Goods & 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.

Goods & 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.

Goods & Services

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

Goods & Services

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

Goods & 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.

Abstract

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.

IPC Classes  ?

• H01M 6/36 - Deferred-action cells containing electrolyte and made operational by physical means, e.g. thermal cells
• F42B 15/00 - Self-propelled projectiles or missiles, e.g. rocketsGuided missiles
• H01M 6/46 - Grouping of primary cells into batteries of flat cells
• H01M 6/50 - Methods or arrangements for servicing or maintenance, e.g. for maintaining operating temperature

Abstract

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).

IPC Classes  ?

• G01S 7/40 - Means for monitoring or calibrating
• G01S 13/78 - Systems using reradiation of radio waves, e.g. secondary radar systemsAnalogous systems wherein pulse-type signals are transmitted discriminating between different kinds of targets, e.g. IFF-radar, i.e. identification of friend or foe
• G01S 13/87 - Combinations of radar systems, e.g. primary radar and secondary radar

Abstract

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).

IPC Classes  ?

• F41G 7/00 - Direction control systems for self-propelled missiles
• F41G 7/22 - Homing guidance systems

Abstract

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.

IPC Classes  ?

• B63G 1/00 - Arrangements of guns or missile launchersVessels characterised thereby

Goods & 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.

Goods & 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.

Goods & 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.

Abstract

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.

IPC Classes  ?

• H01T 15/00 - Circuits specially adapted for spark gaps, e.g. ignition circuits
• H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating

Abstract

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).

IPC Classes  ?

• F41G 9/00 - Systems for controlling missiles or projectiles, not provided for elsewhere
• F41G 7/00 - Direction control systems for self-propelled missiles
• F41F 3/06 - Rocket or torpedo launchers for rockets from aircraft
• B64D 7/08 - Arrangement of rocket launchers
• H01R 13/66 - Structural association with built-in electrical component

Abstract

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.

IPC Classes  ?

• H02M 3/06 - Conversion of DC power input into DC power output without intermediate conversion into AC by static converters using resistors or capacitors, e.g. potential divider

Abstract

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.

IPC Classes  ?

• F42B 10/60 - Steering arrangements
• F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems

Abstract

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).

IPC Classes  ?

• G02B 5/04 - Prisms
• F41G 7/22 - Homing guidance systems
• G02B 13/00 - Optical objectives specially designed for the purposes specified below
• G02B 17/04 - Catoptric systems, e.g. image erecting and reversing system using prisms only
• G02B 17/08 - Catadioptric systems
• G02B 26/02 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the intensity of light
• G02F 1/35 - Non-linear optics

Abstract

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.

IPC Classes  ?

• F41H 13/00 - Means of attack or defence not otherwise provided for
• F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems

Abstract

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).

IPC Classes  ?

• B64C 39/02 - Aircraft not otherwise provided for characterised by special use
• B64D 5/00 - Aircraft transported by aircraft, e.g. for release or reberthing during flight
• B64D 3/00 - Aircraft adaptations to facilitate towing or being towed

Abstract

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.

IPC Classes  ?

• F41H 13/00 - Means of attack or defence not otherwise provided for
• H05B 6/72 - Radiators or antennas
• H05B 6/70 - Feed lines
• H05B 6/68 - Circuits for monitoring or control

Abstract

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.

IPC Classes  ?

• F41G 7/22 - Homing guidance systems
• G05D 1/12 - Target-seeking control

Abstract

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.

IPC Classes  ?

• F42B 15/01 - Arrangements thereon for guidance or control
• F42B 15/08 - Self-propelled projectiles or missiles, e.g. rocketsGuided missiles for carrying measuring instruments

Abstract

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.

IPC Classes  ?

• F41G 7/22 - Homing guidance systems
• G06T 7/20 - Analysis of motion
• G06T 7/70 - Determining position or orientation of objects or cameras
• F41G 7/00 - Direction control systems for self-propelled missiles

Abstract

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.

IPC Classes  ?

• F41G 7/22 - Homing guidance systems
• G01S 13/88 - Radar or analogous systems, specially adapted for specific applications

Abstract

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.

IPC Classes  ?

• F41G 7/22 - Homing guidance systems
• G01S 7/03 - Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
• H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons

Goods & 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.

Abstract

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.

IPC Classes  ?

• B02C 19/18 - Use of auxiliary physical effects, e.g. ultrasonics, irradiation, for disintegrating
• B02C 23/10 - Separating or sorting of material, associated with crushing or disintegrating with separator arranged in discharge path of crushing or disintegrating zone
• B02C 23/14 - Separating or sorting of material, associated with crushing or disintegrating with more than one separator
• B02C 23/38 - Adding fluid, other than for crushing or disintegrating by fluid energy in apparatus having multiple crushing or disintegrating zones

Goods & 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.

Goods & 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.

Goods & 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.

Abstract

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).

IPC Classes  ?

