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11.发明申请公开(公告)号：US20160136736A1
公开(公告)日：2016-05-19
申请号：US14716868
申请日：2015-05-19
Applicant: AIRBUS GROUP SAS
Inventor： FERNAND VINHAS , DANIEL ALIAGA , GUILLAUME ABRIVARD , DOMINIQUE SCHUSTER
IPC: B23B41/00
CPC classification number: B23B41/00 , B23B35/00 , B23B51/00 , B23B2222/28 , B23B2222/88 , B23B2226/275 , B23B2226/31 , B23B2228/36 , B23B2251/14 , B23B2251/202 , B23B2251/204 , B23B2265/12
Abstract: A method for drilling through an assembly forming a stack of at least two different materials uses a drill bit having at least a first cutting edge and a second cutting edge inclined in an axial plane of the drill bit so that the end of the drill bit has a projecting conical shape. The first cutting edge is configured to drill a first material. The second cutting edge is made differently from the first cutting edge, to drill a second material. A first rotational drive axis of the drill bit is laterally offset during the drilling by an offset distance D relative to the axis of the drill bit in a direction opposite the first cutting edge when the drill bit is drilling through the first material, and alternately, in a direction opposite the second cutting edge when the drill bit is drilling through the second material.
Abstract translation: 用于钻穿通过组装至少两种不同材料的组件的组件的方法使用具有至少第一切削刃和在钻头的轴向平面中倾斜的第二切削刃的钻头，使得钻头的端部具有 突出的圆锥形。 第一切削刃被配置成钻第一材料。 第二切削刃与第一切削刃不同，以钻出第二材料。 当钻头穿过第一材料时，钻头的第一旋转驱动轴线在钻孔过程中沿相对于第一切削刃的方向相对于钻头的轴线的偏移距离D横向偏移， 当钻头穿过第二材料时，在与第二切削刃相对的方向上。
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公开(公告)号：US20150339819A1
公开(公告)日：2015-11-26
申请号：US14714273
申请日：2015-05-16
Applicant: AIRBUS GROUP SAS
Inventor： NICOLAS CHEVASSUS , DENIS MARRAUD , ANTOINE TARAULT , XAVIER PERROTTON
CPC classification number: G06T7/80 , G06F3/005 , G06T7/251 , G06T7/70 , G06T19/006 , G06T2207/10004 , G06T2207/10016 , G06T2207/30244 , G06T2215/16 , H04N5/232
Abstract: A method for processing local information acquired by a virtual representation and a device having an inertial unit and an image sensor. At least one image of a real environment of the device is captured. The localization of the device in the virtual representation, corresponding to the localization of the device in the real environment, is obtained by correlating the portions of the captured image and portions of the virtual representation, The inertial unit determines the displacement of the device. The localization of the device in the virtual representation is modified as a function of the displacement so that the real position of the device corresponds, during the displacement, to the localization of the device in the virtual representation.
Abstract translation: 一种用于处理由虚拟表示获取的本地信息的方法和具有惯性单元和图像传感器的设备。 捕获设备的真实环境的至少一个图像。 通过将捕获的图像的部分和虚拟表示的部分相关联来获得对应于设备在真实环境中的定位的虚拟表示中的设备的定位。惯性单元确定设备的位移。 虚拟表示中的设备的定位被修改为位移的函数，使得设备的实际位置在位移期间对应于虚拟表示中的设备的定位。
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公开(公告)号：US11123962B2
公开(公告)日：2021-09-21
申请号：US15510684
申请日：2015-09-14
Applicant: AIRBUS GROUP SAS , ADHETEC
Inventor： Elisa Campazzi , Marie-Paule Guillou , Nicolas Mouyen
IPC: C09J7/22 , C09J7/30 , C09J7/38 , B29C51/02 , B64D45/00 , B32B3/14 , B32B7/05 , B32B7/12 , B32B27/00 , B32B27/06 , B32B27/32 , B32B27/40 , B32B37/12 , B32B27/28 , B29C51/00 , B29K105/00 , B29K71/00 , B29K75/00 , B29K23/00 , B29C63/00 , B64D15/00
Abstract: A multilayer thermoformable film to protect the surface of a workpiece includes an underlayer having first and second faces. The underlayer is made from an adhesive material configured to adhere to the surface of the workpiece by the first face. At least one layer of polymer material is attached to the second face of the adhesive underlayer. The layer of polymer material is resistant to erosion by solid particles and to erosion by liquid particles. It is formed from a polymer material chosen from a polyurethane, a polyether ether ketone and a polyethylene having a very high molecular weight, with a Shore D hardness of between 50 and 65 D. A method of surface protection of the workpiece includes thermoforming the film in a shape adapted to match the shape of at least a portion of the workpiece and applying the film thermoformed onto the surface of the workpiece.
