Produits et services

Sensors, detectors and monitoring instruments; measuring, detecting, monitoring and controlling devices; surveillance cameras; aerials; devices for automatic piloting; image capture devices; visual monitoring apparatus; apparatus for recording images; apparatus for the processing of images; software, for use in the following fields: autonomous navigation; computer software; navigation, guidance, tracking, targeting and map making devices; target location apparatus [optical], target location apparatus [electronic]; target seekers [optical], target trackers [electronic]; electronic and optical target surveillance apparatus; flight controlling apparatus; homing heads; target trackers; steering systems; guidance systems; radar transmitters; radar receivers; radar apparatus; simulators for training operators in weapons systems control; all the aforesaid goods, especially, for use in relation to the following goods: missiles, rockets, aircrafts, aerial drones or remote carriers; warning systems for the approach of missiles, rockets, aircraft, drones or remote carriers. Aircraft; military aircraft; pilotless aircraft; unmanned aerial vehicles [UAVs]; drones; civilian drones; military drones; pilotless surveying aircraft; remote controlled flying objects; remotely controlled vehicles for transport; vehicle networks comprising several of the aforesaid vehicles, drones or remotely controlled vehicles; parts for the aforesaid vehicles, drones or remotely controlled vehicles; launch mechanisms for the aforesaid vehicles, drones or remotely controlled vehicles; networks comprising several of the aforesaid aircrafts or remotely controlled vehicles; aircrafts and remotely controlled vehicles equipped with weapon systems. Cruise missiles; guided missiles; rockets; guided missiles; air-to-surface missiles; air-to-air missiles; unmanned rockets and missiles for searching military targets; networks comprised of missiles and rockets for finding military targets; weapon systems comprising several of the aforesaid networked missiles, rockets and projectiles; launchers for missiles [weapons]; rocket launchers; containers for launching missiles or rockets; containers for storing missiles or rockets; conducted electrical weapons (CEW); rockets [projectiles]; ballistic weapons; motorized weapons; weapons for launching missiles; weapons for launching projectiles; weapons for launching missiles and projectiles; ballistic weapons; rocket-propelled ballistic missiles; conventional air delivered weapons.

Produits et services

Sensors, detectors and monitoring instruments; measuring, detecting, monitoring and controlling devices; surveillance cameras; aerials; devices for automatic piloting; image capture devices; visual monitoring apparatus; apparatus for recording images; apparatus for the processing of images; software, for use in the following fields: autonomous navigation; computer software; navigation, guidance, tracking, targeting and map making devices; target location apparatus [optical], target location apparatus [electronic]; target seekers [optical], target trackers [electronic]; electronic and optical target surveillance apparatus; flight controlling apparatus; homing heads; target trackers; steering systems; guidance systems; radar transmitters; radar receivers; radar apparatus; simulators for training operators in weapons systems control; all the aforesaid goods, especially, for use in relation to the following goods: missiles, rockets, aircrafts, aerial drones or remote carriers; warning systems for the approach of missiles, rockets, aircraft, drones or remote carriers. Aircraft; military aircraft; pilotless aircraft; unmanned aerial vehicles [UAVs]; drones; civilian drones; military drones; pilotless surveying aircraft; remote controlled flying objects; remotely controlled vehicles for transport; vehicle networks comprising several of the aforesaid vehicles, drones or remotely controlled vehicles; parts for the aforesaid vehicles, drones or remotely controlled vehicles; launch mechanisms for the aforesaid vehicles, drones or remotely controlled vehicles; networks comprising several of the aforesaid aircrafts or remotely controlled vehicles; aircrafts and remotely controlled vehicles equipped with weapon systems. Cruise missiles; guided missiles; rockets; guided missiles; air-to-surface missiles; air-to-air missiles; unmanned rockets and missiles for searching military targets; networks comprised of missiles and rockets for finding military targets; weapon systems comprising several of the aforesaid networked missiles, rockets and projectiles; launchers for missiles [weapons]; rocket launchers; containers for launching missiles or rockets; containers for storing missiles or rockets; conducted electrical weapons (CEW); rockets [projectiles]; ballistic weapons; motorized weapons; weapons for launching missiles; weapons for launching projectiles; weapons for launching missiles and projectiles; ballistic weapons; rocket-propelled ballistic missiles; conventional air delivered weapons.

Produits et services

Vehicles; Tracked vehicles; Remotely operated vehicles; All-terrain vehicles; Unmanned vehicles; Autonomous cars; Military vehicles for transport.

Produits et services

Unmanned aerial vehicles (UAVs); Drones. Rockets; Electrically-operated flying effectors with warheads; Drones with warheads.

Produits et services

Drone detection systems; electric components for controlling operating procedures in drone defence systems; electric components for detecting or verifying or combating drones; optical apparatus and instruments; measuring, signaling and checking apparatus and instruments; apparatus and instruments for conducting, switching, transforming, accumulating, regulating or controlling electricity; digital recording media; data processing equipment; computers; computer software; alarms; testing apparatus not for medical purposes; antennas; observation instruments; data processing apparatus; detectors; distance measuring apparatus; physics (apparatus and instruments for -); radar apparatus; transmitters; mains monitoring apparatus (electric -); camcorders.

Abrégé

An energy source provides electrical energy in a missile, which is configured to heat at least one structural section during an intended flight, so that heat is available there. At least one thermal battery has at least one cell, which contains an electrolyte. The electrolyte is to be heated by the input of heat for providing the electrical energy at the thermal battery. At least one electrolyte can be thermally coupled to the structural section in order to transfer at least part of the heat provided at the structural section during flight from there to the electrolyte. A missile contains the energy source in which at least one electrolyte is thermally coupled to the structural section.

Classes IPC  ?

• H01M 6/36 - Éléments à action différée contenant un électrolyte et rendus opérationnels par des moyens physiques, p. ex. éléments thermiques
• F42B 15/00 - Projectiles autopropulsés, p. ex. roquettesMissiles
• H01M 6/46 - Groupement d'éléments primaires en batteries d'éléments plats
• H01M 6/50 - Procédés ou dispositions pour assurer le fonctionnement ou l'entretien, p. ex. pour le maintien de la température de fonctionnement

Abrégé

The invention relates to a method for checking the alignment of a secondary surveillance radar (2), wherein a radar object (28) with a known actual position (26) is detected by the secondary surveillance radar (2) and the radar position (36) of the radar object (28) is determined and compared with the actual position (26). In order to enable the radar alignment to be checked even if there is not a real radar object (8) present in the airspace captured by the secondary surveillance radar (2), it is proposed that the checking be performed with a virtual radar object (28).

Classes IPC  ?

• G01S 7/40 - Moyens de contrôle ou d'étalonnage
• G01S 13/78 - Systèmes utilisant la reradiation d'ondes radio, p. ex. du type radar secondaireSystèmes analogues dans lesquels des signaux de type pulsé sont transmis effectuant la discrimination entre différents types de cibles, p. ex. radar pour l'identification ami–ennemi
• G01S 13/87 - Combinaisons de plusieurs systèmes radar, p. ex. d'un radar primaire et d'un radar secondaire

Abrégé

The invention relates to a method for operating a missile (2) on a launch platform (6). In order to allow the missile (2) to reliably perform the required trajectory after launch, the missile (2) determines its orientation relative to the launch platform (6) by means of its seeker head (4) and a direction sensor (16a - 16f) of the launch platform (6).

Classes IPC  ?

• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés
• F41G 7/22 - Systèmes autodirecteurs

Abrégé

The invention relates to a ship defense unit (4) with a plurality of rocket launcher pods (6). In order to make retrofitting easier by keeping the volume required for this on the ship (2) low, it is proposed that the ship defense unit (4) has a pivoting mechanism (28, 48) which defines a pivoting motion of the rocket launcher pods (6) from a compact rest position into a launching position requiring a larger volume.

Classes IPC  ?

