The invention relates to a system (1) for ejectably attaching a device (2) to a support structure (3), the system comprising an attachment body (4), a movable plunger (12), a displacement device (16) and a plurality of locking elements (22) on which the plunger (12) is configured to act, wherein the system (1) is configured to consecutively adopt a locked configuration in which the plunger (12) acts on the locking elements (22) to secure the device (2) to the support structure (3), an unlocked configuration in which the plunger (12) is moved by the displacement device (16) to release the locking elements (22) and an ejection configuration in which the plunger (12) continues to be moved by the displacement device (16) so as to exert a force on the device (2) in order to eject it from the support structure (3), and wherein the system (1) thus enables the unlocking and ejection of the device (2) in a sequenced, reliable and secure manner.
F41F 3/065 - Nacelles lance-roquettes, c.-à-d. conteneurs amovibles pour lancer plusieurs roquettes
B64D 1/06 - Mécanismes de largage des bombesTrappes de la soute à bombes
F42B 15/36 - Moyens de liaison entre le moteur-fusée et le corps d'une roquetteRaccords pour relier les différents étages d'une roquetteMoyens de désassemblage
(1) Missiles et systèmes d'armes correspondant, à l'exclusion des fusils (armes) et leurs munitions; aucun de ces produits n'étant lié/destiné au domaine aérospatial.
The invention relates to a separable connection device, in particular for a flying craft and/or spacecraft. The connection device (1), which is simple, compact and lightweight, comprises a connecting pin (4) for holding two parts (2, 3) together and separating them, a movable plunger (17) arranged in the connecting pin (4) and a pressure generator (34), the connection device (1) being able to adopt a locked configuration in which the plunger (17) acts on locking elements (25), the connecting pin (4) exerting a force on the parts (2, 3) by pressing them against each other, an unlocked configuration in which the plunger (17), moved by a pressure generated by the pressure generator (34) in a first chamber, releases the locking elements (25) unlocking the connecting pin (4) and releasing the two parts (2, 3), and a separation configuration in which the plunger (17), moved by the pressure, opens a passage (43) between the first chamber and a second chamber, thereby allowing the pressure generated by the pressure generator (34) to be transferred thereto, the connecting pin (4) being moved by this pressure until an impact is generated on a stop of one of the parts (2, 3) so as to initiate the separation thereof.
F16B 21/16 - Dispositifs sans filetage pour empêcher le mouvement relatif selon l'axe d'une broche, d'un ergot, d'un arbre ou d'une pièce analogue par rapport à l'organe qui l'entoureFixations à ergots et douilles largables sans filetage à parties séparées par gorges ou encoches pratiquées dans l'axe ou l'arbre
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
F16B 19/10 - Rivets creuxRivets en plusieurs morceaux fixés par action mécanique
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Tablet computers, electronic interfaces, calculators,
software, artificial intelligence software for supporting
decision-making for missile operators and particularly with
respect to automatic target detection, recognition and
identification, trajectory calculation; data processing
apparatus and systems, namely, systems for control,
coordination, monitoring, detection, identification of
targets; radar apparatus; pursuit radars; electronic
scanning radars for detecting targets; radar detectors;
electro-optical apparatus for tracking, classifying and the
function of inhibiting directional radio frequency signals;
electronic control, observation, tracking and monitoring
systems and apparatus; sensors, electronic sensors; sensors;
smart effector and sensor assemblies; electronic and
optoelectronic apparatus for processing, receiving,
transferring data and image flows; electronic apparatus for
remote control of signals; all the aforesaid goods designed
for the detection, identification, tracking and
neutralization of military targets. Drones for military and civilian use; drones; military
observation drones; remotely controlled aircraft. Missiles and weapon systems therefor; anti-tank missiles;
interceptor weapon systems, namely effectors, consisting of
missiles, fire control and puruit radars, launching systems
on land vehicles, in silos, or integrated into a boat;
launchers for projectiles; cannons; shooting platforms
[weapons]; remotely operated ammunition.
The device determines, by means of a processing unit, an engagement plan for an air defence system (2) comprising munitions (Mj) fired from launchers (4), the processing unit determining the engagement plan by implementing an auction algorithm that takes into account, on the one hand, the number of munitions (Mj) of the launcher (4), which is a first constraint relating to the munitions (Mj) of the launcher (4), and, on the other hand, a number of firing dates in availability windows, which is a second constraint relating to the firing dates, the engagement plan comprising, for each target (Ci), allocation, on the one hand, of a particular munition (Mj) of a particular launcher (4) and, on the other hand, of a firing date of this munition (Mj), this allocation meeting said first and second constraints.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Tablet computers, Electronic interfaces, Calculating machines, Software, Artificial intelligence software for decision-making support to missile operators, and in particular relating to support in the automatic detection, recognition and identification of targets, path calculation; Data processing apparatus and Data processing systems, namely Target command, coordination, control, detection, identification systems; Radar apparatus; Tracking radars; electronic-scanning radar for target detection; Radar detectors; electro-optical apparatus for tracking, classification and directional radio frequency (RF) inhibition capability; electronic control, observation, monitoring and checking systems and apparatus; Sensors, electronic sensors; Sensors; smart-sensor and effector package; Electronic and optoelectronic apparatus for the processing, reception and transfer of data and Electronic and optoelectronic apparatus for the processing, reception and transfer of image flows; Electronic apparatus for the remote control of signals; all the aforesaid goods in relation to the following fields: Detection, identification, tracking and disposal of military targets. Military and civilian drones; Drones; Military observation drones; remotely operated aircrafts. Missiles and corresponding weapon systems; Anti-tank missiles; Weapon interception systems, namely effectors, comprising missiles, fire control and tracking radars, launching systems on land vehicles, in silos or integrated in boats; Launchers for projectiles; Cannons; Firing platforms [weapons]; Remote-operated ammunition.
11.
SIMULATOR AND SIMULATION METHOD WITH INCREASED PRECISION, IN PARTICULAR A WEAPON SYSTEM SIMULATOR, AND WEAPON SYSTEM PROVIDED WITH SUCH A SIMULATOR
Disclosed is a simulator and simulation method with increased precision, in particular a weapon system simulator, and weapon system provided with such a simulator. —The simulator (1) comprises a unit for generating a virtual image (I1) which is defined according to an orientation reference and a sighting reference, a unit for generating a so-called captured image from angle-error and telemetry measurements relating to one or more real actors (R1 to R4) each of which is equipped with a retroreflector (10), the angle-error and telemetry measurements being performed using a rangefinder, a comparison unit for comparing the current virtual image (I1) and the captured image so as to determine an error value representative of an orientation and/or sighting error, and a resetting unit for resetting the orientation reference and/or the sighting reference in order to correct said error value so as to create an optimised virtual image which is displayed on the vision element (2) in place of the current virtual image.
The pyrotechnic igniter simulator (1) has a detection element (5) that is able to detect at least one ignition pulse, a microcontroller (6) that is able to determine characteristics of the ignition pulse detected by the detection element (5) and to control an impedance block (7) depending on these characteristics, the microcontroller (6) being able to be configured remotely, and the impedance block (7) being able to be simulated at one of two different impedance values depending on these characteristics, one of the impedance values, referred to as the high value, simulating activation of the igniter in response to the detected ignition pulse, and the other impedance value, referred to as the low value, simulating non-activation of the igniter in response to the detected ignition pulse, the resulting simulator (1) being autonomous and especially proficient.
The invention relates to a system which comprises a workspace (3) storage module (5), at least one pointer (6) respectively associated with a gripper (4) of a robotic device (2), a module (8) for capturing the trajectory performed by the at least one pointer (6), a post-processing module (10) for determining a compatible trajectory of the one or more grippers (4), and a saving module (11), configured to save the compatible trajectory of each of the robotic devices (2).
