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Airbus Defence And Space Gmbh patents


Recent patent applications related to Airbus Defence And Space Gmbh. Airbus Defence And Space Gmbh is listed as an Agent/Assignee. Note: Airbus Defence And Space Gmbh may have other listings under different names/spellings. We're not affiliated with Airbus Defence And Space Gmbh, we're just tracking patents.

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Unmanned aerial vehicles

Unmanned aerial vehicles (1), and methods of flying such, comprising at least four rotors (2) arranged such that the plane of rotation of each rotor (2) is co-planar with a face of a notional polyhedron, and wherein each face of the notional polyhedron is co-planar with the plane of rotation of at least one rotor (2). Such methods comprise: a first step of flying the vehicle (1) using a first rotor set (2a-c) to provide lift; and, a second step using a second rotor set (2d-f) to provide lift; wherein, the second rotor set (2d-f) includes at least one rotor (2) that is not used to provide lift in the first step or that operates so that airflow through the rotor (2) is in the opposite direction to that through the rotor (2) during the first step; and, wherein at least one of the first and second sets (2a-c, 2d-f) comprises a plurality of rotors (2).. ... Airbus Defence And Space Gmbh

Method and system for transferring a satellite from an intial orbit into a mission orbit

A system and method for transferring a satellite from an initial orbit into a mission orbit. The method includes anchoring to the satellite of an external unit having a tank containing a reserve of propellants. ... Airbus Defence And Space Gmbh

Electrically connecting multi-layer insulation blankets

Inter alia an apparatus is disclosed including at least two multi-layer insulation, mli, blankets, each mli blanket having a least one bonding point. Therein, a bonding point of a first mli blanket of the at least two mli blankets is electrically connected to a bonding point of a second mli blanket of the at least two mli blankets. ... Airbus Defence And Space Gmbh

Aircraft refueling boom system with nozzle security means

An air refueling boom system comprising a boom joined to the tanker aircraft by means of a mechanical articulation with an inner fuel conduit and a nozzle at its distal end. The tip module of the boom includes a breakable section for separating the tip module in a first and a second portion for allowing a safe separation of tanker and receiver aircraft in a failure event of a refueling operation and linking means of its first and second portions to allow their separation in case of an overload on the nozzle when it is latched to the receptacle and to allow their separation in case of an overload on the nozzle when it is latched to the receptacle.. ... Airbus Defence And Space Gmbh

Process for the electrolytic polishing of a metallic substrate

The present disclosure is directed a process for the electrolytic polishing of a metallic substrate, including the steps of (i) providing an electrolyte in an electrolytic cell having at least one electrode, (ii) disposing a metallic substrate as an anode in the electrolytic cell, (iii) applying a current at a voltage of 270 to 315 v from a power source between the at least one electrode and the metallic substrate, and (iv) immersing the metallic substrate in the electrolyte, wherein the electrolyte includes at least one acid compound, at least one fluoride compound, and at least one complexing agent.. . ... Airbus Defence And Space Gmbh

Lightweight passive attenuator for spacecraft

A lightweight passive attenuator (1) for spacecraft includes two omega cross-section rings (2), placed symmetrically and defining a gap therebetween, and being the main load path of the light passive attenuator (1). A plurality of damper elements (3) are placed in the gap defined between the two omega cross-section rings (2), and not in the main load path of the light passive attenuator (1), such that the omega cross-section rings (2) and the damper elements (3) are assembled at their ends by attachment elements. ... Airbus Defence And Space Gmbh

Aircraft drive device and aircraft provided with a drive device

An aircraft drive device (10) for creating propulsion and/or lift of an aircraft, the drive device comprising a rotating shaft (12), a rotating shaft bearing (14, 16), a rotating shaft drive machine (18) for rotationally driving the rotating shaft (12), and a housing (20), wherein the rotating shaft bearing (14,16) and the rotating shaft drive device (18) are arranged in an interior of the housing (44) and the rotating shaft (12) protrudes to the outside of the housing (20) through a housing opening (42) of the housing (20), wherein in the region of the housing opening (42) an overvoltage arrester device (52) is arranged which is designed for diverting an overvoltage present at the rotating shaft (12).. . ... Airbus Defence And Space Gmbh

Generative production device comprising a measuring device

A device for the layer-wise additive production of a complex three-dimensional component has a measuring mechanism for continuously monitoring quality indicators during the production of the component, wherein the measuring mechanism and a bed with a material powder are surrounded, at least in regions, by a processing cell filled with a protective gas atmosphere and the material powder of an uppermost layer can be melted in a locally limited manner in a melting zone by means of at least one laser. The measuring mechanism has the at least one laser and at least one optical sensor for the priority detection of the quality indicators in the region of the melting zone, in particular by means of raman spectroscopy. ... Airbus Defence And Space Gmbh

Method for communication between a ground terminal on the earth's surface and a satellite

A method for communication between a ground terminal on the earth's surface and a satellite, wherein the ground terminal and a radio terminal of the satellite are set up for ip-based communication. The communication proceeds such that one or more ip-based protocols are used with the interposition of a space-based internet system to transmit control commands for one or more modules of the satellite from the ground terminal to the radio terminal, which receives the control commands by radio from the space-based internet system and forwards them to the module(s). ... Airbus Defence And Space Gmbh

Handheld air sampler device, air sampling arrangement, filter magazine for storing and predefined positioning filter elements on a backing element of a handheld filter device, method for applying a filter element to a backing element of a handheld air sampling device

A handheld air sampler device for enrichment of airborne substances and/or particles, in particular microorganisms, includes: an inlet configured for air intake into a flow channel; an outlet configured for fluidic ally connecting the flow channel to an external vacuum device; a permeable backing element arranged in the flow channel, the backing element being configured to receive and support a filter element; and a sealing element configured for sealing a filter element received on the backing element such that, when a negative pressure is applied to the outlet, air entering the inlet forms an airstream passing the filter element and airborne substances and/or particles, in particular microorganisms, are enriched in the filter element. An air sampling arrangement includes a handheld air sampler device of this type.. ... Airbus Defence And Space Gmbh

Method of preventing separation of a fluid flow and flow body system

A method of preventing separation of a fluid flow flowing over a flow surface is described. The method includes generating longitudinal vortices for suppressing or delaying separation of the flow, and enhancing the longitudinal vortices. ... Airbus Defence And Space Gmbh

Pointing mechanism for use in an electric propulsion system of a spacecraft and electric propulsion system for use in a spacecraft

A pointing mechanism for use in an electric propulsion system of a spacecraft, the pointing mechanism comprises a mobile plate adapted to receive a thruster and defining a thrust vector of the thruster received on the mobile plate. The pointing mechanism further comprises a rotary actuator coupled to the mobile plate by means of a connecting element, the rotary actuator being configured to rotate the connecting element about a rotational axis of the rotary actuator such that the thrust vector defined by the mobile plate rotates about the rotational axis, wherein the thrust vector is inclined relative to the rotational axis.. ... Airbus Defence And Space Gmbh