• B63G 1/00 - Aménagements relatifs à l'artillerie ou au lancement des missilesNavires caractérisés à cet effet

Produits et services

Sensors, detectors and monitoring instruments; Measuring, detecting, monitoring and controlling devices; Surveillance cameras; Aerials; Devices for automatic piloting; Image capture devices; Visual monitoring apparatus; Apparatus for recording images; Apparatus for the processing of images; Software, for use in the following fields: Autonomous navigation; Computer software; Navigation, guidance, tracking, targeting and map making devices; Target location apparatus [optical], Target location apparatus [electronic]; Target seekers [optical], Target trackers [electronic]; electronic and optical target surveillance apparatus; Flight controlling apparatus; Homing heads; Target Trackers; Steering systems; Guidance systems; Radar transmitters; Radar receivers; Radar apparatus; Simulators for training operators in weapons systems control; all the aforesaid goods, Especially, for use in relation to the following goods: Missiles, Rockets, Aircrafts, aerial drones or Remote carriers; Warning systems for the approach of missiles, rockets, aircraft, drones or remote carriers. Aircraft; Military aircraft; Pilotless aircraft; Unmanned aerial vehicles [UAVs]; Drones; Civilian drones; Military drones; Pilotless surveying aircraft; Remote controlled flying objects; Remote carriers; Vehicle networks comprising several of the aforesaid vehicles, drones, missiles or remote carriers; Components for the aforesaid vehicles, drones, missiles or remote carriers; Launching platforms for the aforesaid vehicles, drones, missiles or remote carriers; Rocket launching platforms [vehicles]; Networks comprising several of the aforesaid aircraft or remote carriers; Weapon systems comprising several of the aforesaid networked aircraft or remote carriers. Cruise missiles; Guided missiles; Rockets; Guided missiles; Air-to-surfaces missiles; Air-to-air missiles; Unmanned remote-controlled powered aircraft for use as military targets; Remote carriers for searching for military targets; Networks comprising several of the aforesaid missiles, rockets, aircraft or remote carriers for searching for military targets; Weapon systems comprising several of the aforesaid networked missiles, rockets, aircraft or remote carriers; Launchers for missiles [weapons]; Rocket launchers; Containers for launching missiles or rockets; Containers for storing missiles or rockets; Conducted electrical weapons (CEW); Rockets [projectiles]; Ballistic weapons; Motorized weapons; Weapons for launching missiles; Weapons for launching projectiles; Weapons for launching missiles and projectiles; Ballistic weapons; Rocket-propelled ballistic missiles; Conventional air delivered weapons.

Produits et services

Sensors, detectors and monitoring instruments; Measuring, detecting, monitoring and controlling devices; Surveillance cameras; Aerials; Devices for automatic piloting; Image capture devices; Visual monitoring apparatus; Apparatus for recording images; Apparatus for the processing of images; Software, for use in the following fields: Autonomous navigation; Computer software; Navigation, guidance, tracking, targeting and map making devices; Target location apparatus [optical], Target location apparatus [electronic]; Target seekers [optical], Target trackers [electronic]; electronic and optical target surveillance apparatus; Flight controlling apparatus; Homing heads; Target Trackers; Steering systems; Guidance systems; Radar transmitters; Radar receivers; Radar apparatus; Simulators for training operators in weapons systems control; all the aforesaid goods, Especially, for use in relation to the following goods: Missiles, Rockets, Aircrafts, aerial drones or Remote carriers; Warning systems for the approach of missiles, rockets, aircraft, drones or remote carriers. Aircraft; Military aircraft; Pilotless aircraft; Unmanned aerial vehicles [UAVs]; Drones; Civilian drones; Military drones; Pilotless surveying aircraft; Remote controlled flying objects; Remote carriers; Vehicle networks comprising several of the aforesaid vehicles, drones, missiles or remote carriers; Components for the aforesaid vehicles, drones, missiles or remote carriers; Launching platforms for the aforesaid vehicles, drones, missiles or remote carriers; Rocket launching platforms [vehicles]; Networks comprising several of the aforesaid aircraft or remote carriers; Weapon systems comprising several of the aforesaid networked aircraft or remote carriers. Cruise missiles; Guided missiles; Rockets; Guided missiles; Air-to-surfaces missiles; Air-to-air missiles; Unmanned remote-controlled powered aircraft for use as military targets; Remote carriers for searching for military targets; Networks comprising several of the aforesaid missiles, rockets, aircraft or remote carriers for searching for military targets; Weapon systems comprising several of the aforesaid networked missiles, rockets, aircraft or remote carriers; Launchers for missiles [weapons]; Rocket launchers; Containers for launching missiles or rockets; Containers for storing missiles or rockets; Conducted electrical weapons (CEW); Rockets [projectiles]; Ballistic weapons; Motorized weapons; Weapons for launching missiles; Weapons for launching projectiles; Weapons for launching missiles and projectiles; Ballistic weapons; Rocket-propelled ballistic missiles; Conventional air delivered weapons.

Produits et services

Drone detection systems; Electric components for controlling operating procedures in drone defence systems; Electric components for detecting or verifying or combating drones; Optical apparatus and instruments; Measuring, signaling and checking apparatus and instruments; Apparatus and instruments for conducting, switching, transforming, accumulating, regulating or controlling electricity; Digital recording media; Data processing equipment; Computers; Computer software; Alarms; Testing apparatus not for medical purposes; Aerials; Observation instruments; Data processing apparatus; Detectors; Distance measuring apparatus; Apparatus and instruments for physics; Radar apparatus; Transmitters; Mains monitoring apparatus (Electric -); Camcorders; All the aforementioned devices related to defence and military equipment for detecting, checking or combating drones; None of the foregoing relating to education, entertainment, on-demand television services, telecommunications, broadcasting, broadband, fixed and mobile telephony, advertising services, sponsorship, weather forecasting and smart home services, home protection and security services.

Abrégé

A Marx configuration has a housing surrounding an interior, and a Marx generator arranged in the interior. The Marx generator has a plurality of capacitor stages connected in series, each having at least one first and one second voltage terminal, and respective cross branches. Each two adjacent capacitor stages between the first terminal of the preceding and the second terminal of the following capacitor stage are connected by one of the cross branches. Each of the cross branches contains a spark gap, a sealed gas space for an insulating gas for the spark gaps which are arranged in the interior and at least two of the spark gaps. All spark gaps are arranged in a respective gas space, and the interior contains a sealed fluid space for a cooling fluid for the Marx generator. A base support disposed in the interior and surrounds the gas space partially.

Classes IPC  ?

• H01T 15/00 - Circuits spécialement adaptés aux éclateurs, p. ex. circuits d'allumage
• H05K 7/20 - Modifications en vue de faciliter la réfrigération, l'aération ou le chauffage

Abrégé

An effector data connector (22) for data connection of an effector (10) to a firing platform (2). The effector data connector (22) contains a data storage module (34) for recording firing data in order to increase safety during the use of effectors (10).

Classes IPC  ?

• F41G 9/00 - Systèmes de commande des missiles ou projectiles, non prévus ailleurs
• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés
• F41F 3/06 - Lanceurs de roquettes ou de torpilles pour roquettes à partir d'avions
• B64D 7/08 - Agencement des lanceurs de roquettes
• H01R 13/66 - Association structurelle avec des composants électriques incorporés

Abrégé

A Marx generator has at least two branches for providing a Marx voltage at an output pole. Each of the branches has a plurality of capacitor stages with voltage poles, cross branches with spark gaps, a last capacitor stage at its output end, and a first capacitor stage connected to an operating voltage. The branches have a common triggering section with a common first capacitor stage, a first adjacent cross branch, and an input pole. Each of the branches has the triggering section and also an individual portion with at least one capacitor stage that is only associated with the branch. A resonator arrangement contains the Marx generator and resonators at the respective output poles of the branches. A radiation arrangement has the resonator arrangement and a multi-feed waveguide with at least two of the resonators for respectively feeding an electromagnetic wave.

Classes IPC  ?

• H02M 3/06 - Transformation d'une puissance d'entrée en courant continu en une puissance de sortie en courant continu sans transformation intermédiaire en courant alternatif par convertisseurs statiques utilisant des résistances ou des capacités, p. ex. diviseur de tension

Abrégé

A method for steering a steerable interceptor missile driven by an engine for intercepting a moving target during a midcourse phase of an interception, includes steering the missile with real steering commands produced at respective steering times based on free control parameters formed as a current parameter vector. The free control parameters are constantly and repeatedly optimized during the midcourse phase by an optimization method for optimizing the control parameters. The optimization method is carried out in parallel with the actual steering. Newly detected information about the movement of the target and/or information about the flight of the missile is used in the optimization method as soon as the information is available. Optimized control parameters are accepted into the current parameter vector after being provided by the optimization method. An interceptor missile contains the current parameter vector and a control and evaluation unit for carrying out the method.

Classes IPC  ?

• F42B 10/60 - Dispositions pour le pilotage
• F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles

Abrégé

The invention relates to an optical device (1) for detecting an object scene (11) with an imaging optical system, said optical device comprising an entry optical unit (13) designed to collect incident electromagnetic radiation and a deflection optical unit (16) designed to deflect the electromagnetic radiation from the entry optical unit (13) to at least one detector unit (8), wherein the deflection optical unit (16) and/or the entry optical unit (13) are mounted rotatably about a longitudinal axis (12) of the optical device (1), and the entry optical unit (13) is mounted so as to be pivotable relative to the deflection optical unit (16) about a pitch axis (20) oriented substantially orthogonally to the longitudinal axis (12), wherein the optical device (1) is designed to generate an intermediate image between two optical elements of the deflection optical unit (16), which intermediate image can be imaged onto the at least one detector unit (8) by means of an imaging optical unit, wherein the entry optical unit (13) is designed to focus and/or fold the beam path of the entry optical unit (13) by means of at least one refractive optical element (15).

