Abstract: 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 provides an assignment of the surface profile to a defect type and to a hit probability that the detected surface profile is based on a defect of the defect type.
Abstract: 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. The monitoring processor has an evaluating logic which is linked to the look-up table and is configured to record the progression over time of performance events of the hardware performance counters during the execution of the application to be monitored on the application processor and to compare the progression with the target performance profiles stored in the look-up table.
Type:
Grant
Filed:
August 29, 2017
Date of Patent:
January 21, 2020
Assignee:
Airbus Defence and Space GmbH
Inventors:
Johannes Freitag, Dietmar Geiger, Bernd Koppenhoefer, Sascha Uhrig, Max Gapp
Abstract: A method for acquiring images using a constellation of satellites in non-geosynchronous terrestrial orbit. The satellites include respective devices for inter-satellite communication. An aggregate of work plans intended for various satellites is formed. A ground station transmits the aggregate intended for one satellite. The satellite receiving the aggregate retransmits the aggregate intended for at least one other satellite from the ground station. Each satellite receiving the aggregate from another satellite re-transmits the aggregate intended for at least one other satellite. Each satellite recovers its work plan from the aggregate received.
Abstract: 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.
Type:
Grant
Filed:
November 22, 2016
Date of Patent:
December 31, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Peter Starke, Harald Kraft, Martin Holzapfel, Marcel Brodbeck
Abstract: A network interface of a network user having at least one physical interface for connecting the network interface to a network interface of a different network user, at least one data selector, which is connected to the physical interface and which is suitable for receiving data from the physical interface and sending data to the physical interface, and at least one data switch, which is connected to the data selector and which is suitable for receiving data from the data selector and sending data to the data selector.
Type:
Application
Filed:
August 28, 2019
Publication date:
December 19, 2019
Applicant:
Airbus Defence and Space GmbH
Inventors:
Andreas Pruecklmeier, Thomas Pistner, Stefan Schneele
Abstract: A method for searching a search area, with a missile and with a missile formation is described Based on the method, in each case at least one radar is arranged in at least two missiles, wherein the method includes: splitting the search area into at least two search subareas, searching the at least two search subareas by the respective radar of the at least two missiles, wherein the at least two missiles carry out the searching cooperatively, wherein the search subareas are chosen such that a total search time is minimal.
Abstract: 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. A method for storing log entries in log entry locations of a storage device of a logging device as well as to a method for verifying the integrity of log entries stored in log entry locations of a storage device is also described.
Abstract: 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 one insulation layer for electrical insulation.
Type:
Grant
Filed:
September 22, 2016
Date of Patent:
November 19, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Juergen Steinwandel, Dietrich Jonke, Helmut Piringer
Abstract: 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.
Abstract: A method for acquiring images using a constellation of satellites in non-geosynchronous terrestrial orbit. The satellites include respective devices for inter-satellite communication. An aggregate of work plans intended for various satellites is formed. A ground station transmits the aggregate intended for one satellite. The satellite receiving the aggregate retransmits the aggregate intended for at least one other satellite from the ground station. Each satellite receiving the aggregate from another satellite re-transmits the aggregate intended for at least one other satellite. Each satellite recovers its work plan from the aggregate received.
Abstract: 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. A direct signal component, transmitted on a direct signal path between the first communication device and the second communication device, of the first electromagnetic signal and of the second electromagnetic signal is attenuated.
Type:
Grant
Filed:
August 31, 2016
Date of Patent:
October 29, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Jirka Klaue, Christoph Heller, Martin Kubisch, Sebastian Stemmer
Abstract: A flow aid for an infusion structure for infiltrating fiber material with resin to produce a fiber composite component includes a resin-impermeable upper layer and a lower layer which are joined together in a peripheral region of the flow aid and provide a flow space between the two layers. The lower layer provides an outlet for discharging resin out of the flow aid into an interior of the infusion structure. The flow aid includes an inlet for feeding the resin into the flow space, thereby facilitating uniform distribution of the resin over all of the fiber material.
Abstract: A method for manufacturing components includes joining a first edge of a thermoplastic-containing first component part and a second edge of a thermoplastic-containing second component part to one another without any overlap. The first and the second edge are interconnected by friction stir welding. Friction stir welding involves rubbing a rotating friction stir welding pin against at least one metal object.
Abstract: 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 laying unit of this type and a method for producing a fiber composite component comprising a device of this type are disclosed.
Type:
Grant
Filed:
November 22, 2016
Date of Patent:
October 29, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Franz Engel, Christian Weimer, Tilman Orth
Abstract: In order to maintain a surface region of an aircraft free of ice in a particularly energy-efficient manner, a device for deicing and/or for preventing ice formation is provided on an aircraft. The device includes a heat emitting device for emitting heat at a surface region of the aircraft, the heat emitting device is designed to dissipate heat along a line in order to produce a predetermined breaking point or a predetermined breaking line or parting line in ice accumulating on the surface region.
Type:
Grant
Filed:
November 12, 2014
Date of Patent:
October 15, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Tobias Strobl, Stefan Storm, Dominik Raps, Tobias Hauk
Abstract: 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.
Type:
Grant
Filed:
July 27, 2016
Date of Patent:
October 8, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Jürgen Steinwandel, Ning Wang, Michael Judas, Jan Van Toor
Abstract: 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 integrated into the at least one roller for the detection of laying errors, and this roller is transmissive at least by region for a radiation emitted by the radiation source.
Type:
Grant
Filed:
June 30, 2016
Date of Patent:
October 8, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Christian Eitzinger, Franz Engel, Tilman Orth, Christian Weimer
Abstract: 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 is configured to actuate each laying unit to automatically interact with at least one other laying unit to lay a predetermined fiber arrangement together.
Type:
Grant
Filed:
November 22, 2016
Date of Patent:
October 8, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Franz Engel, Christian Weimer, Tilman Orth
Abstract: A network interface of a network user having at least one physical interface for connecting the network interface to a network interface of a different network user, at least one data selector, which is connected to the physical interface and which is suitable for receiving data from the physical interface and sending data to the physical interface, and at least one data switch, which is connected to the data selector and which is suitable for receiving data from the data selector and sending data to the data selector.
Type:
Grant
Filed:
June 9, 2016
Date of Patent:
October 8, 2019
Assignee:
Airbus Defence and Space GmbH
Inventors:
Andreas Pruecklmeier, Thomas Pistner, Stefan Schneele
Abstract: A blasting medium for blasting a component, wherein the component comprises Al and/or Mg, especially an Al and/or Mg alloy, to a method of blasting a component, wherein the component comprises Al and/or Mg, especially an Al and/or Mg alloy, and a method of producing a blasting medium are described herein.