OPTICAL TRANSPONDER INTENDED TO HELP MONITOR A STATE OF AT LEAST ONE INTERNAL DEVICE CONTAINED IN A COMMUNICATION CONTAINER, AND ASSOCIATED COMMUNICATION CONTAINER AND COMMUNICATION SYSTEM
The invention relates to an optical transponder intended to help monitor a state of at least one internal device contained in a communication container, to a communication container and to a communication system. The optical transponder comprises a receiving element (2) for receiving a light signal (SL1) from an optical communication system (16), a control unit (4) for receiving at least one electrical signal (SE3) representative at least of a physical parameter characterising an instantaneous physical state of the interior of the communication container (6) and/or of a physical parameter characterising an instantaneous physical state of the one or more internal devices (7), and a transmission element (3) for producing a light signal (SL2) representative of the physical parameters.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
41 - Éducation, divertissements, activités sportives et culturelles
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Software; Real-time embedded software; Mission planning and preparation software; Flight control software, guidance software and Navigation software; Software for image processing; Target recognition software; Communication software, Network software, Computer software for routing; computer software for human/machine interfaces; Map software; Artificial intelligence software; Interactive software based on artificial intelligence; Cloud computing software; Modelling and simulating software; Simulation software for use in digital computers; Digital sandbox simulation software; Cloud servers; Weapons simulators; Simulators for training operators in weapons systems control; Electronic systems and apparatus, for use in the following fields: Command assistance; Electronic control systems; Electronic systems and apparatus, for use in the following fields: Projectile command and control; Flight path controls for projectiles; All these goods being for defence and arms sector players for testing operational combat scenarios in a cloud-based combat environment, in particular in space, and development of industrialised solutions before the deployment thereof. Drones, Armed drones, Military drones. Ammunition, including the following products: Loitering munitions and remote-controlled munitions; Missiles and corresponding weapon systems. Providing of training, further training, Training and assistance, in relation to the following fields: Digital sandbox simulation, in particular via providing of computer manager teams and via e-learning services (providing of online electronic training); Organisation of forums, Arranging of lectures, Arranging of colloquiums and Organisation of seminars; All these services being for defence and arms sector players for testing operational combat scenarios in a cloud-based combat environment, including space, and development of industrialised solutions before the deployment thereof. Computer engineering; Cloud computing; Design, Management, hire, facilitating and Updating, In connection with the following goods: Software, computer programs, computer platforms, platforms as a service for digital simulation; Software as a service [SaaS]; Consulting services in the field of software as a service [SaaS]; Hosting of databases; Server hosting; Development of computer software application solutions; Hosting services, software as a service, and rental of software; Research, in relation to the following fields: Artificial intelligence, Especially Augmented Reality; Industrial and technical research, For the design and development of arms and software therefor for space defence missions; Platforms for artificial intelligence as software as a service [SaaS]; Artificial intelligence consultancy; Advisory services relating to man-machine interfaces for computer software; Technological research, in relation to the following fields: Digital sandbox simulation; All the aforesaid services being for defence and arms sector players for testing operational combat scenarios (in a cloud-based combat environment, including in space).
16.
METHOD AND DEVICE FOR GENERATING AN OPTIMIZED 3D POINT CLOUD OF AN ELONGATE OBJECT FROM IMAGES GENERATED BY A MULTIPATH SYNTHETIC-APERTURE RADAR
The device (1) comprises a thresholding unit (6) for performing adaptive thresholding so as to generate a segmentation mask for images generated by a synthetic-aperture radar (2) and subjected beforehand to interferometry processing, a processing unit (7) for accumulating measurements for each of the segmentation masks so as to generate at least one accumulator and one energy profile, an alignment unit (8) for calibrating the accumulators and the energy profiles so as to obtain calibrated accumulators and calibrated energy profiles, a computing unit (9) for computing a unitary cloud for each of the segmentation masks, from the calibrated accumulators and the calibrated energy profiles, and a fusion unit (10) for fusing the unitary clouds so as to obtain said optimized 3D cloud.
G01S 7/41 - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe utilisant l'analyse du signal d'écho pour la caractérisation de la cibleSignature de cibleSurface équivalente de cible
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
A firewall includes a verification unit for comparing messages transiting between the two communication elements with data, called reference data, contained in a database and for detecting, where applicable, a lack of conformity of a message in transit with respect to the reference data. The reference data includes predetermined messages and at least authorized values for fields of the predetermined messages. A central unit for generates an alert signal in the event of the verification unit detecting a lack of conformity of a message in transit. A transmission interface is configured to transmit any alert signal to at least one alert signal management device, which will generate an appropriate protective action when an alert signal is generated.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Data processing system, namely, an integrated command,
coordination and control system that enables the ordering of
a temporary installation compatible with a computer network;
radar apparatus; radar detectors; electronic scanning radar
for detecting targets; electro-optical apparatus for
tracking, classifying and the function of inhibiting
directional radio frequency signals; electronic control,
observation, tracking and monitoring systems and apparatus;
sensors, electronic sensors; smart effector and sensor
assemblies; electronic and optoelectronic apparatus for
processing, receiving and transferring data; electronic
apparatus for remote control of signals; submarine sonars;
the aforementioned products being intended for military and
civil security markets for detecting, identifying, tracking
and neutralizing rogue or threatening drones, also known as
unmanned systems (UXS) operating above and below water. Military drones; drones; remotely operated underwater
vehicles (ROVs) with on-board weapons; submarines; craft;
remote-controlled craft; rocket launching platforms [marine
vehicles]; unmanned remote-controlled military airplanes
with on-board weapons; autonomous naval platforms. Missiles and weapon systems therefor; launchers for
projectiles; torpedoes; radar jamming warheads; cannons;
shooting platforms [weapons].
19.
Device for capturing a flying craft and capture system comprising a drone provided with such a device
A capture system (1) includes a drone (4) with a capture device (3) having a net (5) and a shank (6) configured to form a closed line. The shank (6) defines a leading face (6A) and a trailing face (6B). The net (5) has a maximum diameter that is greater than a maximum diameter of the shank (6), and is attached to the shank (6) on the side (7) of the trailing face (6B). A strip (8) attaches completely around the shank (6) outside of the net (5) on the side (7) of the trailing face (6B). Holding wires (9) attach to the shank (6) on the side (10) of the leading face (6A) for towing by the drone (4). The assembly formed by the shank (6) and the strip (8) enabling the capture device (3) to be held in an optimum position for capturing a flying craft (2).
B64U 70/20 - Dispositions pour le lancement, le décollage ou l'atterrissage pour lancer ou capturer en vol les véhicules aériens sans pilote via un autre aéronef
B64D 3/02 - Adaptations des aéronefs au remorquage ou à la prise en remorque pour remorquage de cibles
B64F 1/02 - Installations au sol ou installations pour ponts d'envol des porte-avions pour l’arrêt des aéronefs, p. ex. filets ou câbles
B64U 101/16 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à la guerre conventionnelle ou électronique à la commande, à la capture ou à l’immobilisation d’autres véhicules
09 - Appareils et instruments scientifiques et électriques
13 - Armes à feu; explosifs
Produits et services
On-board electronic apparatus for helicopters, drones and
combat vehicles for launching and controlling missiles. Missiles and associated equipment, namely, launchers for
missiles.
21.
Device for detecting the absence of a mechanical barrier for a missile and missile comprising such a device
A device for detecting the absence of a mechanical barrier for a missile comprises a rod constrained by a first elastic element and a free end capable of coming into contact with the mechanical barrier and a cam constrained by a second elastic element. The rod can assume one or more of the following positions: an initial entry position wherein the rod is held in a stable position between the cam and the mechanical barrier, an extended position wherein the cam moved the rod in the direction of the free end, and a final entry position wherein the rod is acted upon by the first elastic element after the rod has been released by the cam once the rod has completely entered the missile in the final entry position so as to no longer present a danger to its environment or a hindrance to the proper functioning of the missile.