Classes IPC  ?

• G02B 5/04 - Prismes
• F41G 7/22 - Systèmes autodirecteurs
• G02B 13/00 - Objectifs optiques spécialement conçus pour les emplois spécifiés ci-dessous
• G02B 17/04 - Systèmes catoptriques, p. ex. systèmes redressant et renversant une image utilisant uniquement des prismes
• G02B 17/08 - Systèmes catadioptriques
• G02B 26/02 - Dispositifs ou dispositions optiques pour la commande de la lumière utilisant des éléments optiques mobiles ou déformables pour commander l'intensité de la lumière
• G02F 1/35 - Optique non linéaire

Abrégé

A pulse generator for generating an HPEM pulse includes a Marx generator having a plurality of capacitors that are connected in series between two output poles, providing a Marx voltage between the output poles during operation of the Marx generator. A DS resonator has two input poles and each of the input poles is connected to a respective one of the output poles by a respective supply line. The capacitors are physically disposed along a profile line having two ends at each of which a respective one of the output poles is located. A distance between the output poles is smaller than a longitudinal extent of the Marx generator along the profile line.

Classes IPC  ?

• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
• F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles

Abrégé

The invention relates to an aircraft (2) which has a longitudinal axis (4), two wings (6a, b) which extend along respective wing axes (8a, b), and a folding bearing (10) which is disposed on the longitudinal axis (4) and on which respective bearing ends (14a, b) of the wings (6a, b) are mounted such that the wings can be folded, the wing axes (8a, b) of the wings (6a, b) being oriented along the longitudinal axis (4) in a folded-in packed state (ZP) and said wing axes (8a, b) being oriented obliquely or perpendicularly to the longitudinal axis (4) in a folded-out flight state (ZF), wherein the folding bearing (10) is disposed at the nose (18) of the aircraft (2). A flight system (44) comprises the aircraft (2) and a carrier (42), which has a holding device (40) in or on which the aircraft (2) is or can be stowed in the packed state (ZP) and is removable therefrom. In a method for deploying an aircraft (2) from a carrier (42) moving in a flight direction (F), the aircraft (2) being stowed in or on the carrier (42) in the packed state (ZP), the aircraft (2) is released from the carrier (42) and a pulling element (32) is held on the carrier (42), the aircraft (2) then enters a towed state on account of the air resistance, the wings (6a, b) of the aircraft (2) towed on the pulling element (32) are folded out from the packed state (ZP) into the flight state (ZF) by virtue of the tension at the pulling element (32) caused by the air resistance of the aircraft (2), and the pulling element (32) is released from or hauled in by the aircraft (2).

Classes IPC  ?

• B64C 39/02 - Aéronefs non prévus ailleurs caractérisés par un emploi spécial
• B64D 5/00 - Aéronefs transportés par un aéronef porteur, p. ex. pour être largués ou repris en vol
• B64D 3/00 - Adaptations des aéronefs au remorquage ou à la prise en remorque

Abrégé

A horn antenna for emitting an electromagnetic HPEM microwave pulse along a central axis contains a microwave generator for the pulse having a waveguide along the central axis with a generator opening for the pulse, and a horn structure for shaping the pulse with an input opening and an emission opening for the pulse. The generator contains at least one HPEM source for the pulse. Each HPEM source contains at least two antennas for pulse components, disposed in succession in parallel with the central axis. The pulse is formed as a sum of the pulse components. A method for reconstructing a horn antenna to form the horn antenna with increased power, includes constructively increasing a number of antennas toward a respective HPEM source and orienting remaining antennas in a row relative to the first antenna, increasing the waveguide length, and keeping other dimensions of the horn antenna unchanged.

Classes IPC  ?

• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
• H05B 6/72 - Éléments rayonnants ou antennes
• H05B 6/70 - Lignes pour l'alimentation
• H05B 6/68 - Circuits pour le contrôle ou la commande

Abrégé

In a method for steering a steerable interceptor missile (2) for intercepting a moving target (8), during a midcourse phase (PM) of the interception, which interceptor missile is driven by an engine (10), the interceptor missile (2) is steered with the aid of real steering commands, which are produced at respective steering times on the basis of free control parameters (SP), which free control parameters are in the form of a current parameter vector (10), the free control parameters (SP) are continually and repeatedly optimized during the midcourse phase (PM) with the aid of an optimization method (14) for optimizing the control parameters (SP), the optimization method (14) is carried out in parallel with the actual steering, newly learned information about the movement of the target (8) and/or information about the flight of the interceptor missile (2) is used in the optimization method (14) as soon as said information is available, and optimized control parameters (SP) are accepted into the current parameter vector (10) after said optimized control parameters are provided by the optimization method (14). An interceptor missile (2) contains the current parameter vector (10) and a control and evaluation unit (50) for carrying out the method according to the invention.

Classes IPC  ?

• F41G 7/22 - Systèmes autodirecteurs
• G05D 1/12 - Commande pour la recherche d'un objectif

Abrégé

A method for ascertaining position information for an effector after launching from a launcher of a weapons system including the effector and at least one weapons system unit different from the effector, includes receiving a time synchronization signal at the effector in such a way that the effector and the at least one weapons system unit are temporally synchronized at the latest when the effector is launched. The effector furthermore receives position data of the at least one weapons system unit and a timestamp with unique assignment to the position data through a wireless communication connection after the effector has been launched. Position information is ascertained based on the timestamp, the effector's own time upon receipt of the timestamp, and the position data assigned uniquely to the timestamp. An effector, a computing unit and a weapons system are also provided.

Classes IPC  ?

• F42B 15/01 - Dispositions pour le guidage ou le pilotage sur les projectiles autopropulsés ou les missiles
• F42B 15/08 - Projectiles autopropulsés, p. ex. roquettesMissiles pour le transport d'appareils de mesures

Abrégé

A missile controller guides a missile along a flight path to a stationary or moving target object. The missile controller has at least one side-looking sensor, configured to record surroundings data and has a field of view aligned transverse to the longitudinal axis of the missile, and a control unit having a reception unit for receiving target object data regarding the target object. The target object data containing position data, orientation data and/or speed data of the target object. The control unit is configured to set the orientation of the missile during the guidance at least partly based on the received target object data such that the target object is located in the field of view of the side-looking sensor at least in sections of a final guidance phase.

Classes IPC  ?

• F41G 7/22 - Systèmes autodirecteurs
• G06T 7/20 - Analyse du mouvement
• G06T 7/70 - Détermination de la position ou de l'orientation des objets ou des caméras
• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés

Abrégé

A method for controlling at least one missile radar sensor moving along a trajectory with a missile. The missile radar sensor is set up to recognize a target object. The operating parameters for modulation of the missile radar sensor are adaptively adjusted during the movement along the trajectory depending on target object data on the target object.

Classes IPC  ?

• F41G 7/22 - Systèmes autodirecteurs
• G01S 13/88 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques

Abrégé

A missile, in particular a guided missile, has a missile body and a radar sensor unit for acquiring a target object. The radar sensor unit contains at least one radar antenna, strip-shaped in the longitudinal direction, that is mounted or integrated on a circumferential surface of the missile body such that the longitudinal direction of the at least one strip-shaped radar antenna is aligned in the direction of the missile longitudinal axis.

Classes IPC  ?

• F41G 7/22 - Systèmes autodirecteurs
• G01S 7/03 - Détails de sous-ensembles HF spécialement adaptés à ceux-ci, p. ex. communs à l'émetteur et au récepteur
• H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons

Produits et services

Launchers for missiles; containers for launching weapons; containers for storing weapons; ballistic weapons; rocket-propelled ballistic missiles; launchers for missiles [weapons]; infrared defence rocket warheads; guided missiles; air-to-air missiles; air-to-surface missiles; cruise missiles; projectiles [weapons]; rocket launchers; rockets [projectiles]; explosive devices; blasting explosives; weapon systems; weapons for launching missiles; weapons for launching missiles and projectiles; weapons for launching projectiles; motorized weapons.

Abrégé

A fragmentation system for electrodynamic fragmentation of material contains a feed and an outlet for transporting material along a transport path in a transport direction. At least one high-voltage pulse source is provided, each of the high-voltage pulse sources contains at least one first electrode and at least one second electrode for generating a high-voltage discharge in a discharge chamber. The transport path has a fractionation section, and the fractionation section extends through the discharge chamber. A selection device for selectively extracting the material on the transport path is provided in order to channel material and/or fragments of the material having a diameter smaller than a minimum diameter past at least one portion of one of the fractionation sections.

Classes IPC  ?

