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公开(公告)号：US10203732B2
公开(公告)日：2019-02-12
申请号：US15036802
申请日：2014-11-12
Applicant: AIRBUS GROUP SAS
Inventor： Benoît Dantin
Abstract: An electric cabinet provided with an interconnection system for devices such as computers received in the cabinet. The interconnection system includes at least one waveguide forming part of the frame of the cabinet. The waveguide is provided with openings disposed facing housings for receiving the aforementioned devices. The openings being dimensioned to form a barrier to the passage of radio-frequency wireless communication waves to be transmitted through the waveguide and to form a barrier to external waves.
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公开(公告)号：US10203051B2
公开(公告)日：2019-02-12
申请号：US15528185
申请日：2015-11-19
Applicant: AIRBUS GROUP SAS
Inventor： Benoit Dantin
IPC: F16L9/12 , F16L11/10 , B64D13/00 , F16L11/127 , F16L11/18 , F24F13/02 , F16L11/02 , B29D23/00 , B29K75/00 , B29K83/00 , B29K309/08 , B29L23/00
Abstract: A pipe for forming air flow pipelines in a structure that includes a flexible tube made from composite material, the tube having, on the length of same, sections for which the wall of the tube is stiffened by means of structural elements made from a rigid composite material incorporated into the wall of the tube. The structural elements are configured and arranged at the surface of the tube in such a way as to form a lattice framework surrounding the wall of the tube. The pipe further includes electrical conductors, disposed longitudinally on the wall of the pipe, the electrical conductors having a straight path at the stiffened sections of the pipe and a meandering path at certain of the non-stiffened sections of the pipe, the meandering allowing the conductor to tolerate the possible twisting of the pipe when it is installed in the structure.
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公开(公告)号：US10044996B2
公开(公告)日：2018-08-07
申请号：US14719307
申请日：2015-05-21
Applicant: AIRBUS GROUP SAS
Inventor： Nicolas Chevassus , Denis Marraud , Antoine Tarault , Xavier Perrotton
IPC: H04N9/31 , G06K9/00 , G09F19/18 , G03B17/54 , G01N21/956
Abstract: A method for projecting information issued from a digital design model. Calibration is performed by acquiring characteristic data originating from a surface of interest and comparing the characteristic data with virtual data issued from the digital design model. A spatial position of a projecting device is determined. The projecting device comprises a video projector and at least two separate image-capturing devices. Depending on the spatial position, information issued from the digital design model is projected by the video projector onto the surface of interest.
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公开(公告)号：US10017264B2
公开(公告)日：2018-07-10
申请号：US14966028
申请日：2015-12-11
Applicant: AIRBUS GROUP SAS
Inventor： Emmanuel Joubert , Benoit Ferran , Antonin Sanitas , Germain Morin
CPC classification number: B64D27/24 , B64D37/02 , B64D41/00 , B64D2027/026 , F02B61/06 , F02B65/00 , Y02T50/64 , Y10S903/951
Abstract: The aircraft (10) includes: at least one electric motor (135); at least one stand-alone electrical power supply (110, 120) supplying power to the electric motor; propulsion elements (130) referred to as “auxiliary propulsion elements”, included in the group including: a stand-alone electrical power supply (130) supplying power to the electric motor, a power supply converting thermal energy into electrical energy and supplying power to the electric motor, and an internal combustion engine; and a structure (100) configured to integrate each electric motor, each stand-alone electrical power supply and the auxiliary propulsion elements, the parameters of the structure being substantially identical regardless of the auxiliary propulsion elements. A method of fitting out such an aircraft is also described.