Control station for unmanned air vehicles and working procedure

An unmanned air vehicle control station, comprising critical systems implementing safety involved functions, non-critical systems implementing non-safety involved functions and a gateway computer. The critical systems comprise at least two redundant critical computers, a redundant critical network and critical back-up network, and at least two redundant uav-specific computers that implement uav-specific functions and communicate with the uav, wherein the at least two critical computers and the at least two uav-specific computers are connected to the critical network and to the critical back-up network. ... Airbus Defence And Space Gmbh

Control surface component for a high-lift device of an aircraft and production method therefor

A control surface component for reducing a noise level generated by the flow around the control surface component, in particular flap component, for a high-lift device of a wing of an aircraft, having a lift body, which is designed or configured to generate lift and which comprises a lift body end region, a lift body suction side and a lift body pressure side, wherein a foam body, which can be mounted adjoining the lift body end region, is formed separately from the lift body as an integral element and is exposed, is designed or configured to provide, in the mounted state, a plurality of flow paths which fluidically connect the lift body suction side and the lift body pressure side to compensate for a pressure difference prevailing between the lift body suction side and the lift body pressure side.. . ... Airbus Defence And Space Gmbh

05/24/18 / #20180145723

Noise distribution shaping for signals, particularly spread spectrum signals like cdma signals, with improved robustness

Noise distribution shaping for signals, particularly for the application in receivers for cdma signals. An embodiment provides a method for noise distribution shaping for signals comprising the acts of generating a blanking control signal by comparing a received signal comprising transitions with at least one blanking threshold, determining transitions of the received signal and zones around the determined transitions, and generating a transitions control signal comprising the determined transitions and zones, adapting the at least one blanking threshold or the received signal according to an offset value depending on the amplitude of the received signal and on the transitions control signal, and modifying the noise distribution of the received signal by applying blanking of the received signal under control of the blanking control signal.. ... Airbus Defence And Space Gmbh

05/24/18 / #20180141662

Anti-rattling device for pallets in cargo aircraft

An anti-rattling restraint device and system for pallets in the cargo hold of an aircraft comprising a frame body with an upper side, lateral sides, a first and a second slot sets positioned on said lateral sides, a first and a second shaft, configured to slide along the first and second slot sets respectively, a threaded stud, a lever, comprising a first end, a second end and a lever slot substantially positioned on the second end of the lever, and lock positioned on the upper side of the frame body, wherein the threaded stud is connected to the second shaft, and further connected to the frame body by the lock, and the lever is connected to the frame body by the first and second shafts, and further connected to the threaded stud by the second shaft.. . ... Airbus Defence And Space Gmbh

05/17/18 / #20180136007

Aircraft navigation system and method for aircraft navigation

An aircraft navigation system and a method for aircraft navigation is presented. The aircraft navigation system has a navigation-map data source, navigation-map data provided by the navigation-map data source including information about a multitude of objects o on earth surface which are of high potential visibility and high potential identifiability from elevated positions, each information for an object o ϵ o including a position and a type of the respective object o; a first system for measuring an actual aircraft position p(t); a waypoint data source providing waypoints wpi defining an aircraft intended flight track; a second system for selecting per waypoint wpi one object oi(wpi) with oi(wpi) ϵ o depending on given selection criteria; and a display for displaying an information i(oi(wpi) referring the selected object oi(wpi).. ... Airbus Defence And Space Gmbh

05/10/18 / #20180126415

Active anti-ice coating, coating material and method

The disclosure herein provides an active anti-ice coating, which is capable of releasing an anti-ice agent, which includes anti-ice agent reservoirs, which are embedded in a uv curable matrix material, for providing an effective anti-ice coating with an active anti-ice agent release over a long period of time.. . ... Airbus Defence And Space Gmbh

05/03/18 / #20180124059

Device authentication of aircrew mobile devices on board aircraft

Configurations of security settings of an access point arranged on board an aircraft. An exemplary embodiment of a method for configuring security settings of an access point arranged on board an aircraft for the authentication of mobile terminals comprises: receipt of flight-related security data from a mobile terminal via a configuration interface of the access point; and configuring of security settings of the access point in a configuration mode based on the flight-related security data so that automatic authentication of preconfigured mobile terminals for access to the access point is possible.. ... Airbus Defence And Space Gmbh

05/03/18 / #20180120366

Method and system for detecting useful signals, with respective non-negligible frequency drift, in a total signal

A method for detecting a plurality of useful signals in a total signal. The useful signals correspond to radiofrequency signals emitted by different terminals in a multiplexing frequency band. ... Airbus Defence And Space Gmbh

04/19/18 / #20180105291

Cleaning assembly for leading edges of airfoils

A cleaning assembly for leading edges of airfoils, in particular airfoil profiles of aircraft or spacecraft, has a cleaning device that is provided with at least one cleaning member and is intended for applying mechanical pressure to a planar region of an airfoil, and has a drive having at least one drive element, which drive moves the cleaning device along the surface to be cleaned. It is proposed to adhesively hold the cleaning device on the airfoil by the at least one cleaning member and/or for the at least one cleaning member to have a sticky surface and for the at least one cleaning member to be dimensionally stable and have flexible contours.. ... Airbus Defence And Space Gmbh

04/12/18 / #20180099455

Receptacle and method for the additive manufacturing of a receptacle

A method for the additive manufacturing of a receptacle for storing and/or transporting a product includes three-dimensionally capturing the external form of the product, compiling a computer-readable data set with information about the captured external form of the product, and additively manufacturing the receptacle. In a computer-controlled manner on the basis of the compiled data set, a modelling material is deposited in layers, liquefied and cured. ... Airbus Defence And Space Gmbh

03/29/18 / #20180088244

Batch processing for gnss signal processing in a user satellite

The disclosure herein relates to a receiver for use in a user satellite, located among other things partly or wholly on orbits remote from earth, for example. The receiver comprises a receiving unit and a processing unit. ... Airbus Defence And Space Gmbh

03/29/18 / #20180088000

Method for adaptively cancelling in real time elastic modes in discrete-time signals

A method of aeroservoelastic coupling suppression, and particularly, the field of real time adaptive cancellation of elastic modes in discrete-time signals which measure the dynamics of a flexible structure. The flexible structure comprises a structure with elastic variable characteristics, and more particularly, a structure with non-linear aerodynamics. ... Airbus Defence And Space Gmbh

03/29/18 / #20180086462

Fixed-wing aircraft and method for operating a fixed-wing aircraft

A fixed-wing aircraft includes a load element, which is coupled to a fuselage of the fixed-wing aircraft; and an actuator device, by which a position of the load element can be varied in relation to the fuselage during a flight of the fixed-wing aircraft in order to displace a center of gravity of the fixed-wing aircraft by the load element.. . ... Airbus Defence And Space Gmbh