• B02C 19/18 - Utilisation d'effets physiques auxiliaires aidant la désagrégation, p. ex. ultrasons, irradiation
• B02C 23/10 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen d'un séparateur situé dans le passage de décharge de la zone de broyage ou de désagrégation
• B02C 23/14 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen de plusieurs séparateurs
• B02C 23/38 - Addition de fluide, dans un but autre que celui de broyer ou de désagréger par l'énergie du fluide dans des appareils comportant plusieurs zones de broyage ou de désagrégation

Produits et services

Calculators; Computer systems; Monitoring instruments; Apparatus for the processing of images; Image analyzers; Programs and software for image processing; Computer software to enable the provision of information via communications networks; Computer software for mobile applications that enable interaction and interface between vehicles and mobile devices; Computer programmes for data processing; Interfaces for computers; Interfaces for computers; Interfaces for computers; Interfaces for detectors; Sensor interfaces; Protective assistance systems; Computer software for weapons systems; Software for networked components of a weapons system; All the aforesaid goods in particular being designed for networking within a weapons system. Vehicles adapted for military purposes; Drones; Military drones; Unmanned aeroplanes; Military aircraft; All the aforesaid goods in particular being designed for networking within a weapons system. Launchers for missiles; Ballistic weapons; Rocket-propelled ballistic missiles; Naval gun fire predictors; Launchers for missiles [weapons]; Guided missiles; Air-to-air missiles; Air-to-surfaces missiles; Cruise missiles; Projectiles [weapons]; Rocket launchers; Rockets; Weapons for launching missiles; Weapons for launching missiles and projectiles; Weapons for launching projectiles; Motorized weapons; Weapon systems; Weapons systems comprising of one or more of the aforesaid goods; All the aforesaid goods in particular being designed for networking with one or more of the aforesaid goods. Computer aided transmission of messages; Computer aided transmission of images; Transmission of information by electronic communications networks; In particular the aforesaid services for military purposes. Engineering and computer-aided engineering services; Engineering services relating to computer programming; Engineering services in the field of communications technology; Advisory services relating to man-machine interfaces for computer software; Design and development of data processing software; Development of programmes for data processing; Development of computer programs; Development of computer programs; Updating of software for data processing; In particular the aforesaid services for military purposes.

Produits et services

Launchers for missiles; containers for launching weapons; containers for storing weapons; ballistic weapons; rocket-propelled ballistic missiles; guided missiles; air-to-air missiles; cruise missiles; projectiles [weapons]; explosive devices; blasting explosives; motorized weapons; weapon systems.

Produits et services

Launchers for missiles; Containers for launching weapons; Containers for storing weapons; Ballistic weapons; Rocket-propelled ballistic missiles; Launchers for missiles [weapons]; Infrared defence rocket warheads; Guided missiles; Air-to-air missiles; Air-to-surfaces missiles; Cruise missiles; Projectiles [weapons]; Rocket launchers; Rockets [projectiles]; Explosive devices; Blasting explosives; Weapon systems; Weapons for launching missiles; Weapons for launching missiles and projectiles; Weapons for launching projectiles; Motorized weapons.

Abrégé

The invention relates to a radar antenna (14, 14', 14''). According to the invention, in order to reduce an optical aperture in the presence of a radar antenna (14, 14', 14'') oriented forwards, the radar antenna (14, 14', 14'') is designed as an optically transparent metallic covering which is shaped as an antenna and is applied to an optically transparent body (12).

Classes IPC  ?

• H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
• H01Q 1/38 - Forme structurale pour éléments rayonnants, p. ex. cône, spirale, parapluie formés par une couche conductrice sur un support isolant
• H01Q 1/40 - Éléments rayonnants recouverts avec, ou enrobés d'une matière protectrice
• H01Q 5/22 - Gammes d’ondes radio combinées à des gammes d’ondes en dehors du spectre radio, p. ex. infrarouges ou optiques
• H01Q 9/04 - Antennes résonnantes
• H01Q 21/06 - Réseaux d'unités d'antennes, de même polarisation, excitées individuellement et espacées entre elles

Produits et services

Launchers for missiles; containers in the nature of cases specially adapted for launching weapons thereof; containers in the nature of cases specially adapted for storing weapons; ballistic weapons; rocket-propelled ballistic missiles; guided missiles; air-to-air missiles; cruise missiles; projectiles being weapons; blasting explosives; motorized weapons, namely, motorized missiles, self-propelled missiles and projectile weapons propelled by rocket engines; and weapon systems comprising launchers for missiles, ballistic weapons, rocket-propelled ballistic missiles, guided missiles, air-to-air missiles, cruise missiles, projectiles being weapons, blasting explosives, motorized missiles, self-propelled missiles, and projectile weapons propelled by rocket engines

Produits et services

Devices for transmitting pulsed high-frequency electromagnetic radiation; Devices for emitting high-frequency microwave radiation for interrupting electric circuits and electronics; Vehicles with devices for transmitting pulsed high-frequency electromagnetic radiation; Vehicles with devices for emitting high-frequency microwave radiation for interrupting electric circuits and electronics.

Produits et services

Devices for transmitting pulsed high-frequency electromagnetic radiation; Devices for emitting high-frequency microwave radiation for interrupting electric circuits and electronics, All the aforesaid apparatus based on defence and military equipment.

Produits et services

Devices for transmitting pulsed high-frequency electromagnetic radiation; Devices for emitting high-frequency microwave radiation for interrupting electric circuits and Electronics.

Produits et services

Drones, In particular small drones or coaxial drones; Unmanned aeroplanes; Unmanned aircraft or drones for combating battle tanks with projectile forming loads; Drones for combating targets with blast forming or chip forming loads; Drones for transferring or projecting pyrotechnic loads.

Produits et services

Drones, In particular small drones or coaxial drones; Unmanned aeroplanes; Unmanned aircraft or drones for combating battle tanks with projectile forming loads; Drones for combating targets with blast forming or chip forming loads; Drones for transferring or projecting pyrotechnic loads.

Abrégé

The invention relates to a method for determining a target (36), in which method an image (28) illustrating the target (36) is specified and a target identification unit (18) identifies the illustrated target (36) as such from image features of the image (28) and predefined classifiers (56). According to the invention, in order to determine targets reliably, the target identification unit (18) determines new classifiers (66) from the image (28) using knowledge of the target (36), by means of which classifiers the target (36) is identifiable as such with a greater identification accuracy than with the classifiers (56) used for identification.

Classes IPC  ?

• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés
• F41G 7/22 - Systèmes autodirecteurs
• G06T 7/73 - Détermination de la position ou de l'orientation des objets ou des caméras utilisant des procédés basés sur les caractéristiques
• G06K 9/32 - Alignement ou centrage du capteur d'image ou de la zone image
• G06K 9/46 - Extraction d'éléments ou de caractéristiques de l'image

Abrégé

A high-power electromagnetic source for HPEM pulses in a desired radiation direction includes at least three antennas fixed in relation to one another for pulse components, wherein at least two groups of antennas with a respective main direction are present, and a control unit for the activation and phase position of the pulse components for the superimposition for the HPEM pulse, wherein the current radiation direction of said pulse is selectable in an angle range around the main direction. A vehicle with an HPEM source has the antennas mounted in a fixed position or a support for the antennas is pivotably mounted on the vehicle. In a method for emitting the HPEM pulse, all antennas are controlled in order to select the radiation direction in the angle range of less than 360°.

Classes IPC  ?

• G01S 7/282 - Émetteurs
• G01S 13/931 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour prévenir les collisions de véhicules terrestres
• H01Q 3/06 - 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 pour faire varier une coordonnée de l'orientation dans un angle limité
• 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
• H01Q 15/14 - Surfaces réfléchissantesStructures équivalentes
• H01Q 21/29 - Combinaisons d'unités d'antennes de types différents interagissant entre elles pour donner une caractéristique directionnelle désirée
• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
• G01S 13/72 - Systèmes radar de poursuiteSystèmes analogues pour la poursuite en deux dimensions, p. ex. combinaison de la poursuite en angle et de celle en distance, radar de poursuite pendant l'exploration

Produits et services

Launchers for missiles; Containers for launching weapons; Containers for storing weapons; Ballistic weapons; Rocket-propelled ballistic missiles; Guided missiles; Air-to-air missiles; Cruise missiles; Projectiles [weapons]; Explosive devices; Blasting explosives; Motorized weapons; Weapon systems.

Produits et services

Launchers for missiles; Containers for launching weapons; Containers for storing weapons; Ballistic weapons; Rocket-propelled ballistic missiles; Guided missiles; Air-to-air missiles; Cruise missiles; Projectiles [weapons]; Explosive devices; Blasting explosives; Motorized weapons; Weapon systems.

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles.

