Détails
  • H01Q 21/08 - Réseaux d'unités d'antennes, de même polarisation, excitées individuellement et espacées entre elles les unités étant espacées le long du trajet rectiligne ou adjacent à celui-ci
  • H01Q 25/04 - Antennes multimodes

88.

GNSS antenna add-on

      
Numéro d'application 16762924
Numéro de brevet 11313975
Statut Délivré - en vigueur
Date de dépôt 2018-11-14
Date de la première publication 2020-09-10
Date d'octroi 2022-04-26
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Capet, Nicolas
  • Marmet, François-Xavier

Abrégé

An add-on device configured to reduce the power level of reflected paths of GNSS signals reaching a GNSS receiver's antenna, the associated GNSS receiver set, some equipment embedding the add-on device, and the associated method to reduce the power level of reflected GNSS signals are provided. The GNSS signals are transmitted according to a first polarization, and the add-on device comprises a material configured to be transparent to the first polarization and to reflect GNSS signals polarized according to a second polarization orthogonal to the first polarization.

Classes IPC  ?

  • G01S 19/22 - Problèmes liés aux multitrajets
  • G01S 19/36 - Détails de construction ou détails de matériel ou de logiciel de la chaîne de traitement des signaux concernant l'étage d'entrée du récepteur

89.

COMMUNICATION SYSTEM COMPRISING A MATRIX IMAGE COMMUNICATION RECEIVER

      
Numéro d'application FR2019053236
Numéro de publication 2020/128386
Statut Délivré - en vigueur
Date de dépôt 2019-12-20
Date de publication 2020-06-25
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Lafuma, Pierre
  • Materne, Alex

Abrégé

The invention relates, inter alia, to a communication system (6) comprising a communication receiver (60) which is provided to receive a useful communication signal from a remote light emission source (61), characterised in that the communication receiver (60) is formed by a matrix image camera (60a1) having a field of view (C1), in which the light emission source (61) is contained, the camera (60a1) comprising a matrix detector (60a2).

Classes IPC  ?

  • H04B 10/118 - Dispositions spécifiques à la transmission en espace libre, c.-à-d. dans l’air ou le vide spécialement adaptées aux communications par satellite

90.

Radiofrequency RF rotating joint for rotary RF wave-guiding device and rotary RF device including such a joint

      
Numéro d'application 16696931
Numéro de brevet 11075436
Statut Délivré - en vigueur
Date de dépôt 2019-11-26
Date de la première publication 2020-06-18
Date d'octroi 2021-07-27
Propriétaire
  • THALES (France)
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Vynohradov, Dimitri
  • Brossier, Jérôme
  • Monteillet, Benjamin
  • Lorenzo, Jérôme
  • Ferrando, Nicolas

Abrégé

k).

Classes IPC  ?

  • H01P 3/123 - Guides d'ondes creux présentant une section complexe ou en forme d'échelons, p. ex. guides d'ondes striés ou rainurés
  • H01P 1/06 - Joints mobiles, p. ex. joints rotatifs
  • H01P 1/18 - Déphaseurs
  • H01P 5/18 - Dispositifs à accès conjugués, c.-à-d. dispositifs présentant au moins un accès découplé d'un autre accès consistant en deux guides couplés, p. ex. coupleurs directionnels
  • H01Q 13/06 - Terminaisons de guide d'onde
  • H01Q 21/06 - Réseaux d'unités d'antennes, de même polarisation, excitées individuellement et espacées entre elles

91.

RADIOFREQUENCY RF ROTATING JOINT FOR ROTARY RF WAVE-GUIDING DEVICE AND ROTARY RF DEVICE INCLUDING SUCH A JOINT

      
Numéro de document 03065566
Statut En instance
Date de dépôt 2019-12-18
Date de disponibilité au public 2020-06-18
Propriétaire
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • THALES (France)
Inventeur(s)
  • Vynohradov, Dimitri
  • Brossier, Jerome
  • Monteillet, Benjamin
  • Lorenzo, Jerome
  • Ferrando, Nicolas

Abrégé

An RF joint rotating about an axis of rotation (Z) comprises a number N, greater than or equal to 1, of RF transmission channels, a first, internal surface of symmetry of revolution about the axis (Z) and of RF transmission having a first, internal radius r1, and a second, external surface of symmetry of revolution about the axis (Z) and of RF transmission having a second, external radius r2, strictly less than said first, internal radius r1.The first and second RF transmission surfaces facing one another and rotationally mobile about the axis (Z) are configured through the first and second radii r1, r2, the geometry of the first and second RF access ports, and the geometry of the first and second RF containment and guidance means, such that:- each RF transmission channel Vi, i varying from 1 to N, comprises a first RF rotating waveguide, and- the N first RF rotating waveguides are distributed angularly over a predetermined number NC, greater than or equal to 1 and less than or equal to N, of sections of surfaces of revolution about the axis (Z) of the second RF transmission surface, each of the NC sections being situated along the longitudinal axis of symmetry (Z) at a predetermined different level L1(k).