03/22/18 / #20180079534

Artificial satellite

Disclosed is an artificial satellite including a battery pack capable of dissipating heat, at least one radiator capable of conveying the heat dissipated by the battery pack into space, and a low-dissipation equipment item having an individual power flux density of less than 250 watts/m2. The satellite includes a thermally insulating cover delimiting, together with the radiator, an interior isothermal zone in which thermal control takes place by radiation, the battery pack and the low-dissipation equipment being arranged in thermally insulating cover. ... Airbus Defence And Space Gmbh

03/08/18 / #20180065732

Fluidic actuator having jet vector control and flow body

. . A fluidic actuator for influencing a flow of a surrounding fluid along a flow surface has a blowing duct for connecting to a pressurized-fluid source, and has a surface blowing opening formed in the flow surface, and a suction duct for connecting to a surface suction opening formed in the flow surface, wherein the suction duct flows into the blowing duct at an entrainment opening.. . ... Airbus Defence And Space Gmbh

03/01/18 / #20180060147

Processor system and method for monitoring processors

A processor system includes an application processor, which has a processor core and hardware performance counters, and a monitoring processor, which is coupled to the application processor by a data transmission interface. The monitoring processor has a look-up table, in which target performance profiles of the progression over time of performance events of the hardware performance counters are stored for an application which is to be executed on the application processor and monitored. ... Airbus Defence And Space Gmbh

02/15/18 / #20180048424

Transmission method and devices for transmission

A method for the transmission of data via an inter communication link (icl) to a receiver unit is provided. The method identifies data to be transmitted in a memory cell of a data storage. ... Airbus Defence And Space Gmbh

02/01/18 / #20180035527

Microelectronic module for altering the electromagnetic signature of a surface, module array and method for altering the electromagnetic signature of a surface

A microelectronic module for altering the electromagnetic signature of a surface. The microelectronic module includes at least one voltage converter for converting a first voltage provided into a higher, lower or identical second voltage. ... Airbus Defence And Space Gmbh

02/01/18 / #20180029727

Satellite comprising electrical propulsion means, method for placing such a satellite in a station and method for keeping said satellite in its station

A satellite, intended to be placed in a station in orbit about a celestial body, including a first electrical thruster of orientatable thrust direction, a second electrical thruster of orientatable thrust direction, and an electrical thruster of fixed orientation that is fixed with respect to the satellite and of line of thrust passing through the center of gravity of the satellite. The satellite includes two electrical-thruster power units and an electrically interconnecting network connecting a first power unit to the first thruster of orientatable thrust direction and to the thruster of fixed orientation, and connecting a second power unit to the second thruster of orientatable thrust direction and to the thruster of fixed orientation. ... Airbus Defence And Space Gmbh

01/25/18 / #20180025814

Device and method for cable assembly

A cable (1) assembly device for producing cabling including: a support surface (2) on which the cable assembly is carried out (1), cable (1) fastening and guide elements (3), said fastening and guide elements (3) comprising a vacuum element for joining it to said support surface (2), a feeder (4) of the cable to be assembled, a computation means that includes a cabling diagram in its memory and the location of the fastening and guide elements (3) on the support surface (2), a storage module (5) for cable (1) fastening and guide elements (3), positioning means (6) of the fastening and guide elements (3) on the support surface (2).. . ... Airbus Defence And Space Gmbh

01/18/18 / #20180017440

Method for processing items and device and use thereof

A device for processing items, in particular items in a production sequence, in different processing steps, has at least one sensor arrangement having a plurality of sensors, wherein at least one item is measured in a detection mode by at least a partial quantity of the sensors as the detection means, wherein an impacting of the at least one item with an irradiation means is determined by a control means while considering a result of the measuring procedure of the at least one item; and wherein the at least one item is irradiated in an irradiation mode by at least a further partial quantity of the plurality of sensors as the irradiation means. If appropriate, at least part of the method is repeated with a renewed measuring, determination and/or irradiation.. ... Airbus Defence And Space Gmbh

01/11/18 / #20180013486

Space network node receiving data from terrestrial and space nodes

A network node is described which is configured for use in space, comprising a transmission interface for transmitting radio frequency signals, a reception interface for receiving radio frequency signals, a network management module for determining communication session information, a controller arranged to control the transmission interface and the reception interface in accordance with session information provided by the network management interface, wherein the transmission and reception interfaces are for receiving data from terrestrial nodes and space-borne nodes. Also described are a network entity comprising the network note and a plurality of adaptive antennas, a satellite containing the network entity and a user equipment device configured for communication with the network node.. ... Airbus Defence And Space Gmbh

01/04/18 / #20180006673

Method and system for suppressing a parasite signal received by a satellite payload

A method for suppressing a parasite signal received with a useful signal by a network of elementary antennas of a payload of a satellite. The suppression method includes an analogue formation step for forming analog beams and a digital formation step for forming a digital beam. ... Airbus Defence And Space Gmbh

01/04/18 / #20180005533

Method for operating an at least temporarily unmanned aircraft or spacecraft and an aircraft or spacecraft of this type

A method for operating an, at least temporarily, unmanned aircraft or spacecraft wherein a flight procedure of the aircraft or spacecraft is carried out in controlled airspace using a previously cleared flight plan, wherein a c2 link is at least temporarily unavailable, and wherein at least one sensor device of the aircraft or spacecraft identifies a dangerous and/or emergency situation which makes it necessary to deviate from the cleared flight plan. To have available a method which makes it possible for an at least temporarily unmanned aircraft or spacecraft to react independently to particular dangerous and/or emergency situations and to avoid damaging events, a control device of the aircraft or spacecraft independently uses a wireless data link to a supervisory authority in order to agree to a changed flight plan containing at least one change.. ... Airbus Defence And Space Gmbh

01/04/18 / #20180001593

Method for producing a sandwich panel comprising a reinforced foam core

A method for producing a sandwich panel with a reinforced foam core includes inserting rod-shaped, thermoplastic reinforcing elements into a thermoplastic foam material such that the reinforcing elements extend through the foam material. End regions of the reinforcing elements project out of the foam material. ... Airbus Defence And Space Gmbh

12/21/17 / #20170361951

Artificial satellite and method for filling a tank of propellent gas of said artificial satellite

Disclosed is artificial satellite including: a mounting structure supporting equipment-bearing walls; a launcher-adapter rigidly connected to the mounting structure; a first radiator; and at least one first system for transporting heat by a fluid, including at least one duct having a first heat-exchange section and a second heat-exchange section, the second heat-exchange section being capable of being in thermal contact with the first radiator. The first heat-exchange section is in thermal contact with at least one portion of the launcher-adapter. ... Airbus Defence And Space Gmbh

12/14/17 / #20170356883

Sensor skin

The disclosure herein relates to a measuring system for determining damage to components including at least one fiber-reinforced plastics material, comprising sensors that can be or are arranged on a component to be mutually spaced, the sensors distributed over a curved surface of the component in the use position. In order provide a measuring system by which it is possible to obtain fiber-reinforced plastics components economically and with reasonable outlay, and by which process parameters and/or state variables can be reliably obtained during production and operation of the component, it is proposed to provide the component with a substrate that is different from the component and on which the sensors can be or are arranged, the substrate being flexible, and for the sensors arranged on the flexible substrate to form a measuring device.. ... Airbus Defence And Space Gmbh