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5.发明申请公开(公告)号：US20170368782A1
公开(公告)日：2017-12-28
申请号：US15527976
申请日：2015-11-18
Applicant: AIRBUS GROUP SAS
Inventor： Albert ABISROR , Didier MESNAGE
IPC: B32B1/00 , B32B7/08 , B32B7/12 , B32B9/02 , B32B5/02 , B32B27/06 , B32B27/12 , B32B37/12 , B32B9/04 , B32B5/18 , B32B38/00 , B64B1/08 , B64B1/40 , B64G1/22 , B64C3/30
CPC classification number: B32B1/00 , B29C66/1122 , B29C66/30341 , B29C66/304 , B29C66/432 , B29C66/4326 , B29C66/45 , B29C66/49 , B29C66/729 , B29D22/02 , B29K2713/00 , B29L2009/00 , B29L2022/02 , B29L2031/3097 , B32B5/028 , B32B5/18 , B32B7/08 , B32B7/12 , B32B9/02 , B32B9/045 , B32B27/065 , B32B27/12 , B32B37/12 , B32B2038/008 , B32B2250/40 , B32B2262/02 , B32B2262/0269 , B32B2262/106 , B32B2266/02 , B32B2266/0221 , B32B2305/022 , B32B2305/18 , B32B2307/50 , B32B2307/7166 , B32B2457/12 , B32B2605/18 , B64B1/08 , B64B1/14 , B64B1/40 , B64C3/30 , B64G1/22 , B64G1/222 , B64G1/62 , B64G1/66 , B64G2001/224
Abstract: A multilayer sealed skin, in particular for an inflatable structure and that includes a first polymer film, a reinforcing fabric disposed on the first polymer film and a second polymer film disposed on the reinforcing fabric and adhered by means of an adhesive to the first polymer film through cavities in the reinforcing fabric. The skin can be applied to the production of an inflatable structural element such as an inflatable beam for which the skin forms an outer wall of the structural element and for which the first film of the skin forms an inner face of the outer wall of the structural element, and the second film forms an outer face of the wall.
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Patent Agency Ranking
6.发明申请公开(公告)号：US20170348924A1
公开(公告)日：2017-12-07
申请号：US15539128
申请日：2015-12-18
Applicant: AIRBUS GROUP SAS
Inventor： STÉPHANE AUFFRAY
CPC classification number: B29C70/546 , B29C70/48 , G01N15/0826 , G01N29/07 , G01N29/11 , G01N29/222 , G01N29/46 , G01N2291/011 , G01N2291/012 , G01N2291/015 , G01N2291/0251
Abstract: An ultrasonic device to characterize the flow of resin entering and exiting an injection mold during the phase of impregnation, by the resin, of a preform contained in the mold. The device includes two ultrasonic sensors arranged respectively in the vicinity of the inlet port where the resin enters the mold and in the vicinity of the outlet port where the resin exits the mold. Each sensor emits an ultrasonic wave towards the end of the mold in the vicinity of which it is positioned, and receives the ultrasonic wave reflected by the medium. Preferably, the device determines the stabilization of the flow of resin passing through the mold based on the signals received by the sensors. A method for implementing the device to determine the completeness of the operation of impregnating, with resin, a preform positioned in an injection mold into which the resin is introduced.
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公开(公告)号：US20170328497A1
公开(公告)日：2017-11-16
申请号：US15528185
申请日：2015-11-19
Applicant: AIRBUS GROUP SAS
Inventor： Benoit DANTIN
IPC: F16L11/10 , F24F13/02 , F16L11/18 , F16L11/127 , B64D13/00 , F16L11/02 , B29D23/00 , B29L23/00 , B29K309/08 , B29K83/00 , B29K75/00
CPC classification number: F16L11/10 , B29D23/00 , B29K2075/00 , B29K2083/00 , B29K2309/08 , B29L2023/005 , B64D13/00 , F16L11/02 , F16L11/127 , F16L11/18 , F24F13/0218 , F24F13/0254 , Y02T50/44
Abstract: A pipe for forming air flow pipelines in a structure that includes a flexible tube made from composite material, the tube having, on the length of same, sections for which the wall of the tube is stiffened by means of structural elements made from a rigid composite material incorporated into the wall of the tube. The structural elements are configured and arranged at the surface of the tube in such a way as to form a lattice framework surrounding the wall of the tube. The pipe further includes electrical conductors, disposed longitudinally on the wall of the pipe, the electrical conductors having a straight path at the stiffened sections of the pipe and a meandering path at certain of the non-stiffened sections of the pipe, the meandering allowing the conductor to tolerate the possible twisting of the pipe when it is installed in the structure.