F42C 15/00 - Dispositifs d'armement des fuséesDispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges
F42C 15/24 - Dispositifs d'armement des fuséesDispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges dans lesquels l'action de sécurité ou d'armement est effectuée par des dispositifs à inertie
F42C 15/34 - Dispositifs d'armement des fuséesDispositifs de sécurité pour empêcher l'explosion prématurée des fusées ou des charges dans lesquels l'action de sécurité ou d'armement est effectuée au moyen d'un organe de blocage placé dans la chaîne pyrotechnique ou explosive entre l'amorce et la charge explosive
22.
Motherboard comprising a planar transformer equipped with components and method for assembling such a motherboard
Disclosed is a motherboard comprising at least one printed circuit board (PCB), referred to as the motherboard PCB, at least one planar transformer, which is mounted on the motherboard PCB, and a plurality of electronic components, which are also mounted on the motherboard PCB. The planar transformer comprises at least one printed circuit board with windings and a connection interface, a magnetic core arranged on the printed circuit board so as to interact with the windings, and at least one electronic component mounted on the printed circuit board.
09 - Appareils et instruments scientifiques et électriques
13 - Armes à feu; explosifs
Produits et services
(1) Appareils électroniques embarqués sur hélicoptère, drone et véhicule de combat pour le lancement et la commande de missiles.
(2) Missiles et équipements associés à savoir lanceurs pour missiles.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Data processing system, namely integrated command, coordination and control system which enables a commander to set up a computer network-enabled temporary facility; Radar apparatus; radar detectors; electronic-scanning radar for target detection; electro-optical apparatus for tracking, classification and directional radio frequency (RF) inhibition capability; electronic control, observation, monitoring and checking systems and apparatus; sensors, electronic sensors; smart-sensor and effector package; electronic and optoelectronic apparatus for the processing, reception and transfer of data; electronic apparatus for the remote control of signals; Underwater sonar; all the aforesaid being intended for military and civilian security markets for the detection, identification, tracking and neutralization of rogue or threatening drones, also referred to as unmanned systems (UXSs) operating above and under water. Military drones; drones; underwater remotely operated vehicles (ROVs) with on-board armament; submarines; seacrafts; remotely operated seacrafts; rocket launching platform [sea vehicles]; military aircrafts with on-board armament, autonomous naval platforms. Missiles and corresponding weapon systems; Launchers for projectiles; Torpedoes; Radar jamming warheads; canons; firing platforms (weapons).
The radio system (10) comprises a waveform generator (1) alternately generating an FMCW wave representing a linearly frequency-modulated continuous wave for radar imaging and a CW wave representing a wave kept at a given frequency for measuring a velocity vector, an amplification chain (2), a set (4) of transmit antennas (41, 42, 43), a set (5) of receive antennas (51, 52, 531, 532), a set (7) of receivers (71-2, 731, 732), and a signal processor (9) implementing processing operations on FMCW signals received from the one or more lateral antennas (51, 52) of the set (5) of receive antennas (51, 52, 531, 532) and spectrally analysing CW signals received from the one or more lateral antennas (51, 52) and from the one or more ventral antennas (531, 532) of the set (5) of receive antennas (51, 52, 531, 532) so as to supply SAR images and components of the velocity vector of said airborne vehicle (20).
G01S 13/34 - Systèmes pour mesurer la distance uniquement utilisant la transmission d'ondes continues, soit modulées en amplitude, en fréquence ou en phase, soit non modulées utilisant la transmission d'ondes continues modulées en fréquence, tout en faisant un hétérodynage du signal reçu, ou d’un signal dérivé, avec un signal généré localement, associé au signal transmis simultanément
G01S 13/58 - Systèmes de détermination de la vitesse ou de la trajectoireSystèmes de détermination du sens d'un mouvement
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
H01Q 21/06 - Réseaux d'unités d'antennes, de même polarisation, excitées individuellement et espacées entre elles
The device (1) for estimating the distance between an observer (2) and a target (4) using at least one image generated by a digital image generator (6) from the position (P1) of the observer (2) comprises a detection and identification unit configured to detect and identify a target (4) in the image at least from a predetermined list of known targets, an orientation estimation unit configured to determine the orientation of the identified target in the image, and a distance estimation unit configured to measure, in the image, the length of at least one characteristic segment of the target and to calculate the distance from said measured length, an actual length of the segment on the target taking into account the orientation of the target, and the spatial resolution of the digital image generator (6).
G06K 9/00 - Méthodes ou dispositions pour la lecture ou la reconnaissance de caractères imprimés ou écrits ou pour la reconnaissance de formes, p.ex. d'empreintes digitales
G06T 7/50 - Récupération de la profondeur ou de la forme
G06T 7/70 - Détermination de la position ou de l'orientation des objets ou des caméras
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
29.
Method and device for passive ranging by image processing and use of three-dimensional models
The device (1) for estimating the distance between an observer (2) and a target (4) using at least one image generated by a digital image generator (6) from the position (P1) of the observer (2) comprises a detection and identification unit configured to detect and identify a target (4) in the image and define an imaged representation of the target (4), and a distance estimation unit configured to perform, on the image, multiple different projections of a three-dimensional model of the target (4) to obtain projected representations of the target (4) and to select the projected representation most similar to the imaged representation, the distance associated with the selected projected representation representing the estimated distance (D) between the position of the observer (2) and the target (4).
G06T 7/73 - Détermination de la position ou de l'orientation des objets ou des caméras utilisant des procédés basés sur les caractéristiques
G06V 10/70 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
09 - Appareils et instruments scientifiques et électriques
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Robots for use in industry; industrial robots. Data recording apparatus; cameras; software; application
software for robots; robotic process automation [RPA]
software; visual programming software; data processing
systems and apparatus; sensors; these goods being intended
for acquiring operator techniques and gestures to transform
them into a program executable by any robot and robotic
production line. Engineering services relating to robotics; software
development; designing and developing programs for data
processing; technical data analysis services; these services
being intended for acquiring operator techniques and
gestures to transform them into a program executable by any
robot and robotic production line.
31.
Cover for a vehicle, in particular for a supersonic or hypersonic vehicle
The antenna (3) cover (1) for a vehicle is designed to cover at least one antenna (3) mounted on the vehicle, the cover (1) being made of composite material with a ceramic matrix reinforced by oxide fibers. The antenna cover (1) is resistant to high temperatures while not posing any sealing problem and remaining transparent to the frequencies used for the antennas (3) of the vehicle.
H01Q 1/42 - Enveloppes non intimement mécaniquement associées avec les éléments rayonnants, p. ex. radome
B32B 3/04 - Caractérisés par des caractéristiques de forme en des endroits déterminés, p. ex. au voisinage des bords caractérisés par une couche pliée au bord, p. ex. par-dessus une autre couche
B32B 7/05 - Liaison entre couches les couches n’étant pas liées sur toute la surface, p. ex. liaison discontinue ou par motifs particuliers
B32B 9/00 - Produits stratifiés composés essentiellement d'une substance particulière non couverte par les groupes
B32B 15/00 - Produits stratifiés composés essentiellement de métal
B32B 15/04 - Produits stratifiés composés essentiellement de métal comprenant un métal comme seul composant ou comme composant principal d'une couche adjacente à une autre couche d'une substance spécifique
B32B 15/20 - Produits stratifiés composés essentiellement de métal comportant de l'aluminium ou du cuivre
B64C 1/38 - Constructions adaptées pour réduire les effets de l'échauffement aérodynamique ou d'un échauffement externe d'autre nature
H01Q 1/02 - Dispositifs de dégivrageDispositifs de séchage
H01Q 1/27 - Adaptation pour l'utilisation dans ou sur les corps mobiles
B64G 1/58 - Protection thermique, p. ex. boucliers thermiques
32.