12/14/17 / #20170356866

Sensor skin comprising temperature sensors

A measurement arrangement for detecting damage to components that are made of at least one fiber-reinforced plastic material, has a plurality of temperature sensors that are arrangeable or arranged on a component at a spacing from one another. In order to provide a measurement arrangement, by means of which temperature data can be cost-effectively obtained during the production and operation of a component and for it to thus be possible for damage to the component to be recorded and monitored, the plurality of temperature sensors on the component form a sensor array and a change in the thermal material properties of the component is detected by means of the sensor array.. ... Airbus Defence And Space Gmbh

12/14/17 / #20170355182

Sensor integration in the joining of structural elements

A method for joining structural elements to a component made of at least one fiber-reinforced plastics material, includes providing at least two structural elements made of at least one fiber-reinforced plastics material having a particular matrix; providing at least one film element made of a thermoplastic heavy-duty material; arranging the at least one film element on a surface of one of the structural elements or between surfaces to be joined of the at least two structural elements to be joined; and producing the component to be joined in a curing process.. . ... Airbus Defence And Space Gmbh

12/07/17 / #20170353329

Hybrid network end system device

Provided is a hybrid network end system device for a network system with an end system unit and a switch. The switch here exhibits at least one first port of the switch and a second port of the switch for connection with the network system.. ... Airbus Defence And Space Gmbh

12/07/17 / #20170353230

End system device with integrated switching device

Provided is an end system device for a network system with a first port for connection with the network system, a second port for connection with the network system, a local interface and a switching device. The switching device is designed to switch into a first or a second mode. ... Airbus Defence And Space Gmbh

12/07/17 / #20170349263

Mono-rail crane system in an aircraft

A mono-rail crane system (and a corresponding operation method) for use in an aircraft. The crane system comprises a first longitudinal mono-rail installable on the underside of a rear cargo door of the airplane parallel to the longitudinal axis of the rear cargo door; a second longitudinal mono-rail, which is installable on a cargo hold ceiling of the aircraft, and, in the fully opened state of the rear cargo door, in aligned continuity with the first longitudinal mono-rail so that the longitudinal axes of the first and second longitudinal mono-rails coincide to form one common longitudinal axis; a crane mobile equipment configured to be moved along the first and second longitudinal mono-rails in order to hoist and transfer the load; and a linear actuator configured to advance and retreat the second longitudinal monorail towards and away from the first longitudinal monorail.. ... Airbus Defence And Space Gmbh

11/30/17 / #20170346478

Dc switching device and method of control

A dc switching device has at least one switching unit which is arranged between two terminals. Further, the dc switching device has a control unit for controlling the at least one switching unit. ... Airbus Defence And Space Gmbh

11/30/17 / #20170345166

Method of estimating the motion of a carrier with respect to an environment and calculation device for navigation system

A method for estimating the motion of a carrier with respect to an environment in relation to which the carrier is moving. The carrier bearing a navigation sensor and a vision sensor producing images of the environment. ... Airbus Defence And Space Gmbh

11/30/17 / #20170341782

System for separating separable spacecraft and shuttle elements

A separation system for separable elements of spacecraft and launchers includes an upper ring, a lower ring and a band with an inner channel which houses slidable clamps, which are applied against the upper ring and the lower ring that form the connection interface between the two separable elements. A device joins/separates the ends of the band, both the upper ring and the lower ring including an outer protruding element with a wedged section to be lodged in the clamps. ... Airbus Defence And Space Gmbh

11/30/17 / #20170341781

Spacecraft

The invention relates to a spacecraft comprising a body having two opposite faces; a first radiator carried by at least one face; the first radiator having an outer face; a first supporting arm extending substantially perpendicularly to the outer face of the first radiator; a drive motor suitable for rotating the first supporting arm about its longitudinal axis a first assembly carried by the first supporting arm, said first assembly comprising a plurality of slats stationary with respect to the first supporting arm; said slats being attached one above the other and separated from each other by a free space.. . ... Airbus Defence And Space Gmbh

10/26/17 / #20170305041

Fiber placement and production method

. . A fiber application tool for a fiber placement and production method has a fiber contact surface area, which has a fiber contact surface for applying and/or pressing the fibers onto a work surface. The tool further includes an activation device for activating an adhesive, matrix, resin, or binder material provided at the fibers by means of an activation radiation so that the fibers are tacked onto the work surface. ... Airbus Defence And Space Gmbh

10/12/17 / #20170291386

Structural component

A structural component, in particular for an aircraft, spacecraft or rocket, has a ply of fiber reinforced polymer; a first carbon nanotube mat; and a metallic layer, wherein the carbon nanotube mat and the metallic layer are arranged on the ply of fiber reinforced polymer to form a hybrid lightning strike protection layer. A component for manufacturing such a structural component, a method for manufacturing a component of this type, a method for manufacturing a structural component and an aircraft or spacecraft with such a structural component are described.. ... Airbus Defence And Space Gmbh

10/05/17 / #20170283043

Actuator assembly

An actuator assembly is capable of manipulating a fluid flowing around a flow body, the fluid being received or able to be received in a volume of at least one cavity arranged in the flow body, and the fluid passing through at least one opening in the at least one cavity during manipulation of the fluid. In this process, the volume of the at least one cavity can be changed by moving a wall portion delimiting or defining the cavity. ... Airbus Defence And Space Gmbh

09/28/17 / #20170279521

Scalable architecture for digital signal processing

Architecture is described for implementing digital signal processors, defined by a plurality of physically distinct processing modules connected by high speed digital interconnections in which a first plurality of first modules have a plurality of analogue or digital signal inputs and arranged to perform a first set of digital processing functions and produce a first plurality of digital interconnection outputs, a second plurality of second modules are arranged to receive the first plurality of digital interconnection outputs and perform a second set of digital processing functions and produce a second plurality of digital interconnection outputs, and a third plurality of third modules are arranged to receive the second plurality of digital interconnection outputs and perform a third set of digital processing functions and produce a plurality of analogue or digital signal outputs, wherein the architecture is scalable by selection of the number of first modules, the number of second modules and the number of third modules and the interconnections between them such that the signal processing required of a digital signal processor is achieved through the distribution of the processing over the combination of the selected numbers of first, second and third modules.. . ... Airbus Defence And Space Gmbh

09/14/17 / #20170259925

Seat fastening device

In order to enhance sliding movement and reconfiguration of vehicle seats while using a simple construction, a seat fastening device is provided for fastening vehicle seats in a vehicle. The seat fastening device comprises a seat rail with a t-shaped profile portion and a carriage enclosing an upper part of the t-shaped profile portion. ... Airbus Defence And Space Gmbh