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8.发明申请公开(公告)号：US20170190124A1
公开(公告)日：2017-07-06
申请号：US15387655
申请日：2016-12-22
Applicant: AIRBUS GROUP SAS
Inventor： MARC DOUILLY , PATRICE RABATE , HUGO FALGARONE
CPC classification number: B29C70/745 , B29C70/84 , B29K2105/20 , B33Y10/00 , B33Y30/00 , B33Y50/02 , B64F5/10 , G05B19/4099 , G05B19/41805 , G05B2219/35062 , G05B2219/37205 , G05B2219/40613 , Y02P80/40 , Y02P90/04 , Y02P90/26
Abstract: A device to correct geometrical differences of surfaces of parts to be assembled at the interface of the assembly. A measurer to acquire data by measuring the geometry of the assembly surfaces of two parts to be assembled to each other with their respective assembly surfaces facing. A simulator configured to simulate the assembly of the parts and to determine from the acquired data at each measured point of a sampling of the interface a thickness of the void resulting from the geometrical discrepancies between the assembly surfaces. An additive fabricator to receive from the simulator data representative of the thicknesses of the voids resulting from the geometrical discrepancies between the assembly surfaces. The additive fabricator configured to deposit material on the assembly surface of at least one of the parts to at least partly fill the void resulting from the geometrical discrepancies between the assembly surfaces.
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公开(公告)号：US20170129194A1
公开(公告)日：2017-05-11
申请号：US15300388
申请日：2015-04-02
Applicant: AIRBUS GROUP SAS
Inventor： Jacques CINQUIN
CPC classification number: B29C70/443 , B29C35/0272 , B29C35/0288 , B29C70/40 , B29C70/54 , B29C2033/023 , B29C2035/0211 , B29K2105/0845 , B29L2009/00
Abstract: A process and installation for producing a composite material part in which plies of continuous and electrically conductive fibres are deposited to form a stack of piles on a substrate. At least the face of the substrate bearing the stack is electrically insulating and the following steps are carried out a) an electrical terminal is inserted between the ends of at least two plies placed directly one on top of the other in the stack, and on at least two opposite sides of these plies b) when the fibres are dry, introducing a resin in order to impregnate the fibres and c) making a current flow between the electrical terminals through the plies in order to set the resin by resistive heating.
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公开(公告)号：US20160248267A1
公开(公告)日：2016-08-25
申请号：US15025993
申请日：2014-09-30
Applicant: AIRBUS GROUP SAS , AIRBUS DEFENCE AND SPACE SAS
Inventor： Benoit FLEURY , Gregor MASSIOT , Pierre-Bertrand LANCELEVEE , Julien LABBE
CPC classification number: H02J7/0042 , B64D2221/00 , G06F17/5009 , H02J4/00 , H02J7/0063 , H02J7/345
Abstract: A method for optimizing the architecture of the power supply of a load, includes the following steps: determination of a mission profile (16) sizing according to the power required by the load over time; definition of the sources of energy storage for hybridization; association of a characteristic behavior model with each source of energy storage; determination of the couples of sources of energy storage that can generate the mission profile with a minimum mass; and determination, from the potential couples of sources of energy storage, of the couple with the weakest mass.
Abstract translation: 一种用于优化负载电源结构的方法包括以下步骤：根据负载所需的功率随时间确定任务简档（16）尺寸大小; 定义用于杂交的能量储存来源; 特征行为模型与每个能量储存源的关联; 确定能够以最小质量生成任务简档的能量存储源的夫妇; 并从能量储存来源的潜在夫妻中确定这对夫妇与最弱的群体。
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