Classes IPC  ?

  • H01P 1/06 - Joints mobiles, p. ex. joints rotatifs
  • H01P 1/161 - Sélecteurs de mode, p. ex. pour empêcher ou favoriser la propagation suivant un mode donnéConvertisseurs de mode fonctionnant selon deux modes orthogonaux indépendants, p. ex. transducteurs orthomodes
  • H01P 5/16 - Dispositifs à accès conjugués, c.-à-d. dispositifs présentant au moins un accès découplé d'un autre accès
  • H01Q 3/02 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne utilisant un mouvement mécanique de l'ensemble d'antenne ou du système d'antenne

92.

SOLID BOOSTER FOR A LAUNCHER

      
Numéro d'application FR2019052831
Numéro de publication 2020/115403
Statut Délivré - en vigueur
Date de dépôt 2019-11-28
Date de publication 2020-06-11
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Bonnal, Christophe

Abrégé

Solid booster (14) for a launcher, the booster being suitable for being separated from the rest of the launcher and comprising a wall (18) defining a combustion chamber (19) comprising an end, termed a front end (19a), and an opposite end, termed a rear end (19b), propellant (24) arranged in the combustion chamber, a combustion channel (26) passing through the combustion chamber from the front end toward the rear end, a nozzle (22) arranged at the rear end of the combustion chamber, an ignition (28) closing off the combustion channel at the front end of the combustion chamber, a skirt (20) covering the ignition at the front end of the combustion chamber, the skirt allowing the mechanical link with the rest of the launcher, and an ignition ejection system (34, 36, 38).

Classes IPC  ?

  • F02K 9/08 - Moteurs-fusées, c.-à-d. ensembles fonctionnels portant à la fois le combustible et son oxydantLeur commande utilisant des propergols solides
  • F02K 9/32 - Parties de leur structureDétails non prévus ailleurs
  • F02K 9/95 - Moteurs-fusées, c.-à-d. ensembles fonctionnels portant à la fois le combustible et son oxydantLeur commande caractérisés par des moyens ou des aménagements de démarrage ou d'allumage

93.

METHOD AND DEVICE FOR GENERATING AT LEAST ONE GNSS SIGNAL FOR TESTING A GNSS RECEIVER

      
Numéro d'application FR2019052248
Numéro de publication 2020/074803
Statut Délivré - en vigueur
Date de dépôt 2019-09-25
Date de publication 2020-04-16
Propriétaire
  • M3 SYSTEMS (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s)
  • Marmet, François-Xavier
  • Jardak, Nabil

Abrégé

Method (100) for generating at least one GNSS signal, the method comprising the following steps of: measurement (101) by a GNSS receiver (8) of a value of at least one parameter of a first GNSS signal (9) received by the GNSS receiver (8); fitting (102) of the value of the at least one parameter of the first GNSS signal (9), and/or determination (103) of another value of at least one other parameter, the at least one other parameter corresponding to at least one other simulated GNSS signal; generation (104) of at least one GNSS signal generated on the basis of the fitted value of the at least one parameter and/or generation of at least one other GNSS signal generated on the basis of the other value of the at least one other parameter.

Classes IPC  ?

  • G01S 19/03 - Éléments coopérantsInteraction ou communication entre les différents éléments coopérants ou entre les éléments coopérants et les récepteurs
  • G01S 19/23 - Test, contrôle, correction ou étalonnage d'un élément récepteur

94.

METHOD FOR THE ROBUST MONITORING OF AT LEAST ONE PARAMETER OF A GNSS SIGNAL

      
Numéro d'application FR2019052120
Numéro de publication 2020/058606
Statut Délivré - en vigueur
Date de dépôt 2019-09-12
Date de publication 2020-03-26
Propriétaire
  • M3 SYSTEMS (France)
  • CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
  • AIRBUS DEFENCE AND SPACE SAS (France)
Inventeur(s)
  • Marmet, François-Xavier
  • Jardak, Nabil

Abrégé

Method for the robust monitoring of at least one parameter of a GNSS signal Method for the monitoring of a GNSS signal, the method comprising steps of: replication of the carrier; integration, over an integration time period to generate an error signal; measurement of a signal-to-noise ratio; filtering of the first error signal with passband Bn; estimation of the frequency and/or of the phase of the carrier and of the phase of the PRN code; updating of the first control value as a function of the estimated frequency of the carrier, a first time interval separating two successive updates as a function of the estimated frequency, and of the estimated phase of the carrier, the first time interval being equal to the integration time period multiplied by a first variable number greater than or equal to 1, a first width of passband of the filtering step and the first variable number each being determined as a function of the signal-to-noise ratio and of the first filtered signal.