09/14/17 / #20170259924

Seat fastening device

To provide a simple seat fastening device with enhanced flexibility and the possibility of an easy movement of vehicle seats, a seat fastening device for fastening vehicle seats in a vehicle is provided comprising a seat track and a slider in a sliding engagement with the seat track. The slider includes a seat fixation element to fix a foot of a vehicle seat, wherein the seat track includes a c-shaped profile and the slider includes a base inserted in the c-shaped profile and wherein the slider includes a clamp to clamp the slider against an inner surface of the c-shaped profile. ... Airbus Defence And Space Gmbh

08/24/17 / #20170242416

Control circuit system and method for the operation thereof

A control circuit system for influencing at least one process variable includes a plurality of sensors which each detect at least one measurement variable, a plurality of actuators which each manipulate at least one control variable, wherein the sensors and actuators are each assigned electronic circuits for control, and at least one control mechanism which controls and/or coordinates each of the plurality of sensors and actuators by means of at least one control unit. The control circuit system is sub-divided into a plurality of sub-units which are each provided with at least one sensor, at least one actuator and at least one control unit, and for a plurality of the sub-units, in particular all of the sub-units, each to be set up to operate a control circuit system.. ... Airbus Defence And Space Gmbh

08/17/17 / #20170237369

Electric power-generating system for a rotor blade, lighting system for a rotor blade, rotor blade and rotor system

An electric power-generating system for a rotor blade includes at least one electromechanical power-converting device and at least one power-guide line, which is connected mechanically to the electromechanical power-converting device. The electromechanical power-converting device is configured in such a way that, during a movement of the power-guide line, the device converts into electric power the forces introduced by the movement of the power-guide line into the electromechanical power-converting device.. ... Airbus Defence And Space Gmbh

08/17/17 / #20170233857

Al-mg-zn alloy with scandium for the integral construction of alm structures

An aluminum alloy, a method for producing a lightweight metal workpiece, a lightweight metal workpiece including the aluminum alloy, as well as the use of the aluminum alloy for producing high-strength lightweight metal workpieces by additive layer manufacturing (alm) and/or spraying methods for load-optimized components, in particular in automobile manufacturing or in aviation and aerospace applications, plant engineering, medical technology, or as coating material for structural components are described herein.. . ... Airbus Defence And Space Gmbh

08/10/17 / #20170225406

Method for manufacturing a stiffened panel made from composite material

A method for manufacturing a stiffened panel made from composite material comprising a skin and elongated reinforcing elements wherein some of the elongated reinforcing elements cross each other. The method comprises the steps of (a) laying up a flat laminate comprising stacked plies of composite layers for forming a structure comprising the elongated reinforcing elements of the panel, (b) cutting the flat laminate along intersection lines of planes defining the webs of two crossing reinforcing elements, (c) cutting in the flat laminate the outline of the elongated reinforcing elements, (d) forming the structure comprising the elongated reinforcing elements of the panel, (e) laying up plies of composite layers for forming the skin, and (f) curing the laid-up plies of the skin and the formed structure comprising the elongated reinforcing elements.. ... Airbus Defence And Space Gmbh

08/03/17 / #20170219134

Double-walled pipe element and method for producing a double-walled pipe element

A pipe element suitable for use in a fuel system of an aircraft comprises an inner pipe and an outer pipe sealingly surrounding the inner pipe and connected to the inner pipe. The pipe element is constructed in one piece and is produced by a 3d printing process.. ... Airbus Defence And Space Gmbh

08/03/17 / #20170217843

Method for producing a double-walled thermostructural monolithic composte part, and part produced

A fibrous preform (1) is produced, provided with a sandwich structure comprising an intermediate flexible core (4) and two outer fibrous frames (2, 3), respectively arranged on opposing outer faces of said flexible core (4) and assembled by sections of wire (8, 9) passing through said fibrous frames (2, 3), said preform (1) being impregnated with resin. Said preform is then hardened and the core (4) is removed, preferably by pre-densification with chemical vapour infiltration, and the structure produced is then densified with liquid-phase infiltration.. ... Airbus Defence And Space Gmbh

07/20/17 / #20170203831

Propeller device for aircraft, spacecraft or watercraft

A propeller device for aircraft, spacecraft or watercraft comprising two or more blades and a spinner. The blades are arranged on a hub so that they can be in a deployed or a retracted position. ... Airbus Defence And Space Gmbh

07/13/17 / #20170198244

Photobioreactor with mats made from light-decoupling optical fibres and electrically conductive fibres generating a travelling electric field

A photobioreactor is described for cultivating phototrophic organisms and in particular a mat, as can be used in one such photobioreactor. The mat has a plurality of first fibres which are light conductive along their longitudinal direction and are constructed to decouple light conducted in the longitudinal direction laterally, at least somewhat transversely to the longitudinal direction. ... Airbus Defence And Space Gmbh

06/29/17 / #20170188205

Method for managing floor control on a communication channel in the context of half-duplex communications

In the context of half-duplex communications in a communication network composed of a plurality of sub-networks associated respectively with supernode devices, a supernode device receiving a floor request: transmits a floor pre-grant message; determines a timer duration according to a distribution law fτ(t) for time period between a floor release and the next floor control, and a network-latency distribution law fδ(d), so that the probability of subsequent dismissing of the floor control is below a predefined threshold; and broadcasts the data transmitted in the context of the floor control, when the timer has elapsed. When a floor request with higher priority is detected before the expiration of the timer, the supernode device does not broadcast the data and notifies that the floor control is finally refused.. ... Airbus Defence And Space Gmbh

06/29/17 / #20170183108

Method and device for control of a sunlight acquisition phase of a spacecraft

A method to control a sunlight acquisition phase of a spacecraft with a nonzero angular momentum of an axis dh. The spacecraft includes a solar generator configured to rotate about an axis y. ... Airbus Defence And Space Gmbh

06/22/17 / #20170180684

Multispectral image capture device comprising a filter wheel

A multispectral image capture device includes a filter wheel (4) and an image sensor. The filters (41-46) are located close to a focusing plane of a light beam used to form the images, and at least one of the filters is more angularly narrow than the optical field of the image sensor. ... Airbus Defence And Space Gmbh

06/22/17 / #20170179607

Circuit board for hf applications including an integrated broadband antenna

A circuit board includes a substantially planar component carrier and a microstrip which is applied to a surface of the component carrier. The microstrip extends towards a connection transition which is arranged on a lateral edge of the component carrier. ... Airbus Defence And Space Gmbh

06/22/17 / #20170176163

Method for determining a surface profile change in a filling compound in a recess

A method for determining a surface profile change in a filling compound in a recess includes determining a first surface profile of a surface of the filling compound across the recess at an initial temperature; cooling or heating the recess comprising the filling compound to a predetermined measurement temperature; determining a second surface profile of the surface of the filling compound across the recess at the measurement temperature; and comparing the second surface profile with the first surface profile to determine the surface profile change.. . ... Airbus Defence And Space Gmbh

06/22/17 / #20170175307

Coated composite component

A coated composite component includes, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric. A method for producing a coated composite component including, in this order, a composite component, a fluorine-containing film and/or a fluorine-containing woven fabric, knitted fabric or crocheted fabric, and a tear-off fabric.. ... Airbus Defence And Space Gmbh