SIMULATOR AND SIMULATION METHOD WITH INCREASED PRECISION, IN PARTICULAR A WEAPON SYSTEM SIMULATOR, AND WEAPON SYSTEM PROVIDED WITH SUCH A SIMULATOR
- Disclosed is a simulator and simulation method with increased precision, in particular a weapon system simulator, and weapon system provided with such a simulator. - The simulator (1) comprises a unit for generating a virtual image (I1) which is defined according to an orientation reference and a sighting reference, a unit for generating a so-called captured image from angle-error and telemetry measurements relating to one or more real actors (R1 to R4) each of which is equipped with a retroreflector (10), the angle-error and telemetry measurements being performed using a rangefinder, a comparison unit for comparing the current virtual image (I1) and the captured image so as to determine an error value representative of an orientation and/or sighting error, and a resetting unit for resetting the orientation reference and/or the sighting reference in order to correct said error value so as to create an optimised virtual image which is displayed on the vision element (2) in place of the current virtual image.
The device (1) comprises a thresholding unit (6) for performing adaptive thresholding so as to generate a segmentation mask for images generated by a synthetic-aperture radar (2) and subjected beforehand to interferometry processing, a processing unit (7) for accumulating measurements for each of the segmentation masks so as to generate at least one accumulator and one energy profile, an alignment unit (8) for calibrating the accumulators and the energy profiles so as to obtain calibrated accumulators and calibrated energy profiles, a computing unit (9) for computing a unitary cloud for each of the segmentation masks, from the calibrated accumulators and the calibrated energy profiles, and a fusion unit (10) for fusing the unitary clouds so as to obtain said optimized 3D cloud.
G01S 13/42 - Mesure simultanée de la distance et d'autres coordonnées
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
G01S 7/41 - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe utilisant l'analyse du signal d'écho pour la caractérisation de la cibleSignature de cibleSurface équivalente de cible
G01S 13/88 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques
The target marking device (1) comprises a drone (2) which is provided with at least one transmitter (4), the transmitter (4) comprising an activation element (10) for activating it so that it transmits at a given time a signal (S) which represents a position information item, the transmitter (4) being configured to transmit at least one of the following signals: an infrared signal, a light signal, a sound signal, a signal generated by a chemical substance, the target marking device (1) being part of a target tracking system (6) and/or a target processing system which is provided with movable machinery (7).
B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
B64D 47/02 - Aménagements ou adaptations des dispositifs de signalisation ou d'éclairage
B64U 101/00 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques
B64U 101/15 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à la guerre conventionnelle ou électronique
The neutralisation system (1) comprises a drone (2) configured to be able to fly close to a target and transmit at least position information concerning the position of the target, the neutralisation system (1) also comprising at least one missile (6) capable of being guided towards the target in order to neutralise it and at least one control station (8), the control station (8) comprising a receiving unit (9B) capable of receiving at least the position information transmitted by the drone (2) and a display unit (10A) capable of displaying this information to an operator, the missile (6) being configured to be able to be guided towards the target by means of the position information received by the control station (8).
B64U 101/15 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à la guerre conventionnelle ou électronique
B64U 101/30 - Véhicules aériens sans pilote spécialement adaptés à des utilisations ou à des applications spécifiques à l’imagerie, à la photographie ou à la vidéographie
G05D 1/00 - Commande de la position, du cap, de l'altitude ou de l'attitude des véhicules terrestres, aquatiques, aériens ou spatiaux, p. ex. utilisant des pilotes automatiques
36.
MOTION LEARNING SYSTEM AND METHOD FOR PROGRAMMING AT LEAST ONE ROBOTIC DEVICE
The invention relates to a system which comprises a workspace (3) storage module (5), at least one pointer (6) respectively associated with a gripper (4) of a robotic device (2), a module (8) for capturing the trajectory performed by the at least one pointer (6), a post-processing module (10) for determining a compatible trajectory of the one or more grippers (4), and a saving module (11), configured to save the compatible trajectory of each of the robotic devices (2).
G05B 19/425 - Apprentissage de positions successives par commande numérique, c.-à-d. des commandes étant introduites pour commander l'asservissement en position de la tête porte-outil ou de l'effecteur de bout de bras
09 - Appareils et instruments scientifiques et électriques
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Robots for use in industry, namely technical product manufacturing, aerospace manufacturing, automotive manufacturing, mechanical manufacturing, metallurgy, robotics for entertainment purposes namely robots for amusement attractions associated with video games in virtual reality; industrial robots Data recording apparatus; cameras; downloadable or recorded computer software for process recording of technical gestures and operator techniques, simulation, industrial robot programming, process configuration, and execution system safety and supervision; downloadable or recorded application software for robots for programming and simulating its trajectories and processes; downloadable or recorded robotic process automation (RPA) software for executing the industrial process with the robot; downloadable or recorded visual programming software; data processing systems, comprised of computer hardware programmed with a 3D virtual representation of a robot and with an algorithm for controlling the robot; electric sensors; all the foregoing goods being intended for acquiring operator techniques and gestures to transform such gestures and techniques into a program executable by any robot and robotic production line Engineering services relating to robotics; computer software development; designing and developing computer programs for data processing; technical data analysis services, namely robotics processes simulation and programming; all the foregoing services being intended for acquiring operator techniques and gestures to transform such gestures and techniques into a program executable by any robot and robotic production line
38.
METHOD AND FIREWALL CONFIGURED TO MONITOR MESSAGES TRANSITING BETWEEN TWO COMMUNICATION ELEMENTS
- The firewall (1) comprises a verification unit (7) for comparing messages transiting between the two communication elements with data, called reference data, contained in a database and for detecting, where applicable, a lack of conformity of a message in transit with respect to these reference data, said reference data comprising predetermined messages and at least authorized values for fields of these predetermined messages, a central unit (10) for generating an alert signal in the event of the verification unit (7) detecting a lack of conformity of a message in transit, and a transmission interface (11) configured to transmit any alert signal to at least one alert signal management device, which will generate an appropriate protective action when an alert signal is generated.
09 - Appareils et instruments scientifiques et électriques
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Industrial robots; Industrial robots. Data collection apparatus; Film cameras; Software; Application software for robot; Robotic Process Automation [RPA] software; Visual programming software; Data processing apparatus and Data processing systems; Sensors; All the aforesaid goods being for the acquisition of operator techniques and gestures for processing thereof in an executable programme via robots and robotic production chains of all kinds. Engineering services relating to robotics; Software development; Design and development of data processing programs; Technical data analysis services; Computer services for the analysis of data; All the aforesaid services being for the acquisition of operator techniques and gestures for processing thereof in an executable programme via robots and robotic production chains of all kinds.
40.
Method for connection by brazing enabling improved fatigue resistance of brazed joints
The connection method between at least two elements (E1, E2) corresponding to a printed circuit (4) and to an electronic component (5), comprises a step of forming a plurality of pad-type stacks (2) of bosses (3), the stacks (2) of bosses (3) being formed on a face (10) of a first (E1) of the elements (E1, E2), the stacks (2) of bosses (3) each comprising the same given number of bosses (3), said method also comprising a step of depositing a brazing product (7) on this first element (E1) provided with stacks (2) of bosses (3), a step of arranging the second (E2) of the elements (E1, E2) on the first element (E1), and a step of remelting the assembly thus formed, in order to obtain an electronic device (1). This method makes it possible to produce a precise and flexible raising of surface mounted electronic components.
The deployment device may include a support piece, the deployable element, in particular a handle, may be rotatably mounted on said support piece and being connected by means of an elastic element to the support piece. The deployable element may include at least one pin capable of being moved along a curved guide of the support piece and adopting one or both of the two stable positions, respectively, in two housings provided in the support piece. The stable positions may respectively correspond to a stowed position and a deployed position of the deployable element. The guide and the elastic element may be configured to generate an automatic deployment of the deployable element to the deployed position as soon as the deployable element is subjected by an operator to a rotation having an angle greater than or equal to an unlocking angle.