Produits et services

Firearms, artillery guns, ammunition, intelligent munitions, guided munitions, artillery projectiles.

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles; mortar artillery projectiles.

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles; marine artillery projectiles.

Abrégé

A device produces an arming criterion for a fuze for a partly spinning munition. The munition has a first part which spins and a second part without or with little spin during flight of the munition. The device includes a sensor for outputting a characteristic variable for a relative rotation between the first part and the second part and a control unit for producing the arming criterion when the characteristic variable fulfils a flying criterion. The fuze for the partly spinning munition, which has at least one arming criterion, includes the device for providing the arming criterion or one of the arming criteria. The partly spinning munition includes the fuze with the device.

Classes IPC  ?

• F42C 15/40 - 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 s'effectue électriquement
• F42C 15/26 - 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 en utilisant la force centrifuge

Produits et services

Systems and kits for guidance and for increasing the range of missiles and bombs; terminal flight path controls for missiles and bombs. Air-to-surfaces missiles; bombs; containers for launching weapons; containers for storing weapons; conventional air delivered weapons; guided bombs; guided missiles; guided weapons; launchers for missiles; launchers for missiles [weapons]; missiles; weapon systems; weapons; weapons for launching missiles; weapons for launching missiles and projectiles.

Abrégé

The invention relates to a projectile hull (2) comprising a hull body (4) enclosing an inner space (6), with at least one predetermined breaking point (10) for weakening and breakdown into fragments (12), said projectile hull being produced by 3D printing and the predetermined breaking point (10) being formed such that the reactant (16) is not compacted or is only slightly compacted, and/or only a little or no reactant (16) is provided, wherein the hull body (4) has a continuous inner wall (20) and/or outer wall (22) on the predetermined breaking point (10). According to a method for producing the projectile hull (2), the reactant (16) is provided and the hull body (4) is produced by means of 3D printing, wherein the predetermined breaking point (10) is formed as described, and a continuous inner wall (20) and/or outer wall (22) is produced on the predetermined breaking point (10).

Classes IPC  ?

• F42B 12/24 - 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 du type à explosif brisant à structure de corps de fragmentation l'enveloppe du projectile présentant des rainures, des cannelures ou d'autres affaiblissements
• F42B 12/32 - 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 du type à explosif brisant à structure de corps de fragmentation l'enveloppe ou la paroi du projectile contenant un ensemble de corps individuels encastrés, p. ex. de sphères en acier

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles; marine artillery projectiles

Produits et services

Firearms, artillery guns, ammunition, intelligent munitions, guided munitions, artillery projectiles

Produits et services

Firearms; artillery guns; ammunition; intelligent munitions; guided munitions; artillery projectiles; mortar artillery projectiles

Abrégé

In a method for generating a transillumination signal of a section of the subsurface, an HPEM radiation source radiates an electromagnetic pulse into the section for the purpose of exciting electromagnetically reactive structures to emit an electromagnetic response signal. For the pulse, a pulse duration of at most 500 ns, a center frequency in the range between 10 MHz and 10 GHz, and a bandwidth in the range from 10% to 150% of the center frequency is set. The transillumination signal is formed as the sum of response signals received at a measuring location. In a method for detecting a cavity in the subsurface, the above method is carried out, and the structures are detected from the transillumination signal with the aid of a detection method, and the cavity is detected if the structures satisfy a detection criterion.

Classes IPC  ?

• G01S 7/282 - Émetteurs
• G01S 13/88 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques
• G01V 3/12 - Prospection ou détection électrique ou magnétiqueMesure des caractéristiques du champ magnétique de la terre, p. ex. de la déclinaison ou de la déviation fonctionnant par ondes électromagnétiques
• A61B 5/00 - Mesure servant à établir un diagnostic Identification des individus
• G01N 22/00 - Recherche ou analyse des matériaux par l'utilisation de micro-ondes ou d'ondes radio, c.-à-d. d'ondes électromagnétiques d'une longueur d'onde d'un millimètre ou plus
• G01N 21/47 - Dispersion, c.-à-d. réflexion diffuse

Abrégé

A radiation source for emitting an electromagnetic HPEM microwave pulse contains a microwave generator for generating the pulse. The generator has a generator opening for outputting the pulse. A horn structure is provided for shaping the pulse. The horn structure has an input opening, which is connected to the generator opening and is intended to radiate in the pulse, and an emission opening for emitting the shaped pulse. The generator contains at least two pulse sources for respectively generating a pulse component. The pulse is the sum of the pulse components. A radiation device contains such a radiation source and a control device for triggering the pulse sources in a temporally synchronized manner for the purpose of respectively emitting a pulse component.

Classes IPC  ?

• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs

Abrégé

A launcher device for launching ammunition or weapons provided with primers, contains a plurality of launch tubes combined so as to form a launcher battery. Each of the launch tubes is loaded with ammunition or a weapon, and each of the launch tubes is closed off by a cover. A device is provided for detecting damage to the covers closing off the launch tubes.

Classes IPC  ?

• F41F 3/077 - Panneaux de fermeture ou couvercles pour des tubes de lancement
• F41F 3/042 - Lanceurs de roquettes ou de torpilles pour roquettes servant en même temps de conteneur pour le transport de la roquette

Abrégé

The invention relates to a fragmentation system (1) for an electrodynamic fragmentation of material (5), comprising a feed (3) and an outlet (4) for transporting material along a transport path (8) in a transport direction (9), comprising at least one high-voltage pulse source (11), wherein each of the high-voltage pulse sources (11) has at least one first electrode (10a) and at least one second electrode (10b) for generating a high-voltage discharge (19) in a discharge chamber, and the transport path (8) has a fractionation section (18), said fractionation section (18) running through the discharge chamber. The fragmentation system also comprises a selection means for a selective discharge of the material (5) on the transport path in order to extract material (5) and/or fragments of the material with a diameter which is smaller than a minimum diameter at at least one part of one of the fractionation sections (18). In a method for an electrodynamic fragmentation of material (5), material (5) is transported from an inlet (3) to an outlet (4) along a transport path (9). The transport path (8) has a fractionation section (18), at least one high-voltage pulse source (11) has at least one first electrode (10a) and at least one second electrode (10b), and the high-voltage pulse source (11) generate a high-voltage discharge in a discharge chamber, said discharge chamber being arranged between the first electrode (10a) and the second electrode (10b). Material (5) and/or fragments of the material with a diameter which is smaller than a minimum diameter is extracted at at least one part of one of the fractionation sections (18).

Classes IPC  ?

• B02C 19/18 - Utilisation d'effets physiques auxiliaires aidant la désagrégation, p. ex. ultrasons, irradiation
• B02C 23/10 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen d'un séparateur situé dans le passage de décharge de la zone de broyage ou de désagrégation
• B02C 23/14 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen de plusieurs séparateurs
• B02C 23/38 - Addition de fluide, dans un but autre que celui de broyer ou de désagréger par l'énergie du fluide dans des appareils comportant plusieurs zones de broyage ou de désagrégation

Abrégé

The invention relates to a fragmentation system (1) for an electrodynamic fragmentation of material (5), comprising a feed (3) and an outlet (4) for transporting material along a transport path (8) in a transport direction (9), comprising at least one high-voltage pulse source (11), wherein each of the high-voltage pulse sources (11) has at least one first electrode (10a) and at least one second electrode (10b) for generating a high-voltage discharge (19) in a discharge chamber, and the transport path (8) has a fractionation section (18), said fractionation section (18) running through the discharge chamber. The fragmentation system also comprises a selection means for a selective discharge of the material (5) on the transport path in order to extract material (5) and/or fragments of the material with a diameter which is smaller than a minimum diameter at at least one part of one of the fractionation sections (18). In a method for an electrodynamic fragmentation of material (5), material (5) is transported from an inlet (3) to an outlet (4) along a transport path (9). The transport path (8) has a fractionation section (18), at least one high-voltage pulse source (11) has at least one first electrode (10a) and at least one second electrode (10b), and the high-voltage pulse source (11) generate a high-voltage discharge in a discharge chamber, said discharge chamber being arranged between the first electrode (10a) and the second electrode (10b). Material (5) and/or fragments of the material with a diameter which is smaller than a minimum diameter is extracted at at least one part of one of the fractionation sections (18).

Classes IPC  ?

• B02C 19/18 - Utilisation d'effets physiques auxiliaires aidant la désagrégation, p. ex. ultrasons, irradiation
• B02C 23/10 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen d'un séparateur situé dans le passage de décharge de la zone de broyage ou de désagrégation
• B02C 23/14 - Séparation ou triage de matériaux, associé au broyage ou à la désagrégation au moyen de plusieurs séparateurs
• B02C 23/38 - Addition de fluide, dans un but autre que celui de broyer ou de désagréger par l'énergie du fluide dans des appareils comportant plusieurs zones de broyage ou de désagrégation

Abrégé

A munition module includes an ignition point of an explosive configuration positioned away from a detonator within a casing of the explosive configuration. In an initial state, an ignition channel runs from the detonator to the ignition point. The ignition channel is formed so as to be open in an initial state and self-sealing in an exploded state after a detonation has taken place. A warhead with the munition module contains an active covering which at least partially surrounds the explosive configuration and can be accelerated by the reacted explosive. In a munition having the warhead, the detonator is an impact detonator. A munition in the form of an air-burst munition contains the warhead.