06/22/17 / #20170174325

Fluidic oscillator device

A fluidic oscillator device, in particular for a or in a flow control system for an aircraft or spacecraft, has a first and a second fluidic actuator, wherein each of the actuators has an inlet for supplying pressure and a first and a second outlet, from which an actuator flow can be discharged. The device further has a fluidic control for controlling an oscillating discharge of the actuator flow from the first and second outlet of the actuators, wherein the control has a connection portion which is arranged between the first actuator and the second actuator.. ... Airbus Defence And Space Gmbh

06/15/17 / #20170169575

Modular device for high-speed video vibration analysis

A technique for modular high-speed video vibration analysis of a structure. An embodiment of a device for high-speed video vibration analysis comprises a camera arrangement configured to generate at least two high-speed video streams of the structure and a data analyzer unit, connected to the camera arrangement. ... Airbus Defence And Space Gmbh

06/15/17 / #20170168306

Device and method for testing function or use of a head worn see through augmented reality device

A method and device to create a realistic and flexible test environment for the evaluation of augmented reality application and device. The test method and the test device for testing the function and/or use of a head worn see through augmented reality device by means of a virtual reality environment, comprises a head mounted device. ... Airbus Defence And Space Gmbh

06/15/17 / #20170165892

Extrusion device and method for filling a groove with a filling compound

An extrusion device and method for filling a groove with a filling compound. The extrusion device includes an extrusion head which is designed or configured to spring in and out in an extrusion direction of the extrusion device in a manner that is spring-resilient in the extrusion direction.. ... Airbus Defence And Space Gmbh

06/15/17 / #20170165795

Scandium-containing aluminium alloy for powder metallurgical technologies

A scandium-containing aluminium powder alloy, wires and materials including said alloy, and a method for producing the scandium-containing aluminium powder alloy, the wires and materials, the proportion of scandium in the scandium-containing aluminium powder alloy being elevated, are disclosed. At least one element is selected from the group consisting of the lanthanum group except for ce, y, ga, nb, ta, w, v, ni, co, mo, li, th, ag.. ... Airbus Defence And Space Gmbh

06/08/17 / #20170162921

Electrical energy storage device

An electrical energy storage device has a plurality of electrochemical energy storage cells for collecting, supplying and storing electrical energy, each of which has a first electrical terminal and a second electrical terminal, and a contacting device for contacting the first and second electrical terminals of the energy storage cells, wherein the contacting device has a multi-layered structure and has at least one insulation layer and a conductor layer. A vehicle with such an electrical energy storage device is also described.. ... Airbus Defence And Space Gmbh

06/08/17 / #20170158351

Landing device for landing a span-wise loaded aircraft

A landing device for landing an aircraft thereon. The landing device comprises a first group of supporting elements arranged next to each other in a first direction, each supporting element configured to support a portion of a body or a portion of a wing of the aircraft. ... Airbus Defence And Space Gmbh

06/08/17 / #20170157908

Connection element, connection arrangement, method for producing a connection element and method for producing a connection arrangement

A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150° c. ... Airbus Defence And Space Gmbh

06/01/17 / #20170153170

Tensile specimen, method for producing a tensile specimen, device for carrying out a tensile test, and method for carrying out a tensile test

A tensile specimen, in particular a fiber-composite-material tensile specimen, includes a test portion which comprises a fiber material and a tensile stress direction which is predetermined for a material test, and a force-introduction portion, wherein the fiber material in the force-introduction portion extends at least in part along a face which is oriented obliquely to the tensile stress direction.. . ... Airbus Defence And Space Gmbh

06/01/17 / #20170152057

Self-illuminated coupling for automatic aerial refueling

An aerial refueling coupling attached to a hose of a tanker aircraft comprising an inner conical surface configured for receiving a probe of a receiver aircraft. The aerial refueling coupling comprises an illumination device attached to the coupling and configured to point to the inner conical surface of the coupling to illuminate the inner conical surface as a target for a laser seeker locatable in the receiver aircraft, to allow the guidance of the probe to contact the coupling.. ... Airbus Defence And Space Gmbh

05/11/17 / #20170129798

Method for sealing a double-walled glass tube in a vacuum-tight manner

This disclosure relates to a method and an apparatus for sealing a double-walled glass tube in a vacuum-tight manner, in particular a production method for manufacturing of solar collectors. By means of a vacuum chamber, inside of which a holding element is fixed and inside of which a heating conductor is arranged, an electro-conductively heating and a subsequent deforming of the double-walled glass tube can be achieved. ... Airbus Defence And Space Gmbh

05/11/17 / #20170129627

Method for controlling the orbit of a satellite in earth orbit, satellite and system for controlling the orbit of such a satellite

A method for controlling the orbit of a satellite in earth orbit. The orbit of the satellite is controlled by commanding, according to a maneuver plan, a propulsion system having at least one thruster and a transporter to move the propulsion system. ... Airbus Defence And Space Gmbh

05/04/17 / #20170126663

Forward-secure crash-resilient logging device

A logging device configured to store log messages, includes a storage device having a plurality of log entry locations which can be ordered as a sequence, an encryption device configured to generate the encrypted log messages from log messages, an authentication code generator configured to generate an authentication code from the encrypted log message, a key evolving device, a state storage device configured to store state variables for use by the encryption device, the authentication code generator and/or the key evolving device. Furthermore, a verification device configured to verify log entries stored in log entry locations of the storage device is also described. ... Airbus Defence And Space Gmbh

05/04/17 / #20170122888

Method for detecting surface impurities by x-ray fluorescence analysis

A method for detecting surface impurities on a surface of a component by x-ray fluorescence analysis uses a hand spectroscope for application to the surface of a component. The hand spectroscope comprises an x-ray source, a fluorescent radiation detector, an analyzer and a display. ... Airbus Defence And Space Gmbh

05/04/17 / #20170122871

Method for detecting surface residues on components using uv radiation

A method for detecting surface residues on fiber composite plastic material components using ultraviolet radiation includes irradiating a surface of the component with ultraviolet radiation using an ultraviolet radiation source, detecting fluorescent radiation which is emitted from the surface of the component as a result of the irradiation with the ultraviolet radiation, and characterizing surface residues on the basis of the detected fluorescent radiation.. . ... Airbus Defence And Space Gmbh

05/04/17 / #20170121794

Al-mg-si alloy with scandium for the integral construction of alm structures

This relates to an aluminium alloy, a method for producing a lightweight metal workpiece, a lightweight metal workpiece comprising the aluminium alloy, and also the use of the aluminium alloy for producing heat-resistant lightweight metal workpieces by means of additive layer manufacturing (alm) and/or spraying methods or for engine components, cylinder heads, crank housings, heat-resistant safety component parts, air-conditioning system components, structural aircraft component parts, in particular in the case of supersonic aircraft, power unit segments, pylons, or as coating material for component parts.. . ... Airbus Defence And Space Gmbh

04/27/17 / #20170113804

Two-phase type heat transfer device for heat sources operating at a wide temperature range

