Patents Assigned to European Aeronautic Defence and Space Company – EADS France
  • Patent number: 8577662
    Abstract: To analyze an electronic component, this component is exposed to a focused laser beam. The information provided by the laser mapping relating to the position and to the depth of the sensitivity zones of the component is used as input parameter in prediction codes for quantifying the sensitivity of the mapped component to ionizing particles in the natural radioactive environment. The prediction codes are used to determine the occurrence of malfunctions in the electronic component. Determination of the risks associated with the radiative environment imposes two aspects: one, probabilistic, takes into account the particle/matter interaction and the other, electrical, takes into account the charge collection inside the electronic component.
    Type: Grant
    Filed: October 23, 2008
    Date of Patent: November 5, 2013
    Assignees: European Aeronautic Defence and Space Company EADS France, Airbus Operations (S.A.S.), Astrium SAS
    Inventors: Florent Miller, Nadine Buard, Cecile Weulersse, Thierry Carriere, Patrick Heins
  • Publication number: 20130184958
    Abstract: A method of controlling a group (2) of engines developing a necessary power (Wnec) for driving a rotor (3), said group (2) of engines having at least one electrical member (4), electrical energy storage means (5), and a first number n of engines (6) that is greater than or equal to two. A processor unit (10) executes instructions for evaluating a main condition as to whether the group of engines can develop the necessary power while resting one engine, and if so for resting one engine and accelerating a second number engines not at rest, and for causing the electrical member to operate in motor mode, if necessary, the electrical member operating temporarily in electricity generator mode when the storage means are discharged.
    Type: Application
    Filed: July 16, 2012
    Publication date: July 18, 2013
    Applicants: EADS (European Aeronautic Defence and Space company EADS France), EUROCOPTER
    Inventors: Nadine Dyrla, Alban Corpron, Emmanuel Joubert, Hichem Smaoui
  • Publication number: 20130126674
    Abstract: An aircraft fuselage structure, includes a circumferential reinforcing frame (2) and a plurality of stringers (3) substantially perpendicular to the frame. The frame includes a mechanically weakened area able to cause its localized buckling under the effect of a compressive force exerted circumferentially thereon. The structure includes an energy absorbing device (5) having two effector members (52) secured to the frame respectively on either side of the weakened area, and a central core (51) maintained between the effector members such that a reduction in the distance between the effector members produces a deformation of the central core, which is able to absorb energy under the effect of the deformation.
    Type: Application
    Filed: April 22, 2011
    Publication date: May 23, 2013
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Jean-Mathieu Guimard, Michel Bermudez, Didier Mesnage
  • Patent number: 8376262
    Abstract: An aircraft includes a cabin in which at least part of the space is demarcated by trim panels and the cabin is provided with a system for the active control of ambient noise. Each trim panel is either an active panel including actuators powered by the active noise control system or a passive panel without such actuators. In addition, the trim panels of the cabin of the one type, either active or passive, are mechanically interchangeable with a panel of the other type, either passive or active, respectively. Power supply wiring for active panels is installed in the aircraft, this wiring being capable of powering all active panels which could be installed, whether said active panels are actually installed or whether interchangeable passive panels are installed. Finally, a power supply system for the active panels is installed in the aircraft and connected to the power supply wiring of the active panels.
    Type: Grant
    Filed: July 9, 2008
    Date of Patent: February 19, 2013
    Assignee: European Aeronautic Defence and Space Company EADS France
    Inventor: Benoit Petitjean
  • Patent number: 8378696
    Abstract: The behavior of a component subjected to pulsed laser radiation is measured. The polarization value, frequency, and temperature (or other operating conditions) to which the component is sensitive are determined by detecting a temporary or permanent fault in the operation of the component. If necessary, the parasitic currents generated are prevented from destroying the tested component at the time of testing. A susceptibility of the component to energetic interactions and the preferred operating conditions for the component are deduced.
    Type: Grant
    Filed: September 5, 2008
    Date of Patent: February 19, 2013
    Assignee: European Aeronautic Defence and Space Company EADS France
    Inventors: Nadine Buard, Florent Miller, Patrick Heins, Thierry Carriere
  • Patent number: 8338803
    Abstract: The invention relates to a device for testing an integrated circuit. The device comprises a plate for receiving and subjecting the integrated circuit to a test. The plate comprises a component for powering and operating the integrated circuit and another component for measuring the operation of the integrated circuit during the test. The device also comprises an irradiation device for subjecting the circuit to a proton bombardment and a mask with a variable thickness provided between a bombardment access region on the integrated circuit and an established zone of the integrated circuit.