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14.发明授权公开(公告)号：US10882201B2
公开(公告)日：2021-01-05
申请号：US15781907
申请日：2016-12-07
Applicant: AIRBUS GROUP SAS
Inventor： Benjamin Campagne , Gwenole Le Moal
Abstract: A method and device for cutting materials for manufacturing parts according to which an image of a cutting line is made recurrently downstream from a cutting head. The images produced are analyzed in real time to calculate amplitudes of deviations in the quality of the surface profiles of the cutting line as the part is being cut and comparing the calculated amplitudes to at least one predefined threshold value. The cutting is stopped in the event of the at least one threshold value being exceeded.
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公开(公告)号：US10450092B2
公开(公告)日：2019-10-22
申请号：US15102980
申请日：2014-12-08
Applicant: AIRBUS GROUP SAS
Inventor： Jean-Francois Geneste
Abstract: A spacecraft includes: a body a surface of revolution connected with the body, and a heat engine positioned at the center of the surface of revolution. The surface of revolution has a substantially open hollow torus shape with a transverse cross-section of a circle and two diametrically opposite portions each having a curvature extending from the circle. A first portion of the diametrically opposite portions has an opening and forms a solar concentrator for concentrating solar radiation in the direction of the heat engine. The first portion forms a primary solar radiation reflector. A second portion of the diametrically opposite portions is coaxial with the first portion and forms a secondary solar radiation reflector. The opening is configured so that the solar radiation passes in the direction of the center of the surface of revolution after reflection at the primary and secondary reflectors.
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Patent Agency Ranking
公开(公告)号：US10354020B2
公开(公告)日：2019-07-16
申请号：US15021243
申请日：2014-09-09
Applicant: AIRBUS GROUP SAS , INSTITUT POLYTECHNIQUE DE GRENOBLE
Inventor： Flavien Boussuge , Lionel Fine , Jean-Claude Leon , Stefanie Hahmann
Abstract: A computer-assisted design method for a second three-dimensional object from a first three dimensional object known only by its boundary surfaces, through a surface model of the B-Rep type, of the planar, cylindrical, cone, sphere, or toroid type, excluding free forms in defining the boundary of the object. The first object is broken down into a set of simple volume primitives. The first object is associated with a construction graph defined from these volume primitives and a set of geometric parameters for using these volume primitives in the specific case of that first object. The construction graph enables a compact description of all of the construction alternatives of the object through Boolean combinations of these primitives. The second object is generated as an alternative of the first object according to that construction graph, by modifying some of these parameters.
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公开(公告)号：US20180042119A1
公开(公告)日：2018-02-08
申请号：US15540828
申请日：2015-12-30
Applicant: AIRBUS GROUP, SAS , MALLARD
Inventor： Benoît DANTIN , Pascal LEMEILLE
IPC: H05K3/14 , C23C28/02 , C23C4/02 , H05K3/10 , C23C4/129 , C23C4/18 , H05K3/46 , C23C24/04 , C23C4/08
CPC classification number: H05K3/14 , C23C4/02 , C23C4/08 , C23C4/129 , C23C4/18 , C23C24/04 , C23C28/021 , H05K1/056 , H05K1/165 , H05K3/102 , H05K3/225 , H05K3/4685 , H05K2201/0341 , H05K2203/1344 , H05K2203/173
Abstract: A structure including at least one electrical line on one surface of the structure, one electrically conductive layer of the line resulting from deposition of an electrically conductive material via a cold spraying method, and the line includes a protective bonding layer on which the electrically conductive material is deposited via the cold spraying method, the protective bonding layer forming a continuous protective shield between the structure and the cold-sprayed material. An insulating layer is advantageously located between the structure and the protective bonding layer. Achieving an electrical line on a surface of the structure involves implementing a step of oxy-fuel flame spraying of a protective material to form a protective bonding layer, followed by a step of cold spraying of the electrically conductive material of the electrically conductive layer onto the protective bonding layer.