• H01Q 1/28 - Adaptation for use in or on aircraft, missiles, satellites, or balloons
• H01Q 1/38 - Structural form of radiating elements, e.g. cone, spiral, umbrella formed by a conductive layer on an insulating support
• H01Q 1/40 - Radiating elements coated with, or embedded in, protective material
• H01Q 5/22 - RF wavebands combined with non-RF wavebands, e.g. infrared or optical
• H01Q 9/04 - Resonant antennas
• H01Q 21/06 - Arrays of individually energised antenna units similarly polarised and spaced apart

Goods & 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

Goods & 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.

Goods & 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.

Goods & Services

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

Goods & 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.

Goods & 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.

Abstract

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.

IPC Classes  ?

• F41G 7/00 - Direction control systems for self-propelled missiles
• F41G 7/22 - Homing guidance systems
• G06T 7/73 - Determining position or orientation of objects or cameras using feature-based methods
• G06K 9/32 - Aligning or centering of the image pick-up or image-field
• G06K 9/46 - Extraction of features or characteristics of the image

Abstract

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°.

IPC Classes  ?

• G01S 7/282 - Transmitters
• G01S 13/931 - Radar or analogous systems, specially adapted for specific applications for anti-collision purposes of land vehicles
• H01Q 3/06 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation over a restricted angle
• H01Q 3/34 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase by electrical means
• H01Q 15/14 - Reflecting surfacesEquivalent structures
• H01Q 21/29 - Combinations of different interacting antenna units for giving a desired directional characteristic
• F41H 13/00 - Means of attack or defence not otherwise provided for
• G01S 13/72 - Radar-tracking systemsAnalogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar

Goods & 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.

Goods & 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.

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & Services

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

Abstract

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.

IPC Classes  ?

• F42C 15/40 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected electrically
• F42C 15/26 - Arming-means in fuzesSafety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means using centrifugal force

Goods & 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.

Abstract

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).

IPC Classes  ?

• F42B 12/24 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings
• F42B 12/32 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & Services

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

Abstract

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.

IPC Classes  ?

• G01S 7/282 - Transmitters
• G01S 13/88 - Radar or analogous systems, specially adapted for specific applications
• G01V 3/12 - Electric or magnetic prospecting or detectingMeasuring magnetic field characteristics of the earth, e.g. declination or deviation operating with electromagnetic waves
• A61B 5/00 - Measuring for diagnostic purposes Identification of persons
• G01N 22/00 - Investigating or analysing materials by the use of microwaves or radio waves, i.e. electromagnetic waves with a wavelength of one millimetre or more
• G01N 21/47 - Scattering, i.e. diffuse reflection

Abstract

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.

IPC Classes  ?

• F41H 13/00 - Means of attack or defence not otherwise provided for

Abstract

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.

IPC Classes  ?

• F41F 3/077 - Doors or covers for launching tubes
• F41F 3/042 - Rocket or torpedo launchers for rockets the launching apparatus being used also as transport container for the rocket

Abstract

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).

IPC Classes  ?

• B02C 19/18 - Use of auxiliary physical effects, e.g. ultrasonics, irradiation, for disintegrating
• B02C 23/10 - Separating or sorting of material, associated with crushing or disintegrating with separator arranged in discharge path of crushing or disintegrating zone
• B02C 23/14 - Separating or sorting of material, associated with crushing or disintegrating with more than one separator
• B02C 23/38 - Adding fluid, other than for crushing or disintegrating by fluid energy in apparatus having multiple crushing or disintegrating zones

Abstract

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).

IPC Classes  ?

• B02C 19/18 - Use of auxiliary physical effects, e.g. ultrasonics, irradiation, for disintegrating
• B02C 23/10 - Separating or sorting of material, associated with crushing or disintegrating with separator arranged in discharge path of crushing or disintegrating zone
• B02C 23/14 - Separating or sorting of material, associated with crushing or disintegrating with more than one separator
• B02C 23/38 - Adding fluid, other than for crushing or disintegrating by fluid energy in apparatus having multiple crushing or disintegrating zones

Abstract

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.

IPC Classes  ?

• F42C 19/08 - PrimersDetonators
• F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type

Abstract

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.

IPC Classes  ?

• G01J 5/00 - Radiation pyrometry, e.g. infrared or optical thermometry
• F41G 7/22 - Homing guidance systems
• H04N 5/33 - Transforming infrared radiation
• H04N 5/357 - Noise processing, e.g. detecting, correcting, reducing or removing noise
• H04N 17/00 - Diagnosis, testing or measuring for television systems or their details
• F41G 7/00 - Direction control systems for self-propelled missiles
• G01S 3/78 - Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
• G01J 5/22 - Electrical features thereof

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & 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.

Abstract

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).

IPC Classes  ?

• F41H 13/00 - Means of attack or defence not otherwise provided for
• F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems
• F42B 15/36 - Means for interconnecting rocket-motor and body sectionMulti-stage connectorsDisconnecting means
• F42B 12/62 - Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile

Goods & 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)

Goods & 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)

Abstract

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.