    Type: Grant
    Filed: December 2, 2009
    Date of Patent: December 25, 2012
    Assignee: European Aeronautic Defence and Space Company Eads France
    Inventors: Florent Miller, Cécile Weulersse, Antonin Bougerol, Thierry Carriere, Patrick Heins, Samuel Hazo
  • Publication number: 20120284006
    Abstract: To analyze an electronic component, this component is exposed to a focused laser beam. The information provided by the laser mapping relating to the position and to the depth of the sensitivity zones of the component is used as input parameter in prediction codes for quantifying the sensitivity of the mapped component to ionizing particles in the natural radioactive environment. The prediction codes are used to determine the occurrence of malfunctions in the electronic component. Determination of the risks associated with the radiative environment imposes two aspects: one, probabilistic, takes into account the particle/matter interaction and the other, electrical, takes into account the charge collection inside the electronic component.
    Type: Application
    Filed: October 23, 2008
    Publication date: November 8, 2012
    Applicants: AIRBUS FRANCE, EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE, ASTRIUM SAS
    Inventors: Florent Miller, Nadine Buard, Cecile Weulersse, Thierry Carriere, Patrick Heins
  • Patent number: 8306785
    Abstract: To solve a leakage problem in a box, it is proposed to provide the box with an electronic circuit for measurement of its specific humidity. It is shown that by comparing this current specific humidity to an initial specific humidity and by evaluating the difference found in relation thereto, one has a reliable tool for measuring the permanence of tightness.
    Type: Grant
    Filed: March 5, 2008
    Date of Patent: November 6, 2012
    Assignee: European Aeronautic Defence and Space Company EADS France
    Inventors: Bruno Foucher, Vincent Rouet
  • Patent number: 8252134
    Abstract: According to the invention, one or more thermoplastic sheets (NdT: “feuilles thermoplastique” in the original) (2) are applied on a flat or curved tool (13), and strips (NdT: “des bande” in the original) of a polymer are applied and pressed onto the sheets (2). They are maintained by suction pumps (8), the orifices (4) of which open into a closed volume or one substantially delimited by a sealing joint (3) and occupied by a draining fabric (7). The heating treatment concomitant to the deposition to harden or consolidate the prepreg softens the sheets (2), distorts them to the curvature of the tool (13) and incorporates them in the structure of the prepreg. Application to methods of draping parts with composite material.
    Type: Grant
    Filed: February 5, 2008
    Date of Patent: August 28, 2012
    Assignee: European Aeronautic Defence and Space Company-EADS France
    Inventor: Eric Soccard
  • Publication number: 20120147384
    Abstract: A strain gauge includes a substrate (2) for mounting an element (3) to be reversibly lengthened by a force applied while displaying a variation in the resistance thereof, the element (3) lengthening itself along an axis for measurement by the gauge. The gauge includes at least one contrast target (5, 6) capable of reflecting an incident light beam, the at least one contrast target (5, 6) being placed on the gauge in a predetermined position that makes it possible to predetermine the center of the axis (4), for measurement by the strain gauge (1), by detecting the position of the at least one contrast target (5, 6).
    Type: Application
    Filed: August 12, 2010
    Publication date: June 14, 2012
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Nicolas Swiergiel, Catherine Bosquet, Sebastien Didierjean
  • Patent number: 8175818
    Abstract: A monitoring device of environmental parameter values of an environment surrounding a system. The device includes a sensor to these parameters, and includes a capability to transmit, in real time, each measurement to a processing unit. The processing unit is installed in the system and includes a capability to filter the transmitted measurements. This processing unit comprises a capability to determine cycles from the measurements thus simplified as well as a capability to calculate, in real time, of a percentage of length of consumed life of the system, from the thus determined cycles.
    Type: Grant
    Filed: January 23, 2007
    Date of Patent: May 8, 2012
    Assignee: European Aeronautic Defence and Space Company EADS France et EADS CCR
    Inventors: Bruno Foucher, Vincent Rouet
  • Publication number: 20120106022
    Abstract: A part (1) includes a structural portion made of an electrically insulating or low-conductive composite material (2) and includes, on a surface (11) of the structural portion likely to be subjected to lightning impacts (10), a metallization layer (30) covered with an electrically insulating protection paint (4). The metallization layer includes a layer of a first electrically conductive metal material (31), referred to as HVT material, and includes at least one second electrically conductive metal material (32), referred to as LVT material, having a vaporization temperature ?l substantially lower than the vaporization temperature ?h of the first electrically conductive HVT metal material. A lightning impact results in the vaporization of the LVT material and the removal of the paint on a surface larger than that in which the HVT material is vaporized, and therefore exposes or lifts a portion of the metallization around the lightning impact point, thereby promoting the anchoring of the lightning arc base.
    Type: Application
    Filed: January 7, 2010
    Publication date: May 3, 2012
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Daniel Aliaga, Frederick Cavaliere
  • Publication number: 20120096562
    Abstract: The invention relates to a method for protection of a computer program source code comprising the following steps: translating said source code into a target code, generating an object code starting from said target code, applying an obfuscation program to protect said source code. According to the invention, the obfuscation step is executed after the source code has been translated into target code and before the generation of said object code.