A two-phase type heat transfer device (10) for heat sources operating at a wide temperature range. The heat transfer device (10) includes an evaporator (21) collecting heat from a heat source, a condenser (21) providing heat to a cold sink by a first working fluid passing through liquid and vapor transport lines (25, 27) that connect the evaporator (21) and the condenser (23). ... Airbus Defence And Space Gmbh

04/27/17 / #20170113777

Structural arrangement, aircraft or spacecraft, and method for producing a structural arrangement

A structural arrangement for an aircraft or spacecraft, in particular a fuselage structural arrangement, is disclosed. The structural arrangement includes: a former; a metal skin; and a fibre composite layer which is uniformly structured in a direction running transversely to the former and is arranged between the former and the metal skin. ... Airbus Defence And Space Gmbh

04/20/17 / #20170109666

Aircraft fleet configuration

According to an exemplary embodiment of the present invention, an aircraft fleet configuration system for configuring a fleet of multiple aircraft is provided. The system comprises an input module for inputting customer-specific configuration data, a database comprising a set of rules and a processing unit for automatically varying the customer-specific configuration data in order to generate the virtual fleet. ... Airbus Defence And Space Gmbh

04/20/17 / #20170106996

Display assembly, use of a display assembly, and aircraft assembly having such a display assembly

A display assembly for displaying a parameter of an aircraft, comprising a parameter device and a non-transparent display device. The parameter device for gathering a parameter of the aircraft and/or of an equipment of the aircraft includes a sending unit for sending the parameter. ... Airbus Defence And Space Gmbh

04/06/17 / #20170099702

Ice protection device and method

An ice protection device for an aircraft surface having a composite layer. The device comprises a layer of electrically conductive material configured to be located at an outer face of the composite layer and adapted to be heated by electromagnetic induction. ... Airbus Defence And Space Gmbh

04/06/17 / #20170095985

Binder activation by means of light-emitting diodes in the production of fibre-reinforced plastic laminate

An activation device used for binder activation during the production of a fiber-reinforced plastic laminate. The activation device has at least one light-emitting diode for heating a portion of at least one semi-finished fiber ribbon. ... Airbus Defence And Space Gmbh

04/06/17 / #20170095982

Layered construction of a fibrous body

A method to produce a fibrous body that includes structures crosslinked in a fluid-permeable manner. The method includes constructing the fibrous body in layers by alternately applying a fiber-matrix material to a layer substrate and fusing each applied layer of the fiber-matrix material. ... Airbus Defence And Space Gmbh

03/30/17 / #20170092137

Unmanned aerial vehicle and method for safely landing an unmanned aerial vehicle

An unmanned aerial vehicle with lift and propulsion system and a flight control system and method. The flight control system has a flight control unit, a navigation system, a communication system and an actuator system. ... Airbus Defence And Space Gmbh

03/30/17 / #20170088206

Autonomous crawling system

An automaton system (10) adapted for moving on a surface (s) including: movement means (1) for moving the automaton system on said surface, and actuation means (2) attached to the movement means (1) adapted for acting on the surface, wherein the movement means (1) are adapted for being supported on the surface at a fixed height (h), and in that the actuation means (2) are attached to the movement means (1) by means of an adaptation structure (3), such that the adaptation structure (3) allows the actuation means (2) to act on the surface (s) perpendicular to the tangent of the surface (s) at a point of actuation (a).. . ... Airbus Defence And Space Gmbh

03/23/17 / #20170084987

Aircraft comprising a plurality of antenna units

A flying machine or other vehicle includes at least two antenna units and a central control unit. In a first mode of operation, the two antenna units send and/or receive signals independent of each other in different, non-overlapping frequency bands. ... Airbus Defence And Space Gmbh

03/23/17 / #20170082860

Hmd apparatus with adjustable eye tracking device

Provided is a head-mounted display apparatus that includes an imaging optical system and a camera holder. The imaging optical system includes a display unit, an eye camera, and a control device. ... Airbus Defence And Space Gmbh

03/23/17 / #20170082221

Aircraft bleeding duct in composite material related application

Non-straight ducts for conducting fluids at temperatures higher than 280° c. And pressures higher than 4 bar made of a composite material and, particularly, hot air bleed ducts of an aircraft made of a carbon-fiber reinforced polymer aimed to reduce weight of the bleeding system by replacing most of the metallic material from which the bleeding ducts are currently made.. ... Airbus Defence And Space Gmbh

03/23/17 / #20170081033

Electrical de-icing for aircraft

A heating element for in-flight de-icing of aircraft is disclosed. The heating element includes a carbon fiber material that is designed to be arranged on a component of an aircraft. ... Airbus Defence And Space Gmbh

03/23/17 / #20170081022

Cooperative actuator system for active flow control

A cooperative actuator system for active flow control, a vehicle comprising such cooperative actuator system, and a method for operating an actuator system for active flow control. The cooperative actuator system includes actuators, a control unit, and a data unit. ... Airbus Defence And Space Gmbh

03/23/17 / #20170080649

Manufacture of objects having a fiber-reinforced region

A method suitable for manufacturing complex and stable objects of a wide range of sizes. The method involves producing an object structure by a generative production method and/or by an injection molding method, and producing a fiber-reinforced resin layer in at least one sub-region of the object structure.. ... Airbus Defence And Space Gmbh

03/23/17 / #20170080575

Automating robot operations

A method to control operation of a robot includes generating at least one virtual image by an optical 3d measurement system and with respect to a 3d measurement coordinate system, the at least one virtual image capturing a surface region of a component. The method further includes converting a plurality of point coordinates of the virtual image into point coordinates with respect to a robot coordinate system by a transformation instruction and controlling a tool element of the robot using the point coordinates with respect to the robot coordinate system so as to implement the operation.. ... Airbus Defence And Space Gmbh

03/09/17 / #20170070910

Method for managing congestion of a transmission link in a packet communication network

In order to detect congestion on a transmission link, endpoint items of network equipment are associated with congestion-detection applications. Per class of service, one application sends to the other control messages indicating volumes of data transmitted by the concerned item of network equipment via the transmission link. ... Airbus Defence And Space Gmbh

03/02/17 / #20170064547

Method for generating a digital key for secure wireless communication

. . In a method for generating a digital key in a first communication device and in a second communication device, the first communication device transmits a first electromagnetic signal to the second communication device, which extracts the digital key from the received first electromagnetic signal. The second communication device transmits a second electromagnetic signal to the first communication device, which likewise extracts the digital key from the received second electromagnetic signal. ... Airbus Defence And Space Gmbh

03/02/17 / #20170064049

Network module for sending and/or receiving of data packages from a network arrangement and method

A network module for sending and/or receiving of data packages from a network arrangement located in a network with ring structure, wherein the data package includes at least one data package segment, a source address, a destination address and an identification number. The network module includes a first network interface and a second network interface, for receiving and/or sending of data packages via the ring structure, a processor configured to determine, based on the destination address, if data packages received are directed to the network module and to determine if the source address and/or the destination address are contained in a predefined list of the network participants, to determine, based on the source address and the identification number, if a copy of a data package directed to the network module is already created in a memory, to create a copy of the data package in the memory.. ... Airbus Defence And Space Gmbh