A cooling device uses an endothermic chemical reaction for cooling. The cooling device includes a sealed casing with at least two reagents that generate an endothermic chemical reaction when they come into contact. The cooling device further includes a separating membrane separating the reagents in a storage position; a contact-making system which can be activated and configured to bring the reagents into contact with one another when activated, an interface element for activating the contact-making system; and a thermal interface with a thermally conductive metal base plate. One of the surfaces of the base plate is subjected to the endothermic chemical reaction, and the other surface of the base plate is accessible from outside the cooling device.
F25D 5/02 - Dispositifs utilisant des réactions chimiques endothermiques, p. ex. utilisant des mélanges frigorigènes portatifs, c.-à-d. adaptés pour être facilement transportables par une personne
B01J 16/00 - Procédés chimiques généraux faisant réagir des liquides avec des solides non particulaires, p. ex. des matériaux en feuillesAppareillage spécialement adapté à cet effet
B01J 19/18 - Réacteurs fixes avec éléments internes mobiles
F25D 5/00 - Dispositifs utilisant des réactions chimiques endothermiques, p. ex. utilisant des mélanges frigorigènes
F42B 15/34 - Protection contre la surchauffe ou l'irradiation, p. ex. boucliers thermiquesDispositions particulières pour le refroidissement
The capture system (1) comprises a drone (4) provided with a capture device (3) comprising a net (5) and a shank (6) configured to form a closed line, the shank (6) defining a leading face (6A) and a trailing face (6B), the net (5) having a maximum diameter that is greater than a maximum diameter of the shank (6), the net (5) being attached to the shank (6) on the side (7) of the trailing face (6B), the capture device (1) also comprising a strip (8) attached all the way around the shank (6) outside of the net (5) on the side (7) of the trailing face (6B) and holding wires (9) attached to the shank (6) on the side (10) of the leading face (6A) for towing thereof by the drone (4), the assembly formed by the shank (6) and the strip (8) enabling the whole of the capture device (3) to be held in an optimum position for capturing a flying craft (2).
09 - Appareils et instruments scientifiques et électriques
Produits et services
Chassis and frames of metal for test, control and
maintenance benches for missiles. Software and apparatus for data processing intended for
functional control, testing and maintenance of missiles;
machine control software; test benches [checking apparatus];
non-intrusive load control apparatus; non-intrusive device
load control apparatus; measuring, detecting, monitoring
and controlling apparatus; testing apparatus for the
control of electronic devices; apparatus and instruments
for control [inspection]; process control devices; quality
control and testing devices; control equipment for smart
processing systems; electronic control instruments for
machines; electronic control instruments; electric or
electronic control modules; connection cables, electric
cables, coaxial cables, data transmission cables; these
goods intended for functional control, testing and
maintenance of missiles.
45.
DEVICE FOR DETECTING THE ABSENCE OF A MECHANICAL BARRIER FOR A MISSILE AND MISSILE COMPRISING SUCH A DEVICE
- The device (1) for detecting the absence of a mechanical barrier for a missile (M) comprises a rod (5) constrained by a first elastic element (7) and provided with a free end (5a) capable of coming into contact with the mechanical barrier (2), a cam (8) constrained by a second elastic element (9), the rod (5) and the cam (8) being configured such that the rod (5) can assume one or more of the following positions: an initial entry position wherein the rod (5) is held in a stable position between the cam (8) and the mechanical barrier (2), an extended position wherein the rod (5) is moved by the cam (8) in the direction (E) of the free end (5a) in the absence of the mechanical barrier (2), and a final entry position wherein the rod (5) is acted upon by the first elastic element (7) after the rod (5) has been released by the cam (8) once the rod (5) has completely entered the missile (M) in said final entry position so as to no longer present a danger to its environment or a hindrance to the proper functioning of the missile (M).
Disclosed is a motherboard comprising at least one printed circuit board (8), referred to as the motherboard PCB, at least one planar transformer (1), which is mounted on said motherboard PCB (8), and a plurality of electronic components (10), which are also mounted on the motherboard PCB (8), wherein said planar transformer (1) comprises: at least one printed circuit board (3) provided with windings and with a connection interface (4); a magnetic core (5) arranged on the printed circuit board (3) so as to interact with the windings; and at least one electronic component (6) mounted on the printed circuit board (3).
09 - Appareils et instruments scientifiques et électriques
Produits et services
(1) Châssis et bâtis métalliques pour banc d'essai, de contrôle et de maintenance de missiles.
(2) Logiciels et matériel informatiques pour le traitement de données informatiques destinés au contrôle fonctionnel, aux tests et à la maintenance des missiles, logiciel pour la programmation de vol de missiles, appareils pour le traitement de données informatiques destinés au contrôle fonctionnel, aux tests et à la maintenance des missiles, nommément radars de surveillance maritime et aérien, logiciels de contrôle de machines, nommément logiciel destiné au contrôle et à la sécurité par moyens pyrotechniques, à destination militaire et du maintien de l'ordre, bancs d'essai pour missiles; appareils de contrôle de charge de dispositifs non intrusifs, nommément capteurs anti-intrusion; appareils de mesurage, de détection, de surveillance et de contrôle, nommément capteurs infrarouges, lasers infrarouges militaires à faible puissance, radars, capteurs à orientation solaire automatique, capteurs de distance, capteurs de position avec DEL, capteurs optiques, capteurs de pression, radar à émission d'ondes électromagnétiques et détecteurs à infrarouge; appareils de test pour le contrôle de dispositifs électroniques, nommément appareils de tests optiques et électro-optiques, nommément testeurs de courant, testeurs de tension, testeurs de puissance électrique; appareils et instruments de contrôle [inspection], nommément ordinateurs mobiles comportant des capteurs infrarouges de cible et de radars connectés à un ordinateur pour permettre les engagements et les tirs de missile pour l'analyse de la situation tactique et de la menace aérienne, dispositifs de contrôle de processus, nommément lasers militaires pour le guidage de missiles, dispositifs de commande à semi-conducteurs, transmetteurs radio pour commandes à distance, appareils électrodynamiques pour la commande à distance de lancement de missiles à partir de plates-formes de lancement, processeurs de signaux numériques, processeurs de signaux par satellites, processeurs de signaux vocaux numériques, récepteurs de signaux de satellites, dispositifs de test et de contrôle de la qualité pour la maintenance des missiles, équipements de contrôle pour systèmes de fabrication intelligents, nommément scanneurs optique, instruments de contrôle électroniques, nommément, écrans de commande et d'affichage tactiles, modules de contrôle électriques et électroniques, nommément modules de commande mécaniques pour machines, nommément modules de contrôle de tension, modules de puissance pour le contrôle séquentiel; câbles de connexion, nommément câble d'interconnexion en fibre optique, câbles électriques, câbles coaxiaux, câbles de transmission de données, nommément câble à fibre optique, ces produits étant destinés au contrôle fonctionnel, aux tests et à la maintenance de missiles.
09 - Appareils et instruments scientifiques et électriques
Produits et services
Frameworks and stands for testing benches, for missile control and maintenance. Data processing software and apparatus for testing and maintenance of missiles; Test benches; Nonintrusive load monitoring [NILM] apparatus; Nonintrusive appliance load monitoring [NIALM] apparatus; Measuring, detecting, monitoring and controlling devices; Testing apparatus for checking electronic devices; Checking (supervision) apparatus and instruments; Process monitors; Testing and quality control devices; Smart manufacturing system controls; Electronic control systems for machines; Electronic control instruments; Control modules (Electric or electronic -); Connection cables, Cables, electric, Coaxial cables, Data transmission cables; All the aforesaid goods being for use in functional control, testing and maintenance of missiles.
49.