Classes IPC  ?

  • G01S 19/24 - Acquisition ou poursuite des signaux émis par le système

95.

METHOD AND DEVICE FOR MEASURING ATMOSPHERIC PARAMETERS TO ESTIMATE AIR QUALITY AND CLIMATE VARIABLES

      
Numéro de document 03109722
Statut En instance
Date de dépôt 2019-08-26
Date de disponibilité au public 2020-03-05
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Pequignot, Eric

Abrégé

The invention relates to a method and a device for measuring at least one atmospheric parameter (gas, temperature), implementing steps of acquiring spectral images in the ultraviolet and/or the visible and/or the infrared range and scanning according to a tomographic principle. The spectral images are acquired using a network of optical systems (1A-1D) such as infrared cameras, and are used to estimate the air quality and/or meteorological and/or climate parameters in a geographic area, for example an urban agglomeration.

Classes IPC  ?

  • G01N 21/17 - Systèmes dans lesquels la lumière incidente est modifiée suivant les propriétés du matériau examiné
  • G01N 21/31 - CouleurPropriétés spectrales, c.-à-d. comparaison de l'effet du matériau sur la lumière pour plusieurs longueurs d'ondes ou plusieurs bandes de longueurs d'ondes différentes en recherchant l'effet relatif du matériau pour les longueurs d'ondes caractéristiques d'éléments ou de molécules spécifiques, p. ex. spectrométrie d'absorption atomique
  • G01W 1/00 - Météorologie

96.

METHOD AND DEVICE FOR MEASURING ATMOSPHERIC PARAMETERS TO ESTIMATE AIR QUALITY AND CLIMATE VARIABLES

      
Numéro d'application FR2019051961
Numéro de publication 2020/043983
Statut Délivré - en vigueur
Date de dépôt 2019-08-26
Date de publication 2020-03-05
Propriétaire CENTRE NATIONAL D'ÉTUDES SPATIALES (France)
Inventeur(s) Pequignot, Eric

Abrégé

The invention relates to a method and a device for measuring at least one atmospheric parameter (gas, temperature), implementing steps of acquiring spectral images in the ultraviolet and/or the visible and/or the infrared range and scanning according to a tomographic principle. The spectral images are acquired using a network of optical systems (1A-1D) such as infrared cameras, and are used to estimate the air quality and/or meteorological and/or climate parameters in a geographic area, for example an urban agglomeration.

Classes IPC  ?

  • G01N 21/31 - CouleurPropriétés spectrales, c.-à-d. comparaison de l'effet du matériau sur la lumière pour plusieurs longueurs d'ondes ou plusieurs bandes de longueurs d'ondes différentes en recherchant l'effet relatif du matériau pour les longueurs d'ondes caractéristiques d'éléments ou de molécules spécifiques, p. ex. spectrométrie d'absorption atomique
  • G01W 1/00 - Météorologie
  • G01N 21/17 - Systèmes dans lesquels la lumière incidente est modifiée suivant les propriétés du matériau examiné

97.

GNSS receiver with a capability to resolve ambiguities using an uncombined formulation

      
Numéro d'application 15738926
Numéro de brevet 10739471
Statut Délivré - en vigueur
Date de dépôt 2016-06-22
Date de la première publication 2020-02-06
Date d'octroi 2020-08-11
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Laurichesse, Denis

Abrégé

The invention discloses a receiver and a method to process navigation signals from one or more GNSS constellation, wherein an observation model and a measurement model allow a direct calculation of the carrier phase ambiguities. More specifically, in a triple frequency implementation, the receiver calculates in turn the extrawidelane, widelane and narrowlane ambiguities. The code and carrier phase biases can also be directly calculated. Thanks to the invention a quicker acquisition and tracking of a precise position, which will also be less noisy than a prior art solution, especially in some embodiments of the invention using a RAIM and/or a gap-bridging function. Also, code smoothing using the Doppler and low latency clock synchronization allow to decrease the noise levels of the precise point navigation solutions.

Classes IPC  ?

