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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.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Defence And Space Gmbh-related inventors


 new patent  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... Airbus Defence And Space Gmbh

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. The foam material is thermoformed... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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

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

Dc switching device and 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. The switching unit has a first and a second semiconductor switching element, which are arranged in parallel... Airbus Defence And Space Gmbh

Electrical power supply system with multiphase generators and aircraft having such an electrical power supply system

An electrical power supply system for an aircraft includes a plurality of generators, each being couplable to and rotatable by an aircraft engine. and a plurality of electrical conversion units, each having a plurality of inputs and at least one output. Each generator includes at least four AC phases. The... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

Fiber composite laminate and producing a fiber composite laminate

A method for producing a fiber composite laminate, including the steps of applying pressure and/or heat to a first preform, which has one or more dry fiber layers and a thermoplastic elastomer, such that the thermoplastic portion of the thermoplastic elastomer completely impregnates the dry fiber layers of the first... Airbus Defence And Space Gmbh

Aircraft inspection system

In order to provide a simplified inspection of an aircraft for the pilot, an aircraft inspection system is provided which includes at least one movable inspection unit, a position detection arrangement, and at least one data transfer interface. The at least one moveable inspection unit is moveable relative to an... Airbus Defence And Space Gmbh

Aluminum-scandium-calcium alloy

An aluminum-scandium-calcium alloy is produced with a calcium ratio of more than 0.5 wgt.-% and a density of less than 2.6 g/cm3.... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

Apparatus and providing reinforcement strand loops

A device for providing reinforcement strand loops for a multi-needle system for mechanically reinforcing a component made of a foamed plastics material, has a profile body, at least two clamps positioned on the periphery and/or end face of the profile body for fixing a reinforcement strand to the profile body,... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

Electrical drive system for an aircraft and operating method

An electrical drive system for an aircraft includes: at least one first and one second electrical direct voltage sources for supplying a direct voltage, and a first and a second electrical machine modules configured to convert electrical alternating voltage into mechanical movement and vice versa. The first and second modules... Airbus Defence And Space Gmbh

Control circuit 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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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),... Airbus Defence And Space Gmbh

Double-walled pipe element and 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

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... Airbus Defence And Space Gmbh

Aircraft wing with an adaptive shock control bump

An aircraft wing has an upper surface element and a first actuator powered mechanism for varying the shape of the surface element which includes: an upstream segment SEG1, a downstream segment SEG2, an interconnecting segment SEG3 interconnecting a downstream edge of SEG1 with an upstream edge of SEG2, wherein the... Airbus Defence And Space Gmbh

Aircraft wing with spoiler

An aircraft wing has a spoiler movable from a reference position with a deflection angle αref to a given target deflection angle αtarget by an actuator powered mechanism. An upstream edge of the spoiler is interconnected with the aircraft wing exclusively via a strip element made of a resiliently flexible... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

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... Airbus Defence And Space Gmbh

Component device and detecting a damage in a bonding of a component device

The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, which comprises a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, a marker substance device configured to dispense a... Airbus Defence And Space Gmbh

Component device and detecting a damage in a bonding of a component device

The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, the component device having a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, and a detector device having at... Airbus Defence And Space Gmbh

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. A waveguide portion of an antenna element which is produced... 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... Airbus Defence And Space Gmbh

06/15/17 / #20170165892

Extrusion device and 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 / #20170168306

Device and 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,... 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. The data analyzer... Airbus Defence And Space Gmbh

06/08/17 / #20170157908

Connection element, connection arrangement, producing a connection element and 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... 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. Each supporting element... 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,... Airbus Defence And Space Gmbh

06/01/17 / #20170153170

Tensile specimen, producing a tensile specimen, device for carrying out a tensile test, and 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... Airbus Defence And Space Gmbh

05/25/17 / #20170144199

Microelectronic module for cleaning a surface, module array, and cleaning a surface