RADIO SYSTEM WITH MULTIPLE ANTENNA ARRAYS AND ADAPTIVE WAVEFORMS
The radio system (10) comprises a waveform generator (1) alternately generating an FMCW wave representing a linearly frequency-modulated continuous wave for radar imaging and a CW wave representing a wave kept at a given frequency for measuring a velocity vector, an amplification chain (2), a set (4) of transmit antennas (41, 42, 43), a set (5) of receive antennas (51, 52, 531, 532), a set (7) of receivers (71-2, 731, 732), and a signal processor (9) implementing processing operations on FMCW signals received from the one or more lateral antennas (51, 52) of the set (5) of receive antennas (51, 52, 531, 532) and spectrally analysing CW signals received from the one or more lateral antennas (51, 52) and from the one or more ventral antennas (531, 532) of the set (5) of receive antennas (51, 52, 531, 532) so as to supply SAR images and components of the velocity vector of said airborne vehicle (20).
H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
G01S 13/34 - Systèmes pour mesurer la distance uniquement utilisant la transmission d'ondes continues, soit modulées en amplitude, en fréquence ou en phase, soit non modulées utilisant la transmission d'ondes continues modulées en fréquence, tout en faisant un hétérodynage du signal reçu, ou d’un signal dérivé, avec un signal généré localement, associé au signal transmis simultanément
G01S 13/32 - Systèmes pour mesurer la distance uniquement utilisant la transmission d'ondes continues, soit modulées en amplitude, en fréquence ou en phase, soit non modulées
G01S 13/58 - Systèmes de détermination de la vitesse ou de la trajectoireSystèmes de détermination du sens d'un mouvement
F41G 7/34 - Systèmes de commande de guidage pour missiles autopropulsés basés sur des données prédéterminées de la position de la cible
G01S 13/88 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques
G01S 13/02 - Systèmes utilisant la réflexion d'ondes radio, p. ex. systèmes du type radar primaireSystèmes analogues
50.
Pivot connection part for a flying machine or for a flying machine system, in particular a missile
A pivot connection part for a flying machine includes an inner body, an outer body radially surrounding the inner body, and a set of connection elements configured to connect the inner body to the outer body. Breaking the connection elements detaches the inner body from the outer body. A first blocking assembly having a cam and a stop is configured to block relative rotation between the inner and outer bodies in a first rotational direction. A second blocking assembly having a pawl and a resilient stop blade is configured to block relative rotation between the inner and outer bodies in a second rotational direction.
09 - Appareils et instruments scientifiques et électriques
13 - Armes à feu; explosifs
Produits et services
Electronic apparatus, Integrated into the following goods: Helicopters, Drones, Bomb disposal vehicles, in the following fields: Missile launching, missile control. Missiles, Associated equipment, namely, Launchers for missiles.
53.
COVER FOR A VEHICLE, IN PARTICULAR FOR A SUPERSONIC OR HYPERSONIC VEHICLE
The antenna (3) cover (1) for a vehicle is designed to cover at least one antenna (3) mounted on the vehicle, the cover (1) being made of composite material with a ceramic matrix reinforced by oxide fibers. The antenna cover (1) is resistant to high temperatures while not posing any sealing problem and remaining transparent to the frequencies used for the antennas (3) of the vehicle.
The device (1) for estimating the distance between an observer (2) and a target (4) using at least one image generated by a digital image generator (6) from the position (P1) of the observer (2) comprises a detection and identification unit configured to detect and identify a target (4) in the image at least from a predetermined list of known targets, an orientation estimation unit configured to determine the orientation of the identified target in the image, and a distance estimation unit configured to measure, in the image, the length of at least one characteristic segment of the target and to calculate the distance from said measured length, an actual length of the segment on the target taking into account the orientation of the target, and the spatial resolution of the digital image generator (6).
The device (1) for estimating the distance between an observer (2) and a target (4) using at least one image generated by a digital image generator (6) from the position (P1) of the observer (2) comprises a detection and identification unit configured to detect and identify a target (4) in the image and define an imaged representation of the target (4), and a distance estimation unit configured to perform, on the image, multiple different projections of a three-dimensional model of the target (4) to obtain projected representations of the target (4) and to select the projected representation most similar to the imaged representation, the distance associated with the selected projected representation representing the estimated distance (D) between the position of the observer (2) and the target (4).
The target marking device (1) comprises a drone (2) which is provided with at least one transmitter (4), the transmitter (4) comprising an activation element (10) for activating it so that it transmits at a given time a signal (S) which represents a position information item, the transmitter (4) being configured to transmit at least one of the following signals: an infrared signal, a light signal, a sound signal, a signal generated by a chemical substance, the target marking device (1) being part of a target tracking system (6) and/or a target processing system which is provided with movable machinery (7).
F42B 12/40 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour libérer des matériaux, des corps ou des particulesProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour produire une réaction chimique ou physiqueProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation pour le marquage de la cible, c.-à-d. du type à indication d'impact
The neutralisation system (1) comprises a drone (2) configured to be able to fly close to a target and transmit at least position information concerning the position of the target, the neutralisation system (1) also comprising at least one missile (6) capable of being guided towards the target in order to neutralise it and at least one control station (8), the control station (8) comprising a receiving unit (9B) capable of receiving at least the position information transmitted by the drone (2) and a display unit (10A) capable of displaying this information to an operator, the missile (6) being configured to be able to be guided towards the target by means of the position information received by the control station (8).
F42B 12/36 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour libérer des matériaux, des corps ou des particulesProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour produire une réaction chimique ou physiqueProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation
F42B 12/40 - Projectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour libérer des matériaux, des corps ou des particulesProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour produire une réaction chimique ou physiqueProjectiles ou mines caractérisés par la charge militaire, l'effet recherché ou le matériau caractérisés par la nature de la charge militaire ou par l'effet recherché pour la signalisation pour le marquage de la cible, c.-à-d. du type à indication d'impact
G05D 1/12 - Commande pour la recherche d'un objectif
F41G 7/32 - Systèmes de guidage à liaison de commande pour les missiles guidés par fil
F41G 7/30 - Systèmes de guidage à liaison de commande
58.
DEVICE FOR DEPLOYING A DEPLOYABLE ELEMENT, IN PARTICULAR A HANDLE, FOR A WEAPON SYSTEM
The deployment device (1) comprises a support piece (6), the deployable element (2), in particular a handle, being rotatably mounted on said support piece (6) and being connected by means of an elastic element (16) to the support piece (6), the deployable element (2) comprising at least one pin (22) capable of being moved along a curved guide (24) of the support piece (6) and adopting one or both of the two stable positions, respectively, in two housings provided in the support piece (6), said stable positions respectively corresponding to a stowed position and a deployed position of the deployable element (2), the guide (24) and the elastic element (16) being configured to generate an automatic deployment of the deployable element (2) to the deployed position as soon as the deployable element (2) is subjected by an operator to a rotation having an angle greater than or equal to an unlocking angle (θ0).
A device is configured for deflecting a stream of particles for a projectile guided by a link wire, the projectile having a fuselage and an engine capable of producing a propulsive jet containing the stream of particles. The device includes a device support including an inner surface configured to attach the device support to the fuselage of the projectile, and a deflector strip assuming at least an unfolded position in which the deflector strip forms an angle with the device support in order to deflect the stream of particles.
F42B 15/04 - Dispositions pour le guidage ou le pilotage sur les projectiles autopropulsés ou les missiles utilisant un fil, p. ex. pour le guidage des roquettes sol-sol
60.