  • G01S 19/44 - Résolution de l'ambiguïté de la phase de la porteuseAmbiguïté flottanteProcédé LAMBDA [compensation par les moindres carrés de la décorrélation de l'ambiguïté]
  • G01S 19/02 - Détails des installations de contrôle terrestres ou spatiales
  • G01S 19/25 - Acquisition ou poursuite des signaux émis par le système faisant intervenir des données d'assistance reçues en provenance d'un élément coopérant, p. ex. un GPS assisté
  • G01S 19/29 - Acquisition ou poursuite des signaux émis par le système lié à la porteuse
  • G01S 19/32 - Fonctionnement multimode dans un seul et même système par satellite, p. ex. GPS L1/L2

98.

Multipath management in global navigation satellite systems

      
Numéro d'application 16472152
Numéro de brevet 11150355
Statut Délivré - en vigueur
Date de dépôt 2017-12-22
Date de la première publication 2020-01-16
Date d'octroi 2021-10-19
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s)
  • Marmet, François-Xavier
  • Rouch, Cédric

Abrégé

A device for handling multipath of a G.N.S.S. signal, is configured to: determine a spatial position, a clock time and measured multipath parameters comprising a relative delay and relative amplitude; communicate to a remote server the spatial position, clock time and multipath parameters; and receive processed multipath parameters as determined by the remote server. Systems comprising a plurality of such devices and their variants are described. Further aspects are described, in particular the exclusion of one or more satellites, the use of threshold schemes, pull/push modes, configurable refresh rates, quantization of positions, activation of additional sensors, filtering options, determination of merit factors for example as a function of the number of satellites in view and/or of signal-to-noise ratio, peer-to-peer schemes, as well as graphical display, audible sound or haptic feedbacks.

Classes IPC  ?

  • G01S 19/22 - Problèmes liés aux multitrajets
  • G01S 19/11 - Éléments coopérantsInteraction ou communication entre les différents éléments coopérants ou entre les éléments coopérants et les récepteurs fournissant des signaux de positionnement supplémentaires dédiés les éléments coopérants étant des pseudolites ou des répétiteurs de signaux de systèmes de positionnement par satellite à radiophares
  • G01S 19/34 - Consommation électrique
  • G01S 19/36 - Détails de construction ou détails de matériel ou de logiciel de la chaîne de traitement des signaux concernant l'étage d'entrée du récepteur

99.

FREQUENCY TRANSPOSITION DEVICE AND CORRESPONDING FREQUENCY TRANSPOSITION METHOD

      
Numéro d'application EP2019067088
Numéro de publication 2020/007691
Statut Délivré - en vigueur
Date de dépôt 2019-06-26
Date de publication 2020-01-09
Propriétaire
  • CENTRE NATIONAL D'ETUDES SPATIALES (France)
  • INSTITUT NATIONAL POLYTECHNIQUE DE TOULOUSE (France)
  • CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventeur(s)
  • Sombrin, Jacques
  • Armengaud, Vincent
  • Prigent, Gaëtan
  • Bernal, Olivier
  • Marchal, Timothée

Abrégé

The invention relates to a device for the frequency transposition of an input signal centred on a frequency (f1) to an output signal centred on a frequency (f2). Such a device comprises a module for averaging the input signal delivering a set of N first intermediate signals. A first intermediate signal of index (i), where i is a whole number from 1 to N, is a function of an i-th sliding average of the input signal over an i-th first time window of the form [(i-1)/(N*f1); i/(N*f1)] periodised at the frequency (f1). The device also comprises a module for reconstructing the output signal by temporal concatenation of N second intermediate signals windowed in second successive time windows. A second intermediate signal of index (k), where k is a whole number from 1 to N, is obtained from a windowing of the first intermediate signal of index (k) in a k-th second time window of the form [(k-1)/(N*f2); k/(N*f2)] periodised at the frequence (f2).

Classes IPC  ?

  • H03D 9/00 - Démodulation ou transfert de modulation d'ondes électromagnétiques modulées
  • H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission

100.

Method for analyzing a coupled vehicle/passenger system

      
Numéro d'application 16570277
Numéro de brevet 11577860
Statut Délivré - en vigueur
Date de dépôt 2019-09-13
Date de la première publication 2020-01-02
Date d'octroi 2023-02-14
Propriétaire CENTRE NATIONAL D'ETUDES SPATIALES (France)
Inventeur(s) Gonidou, Luc-Olivier

Abrégé

x′ relative to the new passenger.

Classes IPC  ?

  • B64G 1/38 - Amortissement des oscillations, p. ex. amortisseurs de nutation
  • B64G 1/60 - Installations à l'usage de l'équipage ou des passagers
  • B64G 1/64 - Systèmes pour réunir ou séparer des véhicules spatiaux ou des parties de ceux-ci, p. ex. aménagement pour l'accostage ou l'amarrage
  • G06F 17/16 - Calcul de matrice ou de vecteur
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