Classes IPC  ?

• F42C 19/08 - AmorcesDétonateurs
• F42B 12/20 - 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 du type à explosif brisant

Abrégé

The invention relates to a method for determining characteristic-curve correction factors a matrix detector that images in the infrared spectral range. A good image correction can be obtained by virtue of an area of homogeneous temperature being recorded at two different temperatures by the matrix detector, there being two images with different integration times for each temperature. A signal gradient over the integration time is established for each of the pixels from the four pixel values at the two temperatures in each case and the gain being established from the difference of the signal gradients and characteristic-curve correction factors for the gain being stored.

Classes IPC  ?

• G01J 5/00 - Pyrométrie des radiations, p. ex. thermométrie infrarouge ou optique
• F41G 7/22 - Systèmes autodirecteurs
• H04N 5/33 - Transformation des rayonnements infrarouges
• H04N 5/357 - Traitement du bruit, p.ex. détection, correction, réduction ou élimination du bruit
• H04N 17/00 - Diagnostic, test ou mesure, ou leurs détails, pour les systèmes de télévision
• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés
• G01S 3/78 - Radiogoniomètres pour déterminer la direction d'où proviennent des ondes infrasonores, sonores, ultrasonores ou électromagnétiques ou des émissions de particules sans caractéristiques de direction utilisant des ondes électromagnétiques autres que les ondes radio
• G01J 5/22 - Leurs particularités électriques

Produits et services

Firearms, Artillery guns, Ammunition, Intelligent munitions, guided munitions, artillery projectiles, Marine artillery projectiles.

Produits et services

Firearms, Artillery guns, Ammunition, Intelligent munitions, guided munitions, artillery projectiles, Mortar artillery projectiles.

Produits et services

Firearms, Artillery guns, Ammunition, Intelligent munitions, guided munitions, artillery projectiles.

Produits et services

Firearms, Artillery guns, Ammunition, Intelligent munitions, guided munitions, artillery projectiles.

Produits et services

Systems and kits for guidance and for increasing the range of missiles and bombs; Terminal flight path controls for missiles and bombs. Air-to-surfaces missiles; Bombs; Containers for launching weapons; Containers for storing weapons; Conventional air delivered weapons; Guided bombs; Guided missiles; Guided weapons; Launchers for missiles; Launchers for missiles [weapons]; Missiles; Weapon systems; Weapons; Weapons for launching missiles; Weapons for launching missiles and projectiles.

Abrégé

The invention relates to an aerial vehicle (2) for countering drones, comprising a drive (4) and a housing (8) around said drive (4) and an active component (18) for damaging a drone (32). A precise approach towards the drone (32) can be achieved if the aerial vehicle (2) has a seeker head (12) with an optical viewfinder (14) and a control unit (10) for drone detection, for controlling approach towards the detected drone (32) and for triggering the active component (18).

Classes IPC  ?

• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
• F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles
• 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 12/62 - Munitions en grappes ou munitions-cargo, c.-à-d. projectiles portant un seul ou plusieurs sous-projectiles les sous-projectiles étant éjectés dans une direction parallèle à l'axe longitudinal du projectile porteur

Produits et services

Electronic navigational and positioning apparatus and instruments; Satellite navigational apparatus and parts therefor; Software for satellite navigation systems; global navigation satellite system (GNSS) apparatus and parts therefor; GPS apparatus and parts therefor; global navigation satellite system (GNSS) based receivers and parts therefor; GPS-based receivers and parts therefor; Electronic protection systems for global navigation satellite system (GNSS) receivers comprising antenna arrays, electronic filters and digital processing units for global navigation satellite system (GNSS) receivers; Antennas; High-frequency antennas; Antenna arrays; global navigation satellite system (GNSS) antenna arrays; Antenna cables; Computer software for creating and executing computational protection algorithms in time, frequency and space domain to ensure access to global navigation satellite systems (GNSS)

Produits et services

Electronic navigational and positioning apparatus and instruments; Satellite navigational apparatus and parts therefor; Software for satellite navigation systems; global navigation satellite system (GNSS) apparatus and parts therefor; GPS apparatus and parts therefor; global navigation satellite system (GNSS) based receivers and parts therefor; GPS-based receivers and parts therefor; Electronic protection systems for global navigation satellite system (GNSS) receivers comprising antenna arrays, electronic filters and digital processing units for global navigation satellite system (GNSS) receivers; Antennas; High-frequency antennas; Antenna arrays; global navigation satellite system (GNSS) antenna arrays; Antenna cables; Computer software for creating and executing computational protection algorithms in time, frequency and space domain to ensure access to global navigation satellite systems (GNSS)

Abrégé

In a method for protecting a networked military system from malicious users, transactions between the users of the networked military system are stored in a distributed database. Using a block chain method makes it possible to securely store important information in the network and to protect it from manipulation by intruders.

Classes IPC  ?

• G06F 21/62 - Protection de l’accès à des données via une plate-forme, p. ex. par clés ou règles de contrôle de l’accès
• H04L 29/06 - Commande de la communication; Traitement de la communication caractérisés par un protocole

Produits et services

Electronic navigational and positioning apparatus and instruments; Satellite navigational apparatus and parts therefor; Software for satellite navigation systems; GNSS apparatus and parts therefor; GPS apparatus and parts therefor; GNSS-based receivers and parts therefor; GPS-based receivers and parts therefor; Electronic protection systems for GNSS receivers; Antennas; Radio-frequency antennas; Aerial matrices; GNSS antenna arrays; Antenna cables; Software. Installation, repair and maintenance relating to navigation and positioning apparatus and instruments, satellite navigational apparatus and parts therefor, GNSS apparatus and parts therefor, GPS apparatus and parts therefor, GNSS-based receivers and parts therefor, GPS-based receivers and parts therefor, electronic protection systems for GNSS receivers, aerials, radio-frequency antennas, antenna arrays, GNSS antenna arrays and aerial cables. Software development, programming and implementation; IT consultancy and information.

Produits et services

Electronic navigational and positioning apparatus and instruments; Satellite navigational apparatus and parts therefor; Software for satellite navigation systems; GNSS apparatus and parts therefor; GPS apparatus and parts therefor; GNSS-based receivers and parts therefor; GPS-based receivers and parts therefor; Electronic protection systems for GNSS receivers; Antennas; Radio-frequency antennas; Aerial matrices; GNSS antenna arrays; Antenna cables; Software. Installation, repair and maintenance relating to navigation and positioning apparatus and instruments, satellite navigational apparatus and parts therefor, GNSS apparatus and parts therefor, GPS apparatus and parts therefor, GNSS-based receivers and parts therefor, GPS-based receivers and parts therefor, electronic protection systems for GNSS receivers, aerials, radio-frequency antennas, antenna arrays, GNSS antenna arrays and aerial cables. Software development, programming and implementation; IT consultancy and information.

Abrégé

The invention relates to a munition module (6) in which an ignition point (18) of an explosive assembly is positioned at a distance from a detonator (8) within a casing (20) of the explosive assembly (10). An ignition channel (22) runs from the detonator (8) to the ignition point (18) in a starting state (A), wherein the ignition channel (22) is open in a starting state (A) and is designed to be self-closing in an ignition state (S) after an ignition has occurred. A warhead (4) comprising the munition module (6) contains an active coating (12) which at least partly surrounds the explosive assembly (10) and which can be accelerated by the reacted explosive. In a munition (2) comprising the warhead (4), the detonator is an impact detonator. A munition (2) in the form of an air-burst munition contains the warhead (4).

Classes IPC  ?

• F42C 19/08 - AmorcesDétonateurs
• F42B 12/20 - 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 du type à explosif brisant

Abrégé

+) radical, is reacted with a dinitromethane anion. The reaction of the isourea derivative cation with the dinitromethane anion takes place in a solution.

Classes IPC  ?