03/02/17 / #20170060107

Autonomous l1-adaptive controller with exact pole placement

Embodiments relate to a predictor device for controlling at least one actuating variable of a plant having at least one actuator, which can be controlled by the actuating variable, and a state with at least one controlled variable that can be detected by a sensor. The predictor has an adaptation device and an l1-adaptive control apparatus. ... Airbus Defence And Space Gmbh

02/16/17 / #20170043863

Microelectronic module, module array, and method for influencing a flow

A microelectronic module for influencing a flow of a fluid is provided. The module comprises at least one voltage converter for converting a provided first voltage into a higher, lower, or identical second voltage. ... Airbus Defence And Space Gmbh

02/02/17 / #20170034890

Device and method for generating light of a predetermined spectrum with a plurality of differently colored light sources

A lighting device that includes a lighting unit, index unit, drive unit, sensor, and control unit. The lighting unit includes a plurality of light sources, with each light source having different color spectra. ... Airbus Defence And Space Gmbh

02/02/17 / #20170030886

Probabilistic defect detection in laid fiber ribbons

A method for a probabilistic detection of defects in ribbons of material laid on a fiber composite workpiece. The method includes detecting at least one surface profile of a workpiece having laid material ribbons and locating a surface profile entry in a database. ... Airbus Defence And Space Gmbh

02/02/17 / #20170029131

Hybrid electric drive train for vtol drones

A vertical take-off aircraft with a propulsion drive for generating a driving force being effective in a horizontal direction and with a lift drive for generating a lifting force being effective in a vertical direction includes a motor for providing mechanical energy for the propulsion drive and a first generator for providing electrical energy for the lift drive. Moreover, the aircraft includes an exhaust gas turbocharger for the motor with a first turbine being driven by an exhaust gas flow of the motor, wherein the first turbine is configured to provide mechanical energy for the propulsion drive.. ... Airbus Defence And Space Gmbh

01/26/17 / #20170025031

Method and apparatus for testing a device for use in an aircraft

In order to be able to test man-machine interfaces (74) cost-effectively under as realistic conditions as possible at as early a stage as possible, a method for testing at least one device (56) to be operated in aircraft by means of a virtual reality environment, wherein the at least one device (56) to be tested is represented in a virtual manner to a test subject (20), and an interaction between the test subject (20) and the at least one device (56) is recorded by means of or in the virtual reality environment.. . ... Airbus Defence And Space Gmbh

01/19/17 / #20170015070

Testing arrangement for controlling the manufacturing of a component

A testing arrangement serves for controlling the manufacturing of a fiber reinforced component. The testing arrangement includes an inspection device with a sensor system, with the inspection device being configured to move on and/or above one or more material layer(s) and/or a surface of the component and to examine the material layer(s) or the surface with the sensor system. ... Airbus Defence And Space Gmbh

01/12/17 / #20170010077

Shaped charge and application for separating two stages of an aeronautical craft or neutralizing the same

A shaped charge comprising a containment shell, an explosive charge placed in the containment shell and having a v-shaped surface, a fuse placed behind the explosive charge, and a layer of projection material placed in front of the v-shaped surface of the explosive charge. A layer of pyrogenic material is used for heating the projection coating. ... Airbus Defence And Space Gmbh

01/05/17 / #20170002667

Heat-resistant turbine blade made from oxide ceramic

This relates to a turbine blade comprising a preformed fibrous fabric of fibres consisting of carbon, silicon carbide or rhenium fixed with a binder resin, and wherein the preformed and fixed fibrous fabric is coated and infiltrated, respectively, with b4c, wherein the preformed fibrous fabric that has been fixed and coated and infiltrated, respectively, with b4c further has a multilayer coating consisting of at least one layer of silicon carbide and at least one layer of a metal boride, a metal nitride or a metal carbide, and wherein an oxide ceramic is applied over the multilayer coating. The turbine blade is resistant to high temperatures and is particularly well suited for use in a gas turbine. ... Airbus Defence And Space Gmbh

01/05/17 / #20170002475

Method for manufacturing as well as use of a polished nanostructured metallic surface having water- and ice- repellent characteristics

A method for manufacturing a water- and ice-repellent surface on a metallic substrate is disclosed, comprising the steps of a) providing a metallic substrate, b) polishing the metallic substrate, c) contacting of at least a part of the metallic substrate with an electrolyte solution, d) anodizing the metallic substrate of step c) for producing a nanoporous layer on the substrate surface, and e) applying a hydrophobic coating on the nanoporous layer. Thereby the accretion of ice particularly on surfaces of aircraft exposed to a flow is reduced in comparison with the prior art.. ... Airbus Defence And Space Gmbh

01/05/17 / #20170002459

Film and coatings from nanoscale graphene platelets

A composite material includes a magnesium alloy and a layer consisting of nanoscale graphene platelets on at least a part of the surface of the magnesium alloy. A process for manufacturing such a composite material includes providing a magnesium alloy, providing nanoscale graphene platelets and applying the nanoscale graphene platelets to at least a part of the surface of the magnesium alloy.. ... Airbus Defence And Space Gmbh

01/05/17 / #20170002191

Flame-retardant, high temperature resistant thermosets on the basis of naphthalene-based epoxy resins and cyanate esters

The embodiments relate to a polymerisable thermoset composition having improved flame retardant properties, a polymerised thermoset having improved flame retardant properties, a process for manufacturing the polymerised thermoset, and use of the polymerisable thermoset composition to produce lightweight construction components, preferably carbon fibre composites (cfrp), and a lightweight construction component, preferably carbon fibre composite (cfrp), containing the polymerised thermoset.. . ... Airbus Defence And Space Gmbh

01/05/17 / #20170002147

Cyanate ester/aryl ethynyl polyimide resins for composite materials

A polymerizable thermoset composition including a polymerizable organic cyanate ester resin and a polymerizable aryl ethynyl-terminated polyimide, a polymerized thermoset, a process for the production of the polymerized thermoset as well as the use of the polymerizable thermoset composition for the production of lightweight construction components, preferably carbon fibre composite materials (cfc), and a lightweight construction component, preferably carbon fibre composite material (cfc), containing the polymerized thermoset are described.. . ... Airbus Defence And Space Gmbh

01/05/17 / #20170001389

Method and device for repairing components

A method for repairing a component which contains fiber-reinforced plastics material. For curing a deformable material introduced into and/or applied to a repair point of the component, the material is heated by irradiation with light from a light-emitting device. ... Airbus Defence And Space Gmbh

01/05/17 / #20170001384

Devices and methods for depositing reinforcing fiber tapes and detecting laying errors

Devices and methods are disclosed for depositing reinforcing fiber tapes and detecting laying errors. Automatic depositing of reinforcing fiber tapes on a support can occur by a laying head and at least one roller assigned to the laying head. ... Airbus Defence And Space Gmbh








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