    Type: Application
    Filed: February 23, 2010
    Publication date: April 19, 2012
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY-EADS FRANCE
    Inventor: Fabrice Desclaux
  • Publication number: 20120070237
    Abstract: A tool holder for a machining tool includes a cooling means for a compressed air blowing tool and a device for cooling air compressed by a vortex tube device. The tool holder is generally cylindrical and the vortex tube device advantageously includes a plurality of vortex tubes placed annularly around the axis of the cylinder and the cold air outputs of which are directed at the tool held by the tool holder.
    Type: Application
    Filed: July 17, 2009
    Publication date: March 22, 2012
    Applicants: E.P.B., EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE, SARL ALBRET
    Inventors: Delphine Allehaux, Patrice Rabate, Alain Freyermuth, Jean Bernard Cledat, Jean-Pierre Fantin, Ugo Masciantonio
  • Publication number: 20120067544
    Abstract: Device for cooling a rotating tool mounted on a machine, including elements for generating a continually renewed first flow of air, external to the tool and around the tool, at a high flow rate, produced via a Coanda-effect flow amplifier device realized in a housing fixed on the machine around the tool holder connected to a source of pressurized air.
    Type: Application
    Filed: November 25, 2009
    Publication date: March 22, 2012
    Applicant: European Aeronautic Defence and Space Company Eads France
    Inventors: Clement Dunant-Chatellet, Bruno Thomas
  • Publication number: 20120051627
    Abstract: The invention relates to a method for virtually expanding and enriching the field of view of the current image of a scene described by a video including several images. This method includes the following steps of: a—expanding said field of view by at least one mosaic obtained from said images and by inserting at least one contextual datum in the reference frame of the current image of said scene, b—enriching said field of view by at least one piece of information referenced in said contextual datum.
    Type: Application
    Filed: April 2, 2010
    Publication date: March 1, 2012
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY-EADS FRANCE
    Inventor: Denis Marraud
  • Publication number: 20120039506
    Abstract: The invention concerns a method for identifying an object in a video archive including multiple images acquired in a network of cameras including a phase of characterisation of the object to be identified and a phase of searching for the said object in the said archive, where the said characterisation phase consists in defining for the said object at least one semantic characteristic capable of being extracted, even in low-resolution images, from the said video archive.
    Type: Application
    Filed: August 26, 2009
    Publication date: February 16, 2012
    Applicant: European Aeronautic Defence and Space Company - EADS France
    Inventors: Marc Sturzel, Frédéric Jurie
  • Publication number: 20120025864
    Abstract: The invention relates to a device for testing a circuit made up of a printed circuit board on which components, preferably dummy components, are assembled by means of solder connections. The testing device comprises an enclosure for subjecting the circuit under test to a schedule of thermo-mechanical and/or vibration constraints. The testing device comprises a hardware portion comprising bridges of electrical resistors, a software portion comprising means for setting a detection criterion representing damage to one or more solder connections and for displaying the results of the test, an input/output interface for converting each electrical resistor measurement of the tested chains of solder connections into data that can be used by the software portion, and adjustment means for modifying a criterion for detecting damage to the solder connections.
    Type: Application
    Filed: December 15, 2009
    Publication date: February 2, 2012
    Applicant: European Aeronautic Defence and Space Company Eads France
    Inventors: Katell Moreau, Marc Grieu
  • Publication number: 20110276832
    Abstract: A method for processing a sequence of fault messages occurring in a device including many systems, makes it possible to discriminate between fault messages most likely originating from a real system fault and fault messages without any real fault in the associated system (no fault found), characterized in that the method combines: an “air-side” method (100) executed in real time for acquiring fault message data defining sequences stored in a fault database and for immediate diagnosis assistance using a diagnostics tool, and a “ground-side” method (200) for the subsequent analysis of fault sequence data and for improving the diagnostics tool.
    Type: Application
    Filed: November 16, 2009
    Publication date: November 10, 2011
    Applicant: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Nicolas Schneider, Sylvie Delprat
  • Publication number: 20110231125
    Abstract: A detection wire cutter including a conducting wire mechanically secured to a structure that is to be monitored. This wire is electrically powered at one end and at another end feeds back an electrical voltage corresponding to the power supplied, provided that the structure that is to be monitored has not undergone unacceptable mechanical damage. As an improvement, two arrays of wires extending over flat supports in two directions in space are proposed. Each array is powered by a distinct network electrical supply. The two networks extend in layers, with parallel wire portions. The position of a crack does not impede the passage of current between certain terminals, but certain other terminals will no longer receive any current because the crack has broken a network supply general connection between the connection of one wire and that of another.
    Type: Application
    Filed: December 26, 2008
    Publication date: September 22, 2011
    Applicant: European Aeronautic Defence and Space Company EADS France
    Inventors: Sébastien Rolet, Nicolas Dominguez