METHOD FOR CONNECTION BY BRAZING ENABLING IMPROVED FATIGUE RESISTANCE OF BRAZED JOINTS
The connection method between at least two elements (E1, E2) corresponding to a printed circuit (4) and to an electronic component (5), comprises a step of forming a plurality of pad-type stacks (2) of bosses (3), the stacks (2) of bosses (3) being formed on a face (10) of a first (E1) of the elements (E1, E2), the stacks (2) of bosses (3) each comprising the same given number of bosses (3), said method also comprising a step of depositing a brazing product (7) on this first element (E1) provided with stacks (2) of bosses (3), a step of arranging the second (E2) of the elements (E1, E2) on the first element (E1), and a step of remelting the assembly thus formed, in order to obtain an electronic device (1). This method makes it possible to produce a precise and flexible raising of surface mounted electronic components.
An actuation device for ejecting a removable part of a missile includes a pyrotechnic actuator having a pyrotechnic charge configured to generate an overpressure and a piston configured to act on the removable part of the missile, at least one retaining rod, and at least one thermal insulation element configured to thermally insulate at least the pyrotechnic charge. The pyrotechnic actuator is configured to break the retaining rod.
F42B 15/36 - Moyens de liaison entre le moteur-fusée et le corps d'une roquetteRaccords pour relier les différents étages d'une roquetteMoyens de désassemblage
F42B 15/34 - Protection contre la surchauffe ou l'irradiation, p. ex. boucliers thermiquesDispositions particulières pour le refroidissement
62.
Balancing assembly comprising balancing rings for a missile and missile provided with such a balancing assembly
Missile balancing assemblies include two balancing rings configured for mounting on a missile, each balancing ring having a ballast. Each balancing ring is configured to be rotated and rotationally fixed, and may include materials having different densities at different locations. Each balancing ring may further include an angular graduation.
A missile includes a separable nose cone having an ejectable shell cooperating with a support element. The missile has a body with a main longitudinal axis and a nose cone having a shell connected by a rear end thereof to a support element of the missile and defined around a secondary longitudinal axis. The support element has a housing, and the rear end of the shell has a thickness adapted to be received in the housing in a contacting manner. The housing is configured to allow the shell to pivot and to maintain contact while the orientation of the shell is such that the secondary longitudinal axis is at an angle smaller than an ejection angle in relation to said main longitudinal axis, and to end the contact when the secondary longitudinal axis is at an angle higher than or equal to the ejection angle in such a way as to eject the shell from the missile.
The present invention relates to an electromagnetic assembly of polyphase structure, said assembly including: a yoke comprising an electromagnetic body; a plurality of spaced-apart blocks that protrude with respect to one of the carrier faces of the yoke and that are arranged, consecutively, along the periphery of the carrier face of the yoke; and at least one winding that is associated with the blocks, wherein there is only one yoke, the plurality of blocks is arranged in at least two groups of blocks (A, B, C) in which two consecutive blocks of a given group of blocks (A, B, C) are spaced apart by an inter-block distance (E), and each group of blocks (A, B, C) is separated from the adjacent group of blocks (A, B, C) by an inter-group distance (D) that is different from the inter-block distance (E).
A prediction device includes a data input assembly, a modelling unit, a resolution unit, an interpretation unit, and an information transmission unit. The data input assembly is configured to enter attacker data relating to attack models, and defender data relating to ground a zone to be defended and to available defense means. The modelling unit is configured to generate a game tree evaluated on the basis of input data, based on game theory. The resolution unit is configured to define a game balance based on game theory, the game balance defining an attacker strategy and defender strategy pair. The interpretation unit is configured to determine, on the basis of the game balance, an optimum attack solution, as well as an optimum defense solution that is best suited to the optimum attack solution.
A flexible cover includes a main layer made of a first composite material that includes a first woven material and a first elastomer. The flexible cover also includes an auxiliary layer made of a second composite material that includes a second woven material and a second elastomer. The auxiliary layer is secured to a face of the main layer and includes petal-shaped regions that are separated from one another by weakening lines.
The invention relates to a cooling device with an endothermic chemical reaction. The cooling device (1) comprises: a sealed casing (2) including at least two reagents (R1, R2), said reagents (R1, R2) being such that an endothermic chemical reaction is generated when they come into contact with one another; a separating membrane (3) for separating the reagents (R1, R2) in a storage position; a contact-making system (4) which can be activated and configured to bring the reagents (R1, R2) into contact with one another when activated, in order to trigger the endothermic chemical reaction; an interface element (5) for activating the contact-making system (4); and a thermal interface (6) comprising a thermally conductive metal base plate (7), one of the surfaces (S1) of which is subjected, if necessary, to the endothermic chemical reaction and the other surface (S2) of which is accessible from outside the cooling device (1).
22 - Cordes; filets; tentes, auvents, voiles et sacs; matières de rembourrage
24 - Tissus et produits textiles
Produits et services
Nets, namely, camouflage nets for visual, infrared and radar uses; tents; covers for camouflage, namely, unfitted canvas covers for vehicles, watercraft, and shelters; tarpaulins Camouflage fabric for textile use, namely, for use in the manufacture of covers, canvas covers, tarpaulins and clothing for protection against visual, infrared and radar uses; textile goods made out of composite threads designed for camouflaging goods, namely, textile fabrics for the manufacture of covers, canvas covers, tarpaulins and clothing for protection against visual, infrared and radar uses
69.
DEVICE FOR DEFLECTING A STREAM OF PARTICLES FOR A PROJECTILE GUIDED BY A LINK WIRE
- Device for deflecting a stream of particles for a projectile guided by a link wire. The device (1) for deflecting a stream of particles for a projectile (30), the projectile being guided by a link wire and being provided with a fuselage (2) and an engine that is capable of producing a propulsive jet containing the stream of particles, comprises a device support (4) including an inner surface corresponding to a surface that is configured to attach the device support (4) to the fuselage (2) of the projectile (30), and a deflector strip (5) assuming at least an unfolded position in which the deflector strip (5) forms an angle with the device support (4) in order to deflect the stream of particles.
F42B 15/04 - Dispositions pour le guidage ou le pilotage sur les projectiles autopropulsés ou les missiles utilisant un fil, p. ex. pour le guidage des roquettes sol-sol
- The pivot connection part (1) is in one piece and comprises an inner body (2), an outer body (3) radially surrounding the inner body (2), a set of connection elements (4) producing a continuity of material between the inner and outer bodies (2, 3) in an initial relative position, the breaking of the connecting elements (4) detaching the inner and outer bodies (2, 3) from each other and thus allowing a relative rotation between them, a blocking assembly (5) comprising at least one cam (7) and a stop, capable of blocking the relative rotation between the inner and outer bodies (2, 3) in a first direction of rotation in an end relative blocking position, and a blocking assembly (9) comprising at least one pawl (11) and a resilient stop blade (12), capable of blocking the relative rotation between the inner and outer bodies (2, 3) in a second direction of rotation, opposite to said first direction of rotation, in the blocking position.
– The device (7) is a one-piece assembly which comprises a pyrotechnic actuator (9) comprising a pyrotechnic charge (12) able to generate an overpressure and a piston (14) configured to move in a longitudinal direction so that one of the ends of the piston (14) can act on the removable part of the missile, at least one retaining rod (10A, 10B), and at least one thermal insulation element (11A, 11B, 11C) arranged in such a way as to thermally insulate at least the pyrotechnic charge (12), the pyrotechnic actuator (9) being configured to generate a force capable of breaking the retaining rod (10A, 10B), a first end of the retaining rod (10A, 10B) and one end of the pyrotechnic actuator (9) being secured to a securing element (18) belonging to the missile, and a second end, opposite to the first end, of the retaining rod (10A, 10B) being secured to a securing element belonging to the removable part of the missile.
F42B 15/34 - Protection contre la surchauffe ou l'irradiation, p. ex. boucliers thermiquesDispositions particulières pour le refroidissement
F42B 15/36 - Moyens de liaison entre le moteur-fusée et le corps d'une roquetteRaccords pour relier les différents étages d'une roquetteMoyens de désassemblage
09 - Appareils et instruments scientifiques et électriques
Produits et services
Electronic control, observation, tracking and monitoring
systems and apparatus, particularly for missiles; radars;
radar detectors; radars; on-board radars and components
thereof; radar installations; data processing apparatus;
sensors, electronic sensors; electronic and optoelectronic
apparatus for processing, receiving and transferring data;
electronic apparatus for remote control of signals;
telecommunication apparatus; software; computer programs.
