公开(公告)号：US20170129163A1

公开(公告)日：2017-05-11

申请号：US15127363

申请日：2015-03-19

Applicant: AIRBUS GROUP SAS

Inventor： Eric SOCCARD

IPC: B29C65/46 ,  B29C65/78 ,  B29C65/36 ,  B29C65/00

CPC classification number: B29C65/46 ,  B29C65/364 ,  B29C65/3676 ,  B29C65/368 ,  B29C65/7841 ,  B29C65/7847 ,  B29C66/00145 ,  B29C66/004 ,  B29C66/0044 ,  B29C66/112 ,  B29C66/131 ,  B29C66/3472 ,  B29C66/3494 ,  B29C66/474 ,  B29C66/524 ,  B29C66/721 ,  B29C66/73921 ,  B29C66/8122 ,  B29C66/8126 ,  B29C66/81431 ,  B29C66/81455 ,  B29C66/81463 ,  B29C66/81821 ,  B29C66/81825 ,  B29C66/836 ,  B29C66/863 ,  B29C66/91651 ,  B29C66/934 ,  B29K2705/00 ,  B29K2995/0008 ,  B29K2863/00 ,  B29K2879/08

Abstract: The device for welding thermoplastic parts includes a matrix for positioning the parts to be assembled, the matrix including an amagnetic insulating insert that defines joining zones in which the welds must be produced, a bladder defining a sealed volume and means for producing a partial vacuum in the sealed volume, and means for moving a magnetic induction head to near the joining zones and without making contact with the bladder. The welding process includes positioning at least one first part, then of placing metal inserts on areas of the first part corresponding to the joining zones that must be welded, and then positioning at least one second part. A bladder is put in place covering the parts and a partial vacuum is created in the volume defined by the bladder. The magnetic induction head is moved to produce the weld bead without contact while the partial vacuum is maintained.

公开(公告)号：US09643713B2

公开(公告)日：2017-05-09

申请号：US14426955

申请日：2013-09-09

Applicant: AIRBUS GROUP SAS

Inventor： Michel Bermudez ,  Didier Mesnage ,  Hichem Smaoui ,  Benoit Fleury

IPC: H01G9/155 ,  B64C7/00 ,  B64D41/00 ,  B64C1/12 ,  B64C1/40 ,  H01G11/58 ,  H01G11/78 ,  B64C1/00

CPC classification number: B64C7/00 ,  B64C1/12 ,  B64C1/40 ,  B64C2001/0072 ,  B64D41/00 ,  H01G11/58 ,  H01G11/78 ,  Y02T50/43 ,  Y10T29/435 ,  Y10T29/49622

Abstract: A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the method.

公开(公告)号：US20160363658A1

公开(公告)日：2016-12-15

申请号：US15102740

申请日：2013-12-11

Applicant: AIRBUS GROUP SAS

Inventor： Guillaume ALLEON ,  Kaushal JADIA ,  Rajan SRINIVASAN ,  Avik SANTRA

IPC: G01S13/00 ,  G01S7/35

CPC classification number: G01S13/006 ,  G01S7/282 ,  G01S7/35 ,  G01S13/106 ,  G01S13/282

Abstract: The invention is an iterative process for performing iteratively the phase retrieval of an adaptive signal x(t) matching two sets of constraint both concerning the time envelope ue(t) of signal x(t) and magnitude distribution Um(f) of its spectral representation. At each iteration k the process computes an estimate {tilde over (x)}k(t) of signal x(t) which is obtained from a first projection PA on a first set of constraint in time domain of a computed value xk(t) of x(t), xk(t) deriving from an estimate {tilde over (X)}k-1(f) of the spectrum of signal x(t), said estimate {tilde over (X)}k-1(f) being itself obtained from a second projection PB on a second set of constraints in spectral domain of the Fourier transform Xk(f) of the estimate {tilde over (x)}k-1(t) of x(t) computed at iteration k−1. Iterative computation of estimate {tilde over (x)}k(t) is repeated until {tilde over (x)}k(t) meets a predefined criterion which indicates that estimate {tilde over (x)}k(t) is close enough to expected signal x(t).

Abstract translation: 本发明是迭代地执行与信号x（t）的时间包络ue（t）和其光谱的幅度分布Um（f）相关的两组约束匹配的自适应信号x（t）的相位检索 表示。 在每次迭代k中，该过程计算在计算值xk（t）的时域中的第一组约束上从第一投影PA获得的信号x（t）的估计{（t））（k） （x）} k-1（f）的估计{tilde over（X）} k-1（f）得出的x（t），xk（t） （f）本身从计算出的x（t）的估计{tilde over（x）} k-1（t）的傅里叶变换Xk（f）的频域的频域的第二组约束获得自身。 在迭代k-1。 重复估计{tilde over（x）} k（t）的迭代计算，直到{tilde over（x）} k（t）满足预定义的标准，这表明估计（波形）超过（x）} k（t） 足以预期信号x（t）。

公开(公告)号：US20160318188A1

公开(公告)日：2016-11-03

申请号：US15107665

申请日：2014-12-23

Applicant: AIRBUS GROUP SAS

Inventor： Adolfo SUAREZ ROOS

IPC: B25J13/08 ,  B25J19/06 ,  B25J19/00

CPC classification number: B25J13/081 ,  B25J19/0091 ,  B25J19/063

Abstract: An impact detection system for a robotic device. The system includes a flexible covering element for enveloping part of the robotic device, the covering element defining an inner air volume, at least one sensor for measuring the differential pressure between the pressure in the inner air volume and the pressure outside the covering element, and a detection unit designed to receive the measuring signal of the at least one sensor, to carry out an analysis, on the basis of the measuring signal, in order to detect a sudden variation in the pressure, and to emit a stop signal to the robotic device when such a variation is detected.