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公开(公告)号：US09815152B2
公开(公告)日：2017-11-14
申请号：US15051374
申请日：2016-02-23
Applicant: AIRBUS GROUP SAS
Inventor： Gilles Foucher , François Marie , Daniel Aliaga
CPC classification number: B23P6/04 , B23K20/124 , B23K20/1265 , B23K20/128 , B23K20/22 , B23P6/00
Abstract: A method for repairing a defect affecting a weld. A sheet of filler metal is placed on the surface of the welded part, next to the region of the defect. The sheet is locally welded to the welded part in the region of the defect using a friction stir welding tool having a retractable welding pin. The welded part and the sheet are separated such that the filler metal amalgamated with the metal of the welded part remains in position. The local welding operation includes successively performing the following: setting the welding tool into rotation and putting it under pressure; inserting the pin to a small distance from the anvil while maintaining or increasing the pressure on the shoulder of the welding tool; progressively retracting the pin while maintaining or increasing the pressure on the shoulder; and stopping the pressure on the shoulder when the retractable pin has been retracted.
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公开(公告)号：US09677466B2
公开(公告)日：2017-06-13
申请号：US14966180
申请日：2015-12-11
Applicant: AIRBUS GROUP SAS
Inventor： Hichem Smaoui , Bruno Rechain , Fabien Retho
IPC: F02B65/00 , B64C39/02 , F02B37/00 , F02B33/40 , F01D15/10 , F02C6/12 , F02C6/14 , F02C6/20 , B60K6/24 , B60K6/38 , B60K6/40 , B60K6/44 , B60K6/387 , B60K6/442 , B64D27/02
CPC classification number: F02B65/00 , B60K6/24 , B60K6/387 , B60K6/40 , B60K6/442 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/048 , B64D2027/026 , F01D15/10 , F02B33/40 , F02B37/00 , F02C6/12 , F02C6/14 , F02C6/206 , F05D2220/329 , F05D2220/40 , F05D2220/62 , F05D2220/76 , F05D2220/90 , F05D2260/42 , Y02T10/144 , Y02T10/6234 , Y02T10/6295 , Y02T50/64 , Y02T50/671
Abstract: A method of managing a power demand to assure the operation of a pilotless aircraft. The aircraft includes an internal combustion engine supplying a maximum principal power which can vary. The management method is particularly suitable for a rotary wing pilotless aircraft. It guarantees the storage of an amount of electrical energy at least equal to a recovery energy of the aircraft in the event of failure of the internal combustion engine. This recovery energy enables the control of autorotation and landing of the aircraft.
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公开(公告)号：US09649699B2
公开(公告)日：2017-05-16
申请号：US14716868
申请日：2015-05-19
Applicant: AIRBUS GROUP SAS
Inventor： Fernand Vinhas , Daniel Aliaga , Guillaume Abrivard , Dominique Schuster
CPC classification number: B23B41/00 , B23B35/00 , B23B51/00 , B23B2222/28 , B23B2222/88 , B23B2226/275 , B23B2226/31 , B23B2228/36 , B23B2251/14 , B23B2251/202 , B23B2251/204 , B23B2265/12
Abstract: A method for drilling through an assembly forming a stack of at least two different materials uses a drill bit having at least a first cutting edge and a second cutting edge inclined in an axial plane of the drill bit so that the end of the drill bit has a projecting conical shape. The first cutting edge is configured to drill a first material. The second cutting edge is made differently from the first cutting edge, to drill a second material. A first rotational drive axis of the drill bit is laterally offset during the drilling by an offset distance D relative to the axis of the drill bit in a direction opposite the first cutting edge when the drill bit is drilling through the first material, and alternately, in a direction opposite the second cutting edge when the drill bit is drilling through the second material.
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