09 - Appareils et instruments scientifiques et électriques
Produits et services
Sensors, electronic sensors; electronic control and
monitoring apparatus and system for launching missiles;
electronic and optoelectronic apparatus for processing,
receiving and transferring data; electronic apparatus for
remote control of signals; telecommunication apparatus;
software; computer programs.
77.
MISSILE PROVIDED WITH A SEPARABLE NOSE CONE COMPRISING AT LEAST ONE EJECTABLE SHELL COOPERATING WITH A SUPPORT ELEMENT
The invention relates to a missile provided with a separable nose cone comprising at least one ejectable shell cooperating with a support element. Said missile (1) is provided with a body (7) having a main longitudinal axis (X-X) and a nose cone (2) comprising at least one shell (3, 4) connected by a rear end thereof to a support element (10) of the missile (1) and defined around a secondary longitudinal axis, the support element (10) being provided with a housing, the rear end of the shell (3, 4) having a thickness adapted to said housing such that it can be received in the housing in a contacting manner, the housing being designed so as to allow the shell (3, 4) to pivot and to maintain the contact while the orientation of the shell (3, 4) is such that the secondary longitudinal axis is at an angle smaller than a so-called ejection angle in relation to said main longitudinal axis (X-X), and to end said contact as soon as said secondary longitudinal axis (L-L) is at an angle higher than or equal to said ejection angle in such a way as to eject the shell (3, 4) from the missile (1).
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Armored vehicles for locomotion by land; missile-launching
land vehicles. Armored turrets mounted on land vehicles; turrets for
machine guns; missiles and their mobile weapon systems.
82.
Method and device for determining the distance between an airborne receiver and a stationary ground transmitter
A method and device for determining the distance between an airborne receiver and a stationary ground transmitter are disclosed. A digital terrain model is implemented to determine a range of distance values containing the transmitter. A receiver distance is found and, with the range of values, a plurality of theoretical distances is calculated, to each of which a corresponding azimuth angle and elevation angle are associated. The thus calculated azimuth and elevation angles are compared to the measured azimuth and elevation angles of the line of sight under which the receiver observes the transmitter.
G01S 11/12 - Systèmes pour déterminer la distance ou la vitesse sans utiliser la réflexion ou la reradiation utilisant des ondes électromagnétiques autres que les ondes radio
G01S 7/495 - Contre-mesures ou anti-contre-mesures
G01S 3/782 - Systèmes pour déterminer une direction ou une déviation par rapport à une direction prédéterminée
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
G01V 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
83.
METHOD AND DEVICE FOR PREDICTING OPTIMUM ATTACK AND DEFENCE SOLUTIONS IN A MILITARY CONFLICT SCENARIO
The prediction device (1) comprises a data input assembly (2) for entering, into said device (1), both the attacker data relating at least to attack models, and defender data relating at least to a zone to be defended and to available defence means, a modelling unit (4) for generating a game tree evaluated on the basis of input data, in the context of game theory, a resolution unit (6) for defining a game balance in the context of games theory, a balance defining an attacker strategy and defender strategy pair, an interpretation unit (7) for determining, on the basis of the game balance, an optimum attack solution, as well as an optimum defence solution that is best suited to this optimum attack solution, and an information transmission unit (9) for transmitting this information.
A flexible cover comprising at least one, so-called composite, layer, formed from a composite material consisting of at least one fabric and at least one elastomer and a flat metal blade secured to the composite layer by elastomer and comprising pre-cut lines for fragilisation of the flexible cover, the pre-cut lines being arranged so as to create areas in the form of petals, the composite layer and the metal blade being designed so as to return to an initial position once the flexible cover has been opened.
F41F 3/077 - Panneaux de fermeture ou couvercles pour des tubes de lancement
B32B 15/14 - Produits stratifiés composés essentiellement de métal adjacent à une couche fibreuse ou filamenteuse
B32B 15/04 - Produits stratifiés composés essentiellement de métal comprenant un métal comme seul composant ou comme composant principal d'une couche adjacente à une autre couche d'une substance spécifique
B32B 25/02 - Produits stratifiés composés essentiellement de caoutchouc naturel ou synthétique avec des fibres ou particules enrobées dans le caoutchouc ou liées au caoutchouc
F16J 15/06 - Joints d'étanchéité entre surfaces immobiles entre elles avec garniture solide comprimée entre les surfaces à joindre
F16J 15/12 - Joints d'étanchéité entre surfaces immobiles entre elles avec garniture solide comprimée entre les surfaces à joindre par garniture non métallique par renforcement ou couverture métallique
09 - Appareils et instruments scientifiques et électriques
Produits et services
Electronic control, observation, monitoring and checking systems and apparatus, in particular for missiles; Radar apparatus; Radar detectors; Shipboard radars and components; Radar apparatus; Data processing apparatus; Sensors, electronic sensors; Electronic and optoelectronic apparatus for the processing, reception and transfer of data; Electronic apparatus for the remote control of signals; Telecommunication apparatus; Computer software; Software.
09 - Appareils et instruments scientifiques et électriques
Produits et services
Sensors, electronic sensors; Electronic command and control systems and apparatus for launching missiles; Electronic and optoelectronic apparatus for the processing, reception and transfer of data; Electronic apparatus for the remote control of signals; Telecommunication apparatus; Computer software; Software.
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
13 - Armes à feu; explosifs
Produits et services
Armoured vehicles for locomotion by land; Missile launchers (land vehicles). Armoured turrets mounted on land vehicles; Machine gun turrets; Missiles and mobile weapons systems relating thereto.
The present invention relates to an electromagnetic assembly (1) of polyphase structure, said assembly including: a yoke (5) comprising an electromagnetic body; a plurality of spaced-apart blocks (50) that protrude with respect to one of the carrier faces (5A, 5B) of the yoke (5) and that are arranged, consecutively, along the periphery of the carrier face (5A, 5B) of the yoke (5); and at least one winding (6) that is associated with the blocks (50), wherein there is only one yoke (5), the plurality of blocks (50) is arranged in at least two groups of blocks (A, B, C) in which two consecutive blocks (50) of a given group of blocks (A, B, C) are spaced apart by an inter-block distance (E), and each group of blocks (A, B, C) is separated from the adjacent group of blocks (A, B, C) by an inter-group distance (D) that is different from the inter-block distance (E).
The invention relates to a balancing assembly (1) comprising two balancing rings (4A, 4B) to be mounted on a missile, each of said balancing rings (4A, 4B) comprising a ballast (5A, 5B) located on the corresponding balancing ring (4A, 4B). According to the invention, each of the balancing rings (4A, 4B) can be driven in rotation and fixed in a given angular position.
An impact-detection device includes at least one waveguide provided at each of the two ends thereof with a connector. The device further includes a ring with a curved outer contour. The ring forms a separate part with planar radial surfaces. The waveguide is built into the body of the ring about the ring, and the two ends of the waveguide are arranged on the outside of the ring.
G01D 5/353 - Moyens mécaniques pour le transfert de la grandeur de sortie d'un organe sensibleMoyens pour convertir la grandeur de sortie d'un organe sensible en une autre variable, lorsque la forme ou la nature de l'organe sensible n'imposent pas un moyen de conversion déterminéTransducteurs non spécialement adaptés à une variable particulière utilisant des moyens optiques, c.-à-d. utilisant de la lumière infrarouge, visible ou ultraviolette avec atténuation ou obturation complète ou partielle des rayons lumineux les rayons lumineux étant détectés par des cellules photo-électriques en modifiant les caractéristiques de transmission d'une fibre optique