• C07C 209/68 - Préparation de composés contenant des groupes amino liés à un squelette carboné à partir d'amines, par des réactions n'impliquant pas de groupes amino, p. ex. réduction d'amines non saturées, aromatisation ou substitution du squelette carboné
• C07C 209/60 - Préparation de composés contenant des groupes amino liés à un squelette carboné par des réactions de condensation ou d'addition, p. ex. réaction de Mannich, addition d'ammoniac ou d'amines à des alcènes ou à des alcynes ou addition de composés, contenant un atome d'hydrogène actif, à des bases de Schiff, à des quinone-imines ou à des aziranes

Abrégé

In a method for synthesizing 1,1-diamino-2,2-dinitroethylene (FOX-7) or an N-substituted diamino derivative thereof or a salt of 1,1-diamino-2,2-dinitroethylene or of the N-substituted diamino derivative, a carbodiimide is reacted with a dinitromethane anion. The reaction of the carbodiimide with the dinitromethane anion takes place in a solution.

Classes IPC  ?

• C07C 209/68 - Préparation de composés contenant des groupes amino liés à un squelette carboné à partir d'amines, par des réactions n'impliquant pas de groupes amino, p. ex. réduction d'amines non saturées, aromatisation ou substitution du squelette carboné
• C07C 211/09 - Diamines
• C07C 211/15 - Composés contenant des groupes amino liés à un squelette carboné ayant des groupes amino liés à des atomes de carbone acycliques d'un squelette carboné saturé acyclique le squelette carboné étant substitué de plus par des atomes d'halogène ou par des groupes nitro ou nitroso
• C07C 267/00 - Diimides carboniques
• C07C 209/60 - Préparation de composés contenant des groupes amino liés à un squelette carboné par des réactions de condensation ou d'addition, p. ex. réaction de Mannich, addition d'ammoniac ou d'amines à des alcènes ou à des alcynes ou addition de composés, contenant un atome d'hydrogène actif, à des bases de Schiff, à des quinone-imines ou à des aziranes
• C07C 211/24 - Composés contenant des groupes amino liés à un squelette carboné ayant des groupes amino liés à des atomes de carbone acycliques d'un squelette carboné acyclique et non saturé le squelette carboné étant substitué de plus par des atomes d'halogène ou par des groupes nitro ou nitroso

Abrégé

A system of missile control surfaces includes a control surface housing, a control surface shaft which is rotatably mounted in the control surface housing, a control surface secured on the control surface shaft, a control surface drive and a coupling unit. The coupling unit couples the control surface drive to the control surface shaft in such a way that a movement of the control surface drive produces a rotation of the control surface shaft. To enable high forces to be applied reliably to a guided missile control surface, it is proposed that the coupling unit has at least one flexible tension element, which is secured on the control surface drive and is rolled up onto the control surface shaft to a certain extent.

Classes IPC  ?

• F42B 15/01 - Dispositions pour le guidage ou le pilotage sur les projectiles autopropulsés ou les missiles
• F42B 10/64 - Pilotage par le déplacement de surfaces portantes d'ailettes de pilotage

Abrégé

A method for identifying an object in a search image, in which the object and surroundings around the object are recorded by an optics unit of a camera. The optics unit is swivelled in the surroundings during the integration of a recorded image and an image processing unit back calculates the search image from the recorded image using the point spread function and the swivelling movement of the optics unit. Then the search image is searched and the object is identified in the search image.

Classes IPC  ?

• H04N 5/225 - Caméras de télévision
• H04N 5/77 - Circuits d'interface entre un appareil d'enregistrement et un autre appareil entre un appareil d'enregistrement et une caméra de télévision
• G06T 7/00 - Analyse d'image
• G06T 7/70 - Détermination de la position ou de l'orientation des objets ou des caméras

Abrégé

A defense device for combating an unmanned aircraft includes a communications device configured for receiving communications information transmitted by at least one external signal source, an emitting device configured for producing and emitting a high-energy electromagnetic pulse in the event of triggering of the emitting device, and a control device configured to trigger the emission of the high-energy electromagnetic pulse depending on communications information received by the communications device. A protective configuration for combating an unmanned aircraft and a method for operating a protective configuration are also provided.

Classes IPC  ?

• F41H 13/00 - Moyens d'attaque ou de défense non prévus ailleurs
• F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles

Produits et services

Drone defence systems; Electric components for controlling operating procedures in drone defence systems; Electric components for detecting or verifying or combating drones; Electric devices for emitting high-frequency electromagnetic radiation; Optical apparatus and instruments; Measuring, signalling and supervision apparatus and instruments; Apparatus for recording, transmission or reproduction of sound or images; Digital recording media; Data processing equipment; Computers; Computer software; Alarms; Testing apparatus not for medical purposes; Antennas; Distance recording apparatus; Azimuth instruments; Observation instruments; Computer operating programs; Peripherals adapted for use with computers; Computer programs; Computer keyboards; Data processing apparatus; Detectors; Electronic notice boards; Audio- and video-receivers; Distance measuring apparatus; Remote control apparatus; Frequency meters; Masts for wireless aerials; Global Positioning System [GPS] apparatus; High-frequency apparatus; Altimeters; Interfaces (for computers); Directional compasses; Laptop computers; Microphones; Note books; Optical lenses; Radar apparatus; Radios; Sound locating instruments; Transmitters; Simulators for the steering and control of vehicles; Spectroscopes; Camcorders; Time recording apparatus; The aforesaid goods not including circuit breakers or goods directly associated with circuit breakers. Vehicles. Installation, namely installation or assembly of drone defence systems, components for controlling operating procedures in drone defence systems or components for detecting or verifying or combating drones. Providing of training. Technological services and research; Design and development of computer hardware and software; Updating of computer software; Installation of software; Computer software design; Software maintenance; Engineering services; Construction drafting; Studies (technical project-). Security services for the protection of property and individuals; Physical security consultancy; Guard services; Monitoring of burglar and security alarms.

Abrégé

The invention proceeds from a method for classifying a vehicle (2), in which an image (8) of the vehicle (2) is recorded (6), characteristic image features are established (12) from the image (8), the characteristic image features are compared (20) to features from a vehicle database (16), said vehicle database containing a multiplicity of descriptions of various vehicle classes containing characteristic features, and the recorded vehicle (2) is assigned (26) to a vehicle class described in the vehicle database (16). In order to enable a quick classification, it is proposed that key points in the image (8) of the vehicle (2) are established (12) as characteristic image features and at least one multi-dimensional vehicle descriptor is established for each key point.

Classes IPC  ?

• 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

Abrégé

The invention relates to a genuine-material test piece for training explosives sniffer dogs, wherein the genuine-material test piece comprises an explosive in a solid or liquid carrier material contained in a housing (12) comprising an interior space (18) and a closure (10) for the reversible gastight closure of the interior space (18) or of a space comprising the interior space (18), wherein the carrier material with the explosive is contained in the interior space (18), wherein the genuine-material test piece also comprises a gas-permeable means for preventing the carrier material from escaping from the interior space (18) when the interior space (18) of the space is not closed in a gastight manner by means of the closure (10).

Classes IPC  ?

• A01K 15/00 - Dispositifs pour le dressage des animaux, p. ex. nasières ou entravesDispositifs pour renverser les animaux en généralÉquipement pour l'entraînement ou l'exerciceCabines pour saillies
• A61L 9/04 - Désinfection, stérilisation ou désodorisation de l'air utilisant des substances gazeuses ou à l'état de vapeur, p. ex. de l'ozone utilisant des substances évaporées dans l'air sans chauffage
• A01K 15/02 - Équipement pour l'entraînement ou l'exercice, p. ex. labyrinthes pour animaux

Abrégé

A seeker head for a guided missile has an outer casing, a detector unit with a matrix detector, and an optical system for depicting an object from an object scene surrounding the guided missile on the matrix detector. The optical system contains entrance optics and an optical link. The seek head further has a rolling-pitching system with a rolling frame and a pitching frame for aligning at least the entrance optics with the object. In order to be able to detect even objects that are far away and radiating weakly when the guided missile is rolling, it is proposed that the detector unit is arranged on the rolling frame for conjoint rolling.

Classes IPC  ?

• F41G 7/22 - Systèmes autodirecteurs
• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés

Abrégé

A cooling device for cooling a detector element disposed in a jacket cavity of a Dewar vessel uses a Joule-Thomson cooler with an expansion nozzle that opens into an expansion chamber. The cooling device includes a final control element that is adjustable depending on temperature for influencing the flow through the expansion nozzle. A first temperature sensor is disposed in the expansion chamber and a second temperature sensor is disposed within the Dewar vessel outside the expansion chamber. The cooling device includes a control device that is configured for detecting a temperature gradient from sensor values of the first temperature sensor and of the second temperature sensor and for adjusting the final control element depending on the detected temperature gradient.

Classes IPC  ?