A microelectronic module for cleaning a surface is described. The microelectronic module comprises at least one voltage converter for converting a provided first voltage into a higher, lower, or identical second voltage. The module also comprises at least one actuator. The actuator comprises at least one generator for generating an... Airbus Defence And Space Gmbh

05/25/17 / #20170144333

Thermal heating device using light for binder activation and its integration in preforming device

A binder material activating device to activate a binder material on a fibrous substrate, the binder material activating device including a heat exposing device to expose the fibrous substrate with the binder material to heat. The heat exposing device includes a non-focused light source to provide a non-focused light beam... Airbus Defence And Space Gmbh

05/25/17 / #20170144384

Laying unit, device and producing a fiber composite component

A laying unit for producing a fiber composite component includes a drive device which is formed for magnetic cooperation with a running face, which provides a magnetic field and/or is ferromagnetic, to advance the laying unit on the running face. A device for producing a fiber composite component comprising a... Airbus Defence And Space Gmbh

05/25/17 / #20170144386

Laying unit and producing a fibre composite component

A laying unit for producing a fibre composite component is provided. The laying unit includes a housing and a plurality of fibre coils which are designed so as to be able to be unwound during a movement of the laying unit, wherein the fibre coils are provided in a movably... Airbus Defence And Space Gmbh

05/25/17 / #20170144387

Apparatus and producing a fiber composite component

An apparatus for producing a fiber composite component. The apparatus includes a shaping tool and a plurality of laying units which are mechanically independent of one another and are each configured to lay a fiber material on the shaping tool, wherein the laying units each include a control device which... Airbus Defence And Space Gmbh

05/25/17 / #20170149518

Interface device and exchanging user data

An interface apparatus is provided for exchange of different time-critical user data between a host device and a divided medium, by way of a first interface and by way of a second interface, having a resource management device and a temporary memory device. The first interface works with a first... 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... 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,... 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... 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. The method comprises irradiating the surface... 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... Airbus Defence And Space Gmbh

04/27/17 / #20170113777

Structural arrangement, aircraft or spacecraft, and 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... 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. The non-transparent display device is detachable,... 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... 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. The fiber-matrix material contains a matrix material... 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. A method is used for producing a fiber-reinforced plastic laminate. It comprises automatically laying at... Airbus Defence And Space Gmbh

03/30/17 / #20170092137

Unmanned aerial vehicle and 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. The flight control unit can calculate, based on data from the navigation system and/or data... 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... 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 / #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. The actuators are distributed along the surface in at least... 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. The carbon fiber material includes at least two electrical contacts for connecting to an electrical wiring system, and at least... 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. The display unit is to be viewed by an eye of a user, and the control device is to... Airbus Defence And Space Gmbh

Patent Packs
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. The central control unit is adapted to control the two... 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... 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... 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... Airbus Defence And Space Gmbh

02/16/17 / #20170043863

Microelectronic module, module array, and 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. The module also comprises at least one active flow-influencing element for influencing the direction and/or the... 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... 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. In this case, the surface profile entry... Airbus Defence And Space Gmbh

02/02/17 / #20170034890

Device and 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. The index unit is to calculate a color rendering index based on stored data on spectra of... Airbus Defence And Space Gmbh

01/26/17 / #20170021911

Coupling device, wing assembly for an aircraft comprising such coupling device and aircraft comprising such wing assembly

A coupling device for supporting a first wing section against a second wing section of an aircraft, and configured for passive flight load alleviation includes a housing including a chamber including a first portion and a second portion and filled with a fluid, a piston device movably arranged in the... Airbus Defence And Space Gmbh

01/26/17 / #20170025031

Method and 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... 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... 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. At least one radiation source and/or at least one sensor is... 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. The disclosure herein further relates to a light-emitting device for heating... 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... 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,... Airbus Defence And Space Gmbh

Patent Packs
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... 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... 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... Airbus Defence And Space Gmbh








ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009



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