IPC Classes  ?

• G06F 21/62 - Protecting access to data via a platform, e.g. using keys or access control rules
• H04L 29/06 - Communication control; Communication processing characterised by a protocol

Goods & 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.

Goods & 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.

Abstract

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).

IPC Classes  ?

• F42C 19/08 - PrimersDetonators
• F42B 12/20 - Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type

Abstract

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

IPC Classes  ?

• C07C 209/68 - Preparation of compounds containing amino groups bound to a carbon skeleton from amines, by reactions not involving amino groups, e.g. reduction of unsaturated amines, aromatisation, or substitution of the carbon skeleton
• C07C 209/60 - Preparation of compounds containing amino groups bound to a carbon skeleton by condensation or addition reactions, e.g. Mannich reaction, addition of ammonia or amines to alkenes or to alkynes or addition of compounds containing an active hydrogen atom to Schiff's bases, quinone imines, or aziranes

Abstract

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.

IPC Classes  ?

• C07C 209/68 - Preparation of compounds containing amino groups bound to a carbon skeleton from amines, by reactions not involving amino groups, e.g. reduction of unsaturated amines, aromatisation, or substitution of the carbon skeleton
• C07C 211/09 - Diamines
• C07C 211/15 - Compounds containing amino groups bound to a carbon skeleton having amino groups bound to acyclic carbon atoms of an acyclic saturated carbon skeleton the carbon skeleton being further substituted by halogen atoms or by nitro or nitroso groups
• C07C 267/00 - Carbodiimides
• C07C 209/60 - Preparation of compounds containing amino groups bound to a carbon skeleton by condensation or addition reactions, e.g. Mannich reaction, addition of ammonia or amines to alkenes or to alkynes or addition of compounds containing an active hydrogen atom to Schiff's bases, quinone imines, or aziranes
• C07C 211/24 - Compounds containing amino groups bound to a carbon skeleton having amino groups bound to acyclic carbon atoms of an acyclic unsaturated carbon skeleton the carbon skeleton being further substituted by halogen atoms or by nitro or nitroso groups

Abstract

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.

IPC Classes  ?

• F42B 15/01 - Arrangements thereon for guidance or control
• F42B 10/64 - Steering by movement of flight surfaces of fins

Abstract

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.

IPC Classes  ?

• H04N 5/225 - Television cameras
• H04N 5/77 - Interface circuits between an apparatus for recording and another apparatus between a recording apparatus and a television camera
• G06T 7/00 - Image analysis
• G06T 7/70 - Determining position or orientation of objects or cameras

Abstract

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.

IPC Classes  ?

• F41H 13/00 - Means of attack or defence not otherwise provided for
• F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems

Goods & 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.

Abstract

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.

IPC Classes  ?

• G06K 9/00 - Methods or arrangements for reading or recognising printed or written characters or for recognising patterns, e.g. fingerprints

Abstract

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).

IPC Classes  ?

• A01K 15/00 - Devices for taming animals, e.g. nose-rings or hobblesDevices for overturning animals in generalTraining or exercising equipmentCovering boxes
• A61L 9/04 - Disinfection, sterilisation or deodorisation of air using gaseous or vaporous substances, e.g. ozone using substances evaporated in the air without heating
• A01K 15/02 - Training or exercising equipment, e.g. mazes or labyrinths for animals

Abstract

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.

IPC Classes  ?

• F41G 7/22 - Homing guidance systems
• F41G 7/00 - Direction control systems for self-propelled missiles

Abstract

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.

IPC Classes  ?

• F25B 9/00 - Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
• F25B 9/02 - Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using Joule-Thompson effectCompression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point using vortex effect
• F25B 19/00 - Machines, plants or systems, using evaporation of a refrigerant but without recovery of the vapour
• F16K 31/02 - Operating meansReleasing devices electricOperating meansReleasing devices magnetic

Abstract

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.

IPC Classes  ?

• G05B 13/02 - Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
• G06F 17/00 - Digital computing or data processing equipment or methods, specially adapted for specific functions
• F41H 11/02 - Anti-aircraft or anti-guided missile defence installations or systems
• F41G 3/04 - Aiming or laying means for dispersing fire from a battery
• G05B 15/02 - Systems controlled by a computer electric
• F41G 7/00 - Direction control systems for self-propelled missiles

Abstract

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.

IPC Classes  ?

• B60L 1/00 - Supplying electric power to auxiliary equipment of electrically-propelled vehicles
• B60R 99/00 - Subject matter not provided for in other groups of this subclass
• H05K 9/00 - Screening of apparatus or components against electric or magnetic fields

Goods & 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.

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & Services

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

Goods & 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.

Goods & 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.

Goods & 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]

Goods & 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.

Goods & 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.

Goods & 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.

Goods & Services

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

Goods & Services

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