• F25B 9/00 - Machines, installations ou systèmes à compression dans lesquels le fluide frigorigène est l'air ou un autre gaz à point d'ébullition peu élevé
• F25B 9/02 - Machines, installations ou systèmes à compression dans lesquels le fluide frigorigène est l'air ou un autre gaz à point d'ébullition peu élevé utilisant l'effet Joule-ThompsonMachines, installations ou systèmes à compression dans lesquels le fluide frigorigène est l'air ou un autre gaz à point d'ébullition peu élevé utilisant l'effet vortex
• F25B 19/00 - Machines, installations ou systèmes utilisant l'évaporation d'un frigorigène mais sans récupération de vapeur
• F16K 31/02 - Moyens de fonctionnementDispositifs de retour à la position de repos électriquesMoyens de fonctionnementDispositifs de retour à la position de repos magnétiques

Abrégé

A method for operating a ground-based anti-aircraft system includes providing a group of main system components containing a sensor system, a tactical operation control and an effector system. Combat target sensor data are passed from the sensor system to the tactical operation control, processed therein and passed in processed form from the tactical operation control to the effector system, using the data to combat the target. A central integration module having a converter unit and a central data distributor allows differently constructed main system components to be connected. Data from all main system components are routed to the central data distributor by the converter unit and converted therein from component protocol into system-internal data protocol, and passed from the central data distributor to one or more main system components, through the converter unit, converting the distributed data back from system-internal data protocol into component protocol.

Classes IPC  ?

• G05B 13/02 - Systèmes de commande adaptatifs, c.-à-d. systèmes se réglant eux-mêmes automatiquement pour obtenir un rendement optimal suivant un critère prédéterminé électriques
• G06F 17/00 - Équipement ou méthodes de traitement de données ou de calcul numérique, spécialement adaptés à des fonctions spécifiques
• F41H 11/02 - Installations ou systèmes de défense anti-aérienne ou antimissiles
• F41G 3/04 - Dispositifs de pointage pour la dispersion du tir d'une batterie
• G05B 15/02 - Systèmes commandés par un calculateur électriques
• F41G 7/00 - Systèmes de commande de guidage pour missiles autopropulsés

Abrégé

A motor vehicle has a body with an opening that can be closed by a preferably pivotable cover and a box-shaped metallic reflector that is open towards the opening for receiving an HPEM source and that is reversibly insertable into the opening. The reflector is connected to the body by an earth connection following insertion of the reflector. The earth connection is implemented by a brush strip containing fibers of a conductive material that connects the box-shaped reflector to the body circumferentially on all sides in the region of the opening.

Classes IPC  ?

• B60L 1/00 - Fourniture de l'énergie électrique à l'équipement auxiliaire des véhicules à traction électrique
• B60R 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
• H05K 9/00 - Blindage d'appareils ou de composants contre les champs électriques ou magnétiques

Produits et services

Driving assistance systems for military vehicles, in particular cruise control, lane guard systems for military vehicles; Control devices for military vehicles on and off the beaten track, in particular for enabling autonomous capabilities, in particular adaptive cruise control and active lane keeping assistance for military vehicles.

Produits et services

Ammunition and projectiles; Missiles; Guided missiles; Guided missiles with optical seeker heads; Guided missiles; Guided ammunition.

Produits et services

Ammunition and projectiles; Missiles; Guided missiles; Guided missiles with optical seeker heads; Guided missiles; Guided ammunition.

Produits et services

Ammunition for military purposes, cartridge ammunition, medium calibre ammunition, marine ammunition, practice ammunition, insensitive ammunition.

Produits et services

Ammunition for military purposes, cartridge ammunition, medium calibre ammunition, marine ammunition, practice ammunition, insensitive ammunition.

Produits et services

Firearms, Artillery pieces, Ammunition,Intelligent munitions, guided munitions, artillery projectiles.

Produits et services

Monitoring apparatus, in particular omnidirectional monitoring apparatus, special omnidirectional monitoring apparatus for land, air and water vehicles, and parts therefor, in particular including signal processor units, cameras, computers, computer screens, man-machine interfaces, controls, wireless data transmission modules; apparatus for recording, transmission or reproduction of image information, in particular apparatus for recording, transmission or reproduction of image information for land, air or water vehicles, in particular cameras, special cameras for the visual and/or infrared spectrum, and parts therefor, in particular including microbolometers, matrix detectors, CCD chips, lenses, optical elements; navigation apparatus, in particular navigation apparatus for land, air and water vehicles, and parts therefor, in particular including signal processor units, cameras, computers, computer screens, man-machine interfaces, controls, wireless data transmission modules; computer software, in particular computer software for monitoring apparatus, for apparatus for recording, transmission or reproduction of image information, for navigation apparatus. Development and updating of computer software, in particular development and updating of computer software for monitoring apparatus, for apparatus for recording, transmission or reproduction of image information, for navigation apparatus.

Produits et services

Receptacles, containers and tubes of metal, preferably for the storage, transport and launching of missiles of all kinds. Computers, in particular fire control computers for launching missiles of all kinds, interfaces, in particular between computers and missiles of all kinds; computer software for controlling the launching of missiles of all kinds. Missiles of all kinds, in particular guided missiles, preferably guided missiles with an optical seeker head, and parts thereof included in this class; rocket launchers, in particular launching platforms for missiles of all kinds, and parts thereof included in this class. Receptacles, containers and tubes not of metal, in particular of carbon fibre-reinforced plastic material, preferably for the storage, transport and launching of missiles of all kinds. Installation, maintenance and repair of missiles of all kinds; installation, maintenance and repair of receptacles, containers and tubes for the storage, transport and launching of missiles of all kinds; installation, maintenance and repair of rocket launchers, in particular launching platforms for missiles of all kinds. Updating computer software, for launching missiles of all kinds.

Produits et services

Tubes of metal for the storage, transport and launching of missiles; containers of metal for the storage, transport and launching of missiles Fire control computers for launching missiles, interfaces for computers; interfaces between computers and missiles; interface circuits for missiles; computer software for controlling the launching of missiles Guided missiles; guided missiles with an optical seeker head sold as a unit; guided missiles with a rocket launcher sold as a unit; and rocket launchers Industrial carbon fiber-reinforced plastic containers for the storage, transport, and launching of missiles; industrial carbon fiber-reinforced plastic tubes for the storage, transport, and launching of missiles; industrial carbon fiber-reinforced plastic receptacles for the storage, transport, and launching of missiles [ Installation, maintenance and repair of missiles of all kinds; installation, maintenance and repair of receptacles, containers and tubes for the storage, transport and launching of missiles of all kinds; installation, maintenance and repair of rocket launchers, in particular launching platforms for missiles of all kinds ] [ Updating for others computer software that is for launching missiles of all kinds]

Produits et services

Receptacles, containers and pipes of metal, mainly for the storage, transport and launching of missiles of all kinds; launch platforms for missiles of all kinds, and parts therefor (included in class 6). Computers, namely launch control computers for launching missiles of all kinds; interfaces between computers and missiles of all kinds; computer software for controlling the launching of missiles of all kinds. Unmanned missiles of all kinds, in particular guided missiles, mainly guided missiles with optical seeker heads, and parts therefor (included in class 13); rocket launchers and parts therefor (included in class 13). Receptacles, containers and pipes, not of metal, in particular of carbon fibre-reinforced plastic, mainly for the storage, transport and launching of missiles of all kinds. Installation, maintenance and repair of missiles of all kinds; installation, maintenance and repair of receptacles, containers and pipes, for the storage, transport and launching of missiles of all kinds; installation, maintenance and repair of rocket launchers, in particular launch platforms for missiles of all kinds. Updating of computer software, namely for launching missiles of all kinds.

Produits et services

Launch platforms for missiles, and parts therefor (included in class 6). unmanned aerial vehicles, in particular guided missiles, mainly guided missiles with optical seeker heads, and parts therefor (included in class 13), rocket launchers and parts therefor (included in class 13). Receptacles, containers and pipes, not of metal, in particular of carbon fibre-reinforced plastic, for the storage, transport and launching of missiles. Installation, maintenance and repair of missiles;installation, maintenance and repair of receptacles, containers and pipes, for the storage, transport and launching of missiles;installation, maintenance and repair of rocket launchers, in particular launch platforms for missiles.

Produits et services

Launch platforms for missiles, and parts therefor (included in class 6). unmanned aerial vehicles, in particular guided missiles, mainly guided missiles with optical seeker heads, and parts therefor (included in class 13), rocket launchers and parts therefor (included in class 13). Receptacles, containers and pipes, not of metal, in particular of carbon fibre-reinforced plastic, for the storage, transport and launching of missiles. Installation, maintenance and repair of missiles;installation, maintenance and repair of receptacles, containers and pipes, for the storage, transport and launching of missiles;installation, maintenance and repair of rocket launchers, in particular launch platforms for missiles.

Produits et services

[Unmanned and electronically guided targets and components thereof] weapons, rockets and projectiles; missiles; and components of the above mentioned goods

Produits et services

Unmanned guided airborne bodies; missiles; projectiles; weapons; part of the above-mentioned goods.