Abstract translation: 一种机器人装置的冲击检测系统。 该系统包括用于包封机器人装置的一部分的柔性覆盖元件，限定内部空气体积的覆盖元件，用于测量内部空气体积中的压力与覆盖元件外部的压力之间的压差的至少一个传感器，以及 检测单元，被设计为接收所述至少一个传感器的测量信号，以基于所述测量信号进行分析，以便检测所述压力的突然变化，并且向所述机器人发出停止信号 检测到这种变化时的装置。

公开(公告)号：US20160291649A1

公开(公告)日：2016-10-06

申请号：US15036802

申请日：2014-11-12

Applicant: AIRBUS GROUP SAS

Inventor： BENOÏT DANTIN

IPC: G06F1/18 ,  G06F1/20

CPC classification number: G06F1/189 ,  G06F1/182 ,  G06F1/20

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.

Abstract translation: 一个电柜，设有互连系统，用于在机柜中接收的计算机等设备。 互连系统包括形成机柜框架的一部分的至少一个波导。 波导设置有面向壳体的开口，用于接收上述装置。 该开口的尺寸被设计成形成通过波导通过的射频无线通信波通过的屏障，并形成对外部波的屏障。

公开(公告)号：US20160276863A1

公开(公告)日：2016-09-22

申请号：US15033960

申请日：2014-10-30

Applicant: AIRBUS GROUP SAS

Inventor： Nicolas COLIN ,  Didier SIMONET

IPC: H02J7/02 ,  G01S19/13 ,  B64C39/02 ,  H02J50/10

CPC classification number: H02J50/15 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/145 ,  G01S19/13 ,  H02J7/025 ,  H02J17/00 ,  H02J50/10 ,  H02J50/80

Abstract: The invention consists of a system allowing remote wireless transfer of energy from a base station to a moving object, in particular a drone, moving in a given zone around the base station. The system includes means for tracking the moving object relative to the base station at any time, means for transmitting a synthetic acoustic wave focused in the direction of the moving object, these two means being located at the base station and powered by the base station, and acoustic reception means, located on the moving object, for receiving the acoustic wave transmitted by the base station and converting the received acoustic wave into an electrical signal and then into a power supply voltage for a battery.

Abstract translation: 本发明包括允许从基站到移动物体（特别是无人机）的能量的远程无线传输的系统，该无人机在基站周围的给定区域内移动。 该系统包括用于在任何时间相对于基站跟踪移动物体的装置，用于发送在移动物体的方向上聚焦的合成声波的装置，这两个装置位于基站并由基站供电， 以及声音接收装置，位于移动物体上，用于接收由基站发射的声波，并将接收的声波转换为电信号，然后转换为电池的电源电压。

公开(公告)号：US20160264262A1

公开(公告)日：2016-09-15

申请号：US15030845

申请日：2014-10-23

Applicant: AIRBUS GROUP SAS

Inventor： NICOLAS COLIN ,  FRANK GUIBERT

IPC: B64F5/00 ,  B25J19/02 ,  G05D1/00 ,  B25J5/00

CPC classification number: G05D1/0038 ,  B25J5/007 ,  B25J19/023 ,  B64F5/60 ,  G01N29/04 ,  G01N29/226 ,  G01N2291/2694 ,  G05B2219/45066 ,  G05D2201/0207 ,  Y10S901/44

Abstract: A device for visually inspecting the external surfaces of an aircraft includes an inspection area to receive an aircraft, at least one visual inspection robot, and a control center. A movable platform of the robot supports a turret having an observation unit. The robot includes a processing unit which guides the movable platform and process the data received from the observation unit. The processing unit of the robot are configured to autonomously control the robot during the visual inspection of the external surfaces of the aircraft parked in the inspection area; to interrupt a visual inspection in the event of a detection of an anomaly on the external surface of the aircraft; to transmit a visual inspection data to the control center; and to receive instructions from the control center.

Abstract translation: 用于视觉检查飞行器的外表面的装置包括用于接收飞行器的检查区域，至少一个目视检查机器人和控制中心。 机器人的可移动平台支撑具有观察单元的转台。 机器人包括：引导可移动平台并处理从观察单元接收的数据的处理单元。 机器人的处理单元被构造成在停泊在检查区域的飞行器的外表面的目视检查期间自动地控制机器人; 在检测飞机外表面的异常情况下中断视觉检查; 将视觉检查数据传送到控制中心; 并从控制中心接收指令。

公开(公告)号：US20160144981A1

公开(公告)日：2016-05-26

申请号：US14898128

申请日：2014-06-11

Applicant: AIRBUS GROUP SAS

Inventor： Emmanuel JOUBERT ,  Charles NESPOULOUS ,  Bruno RECHAIN ,  Hichem SMAOUI

IPC: B64F1/04 ,  B64F1/22 ,  B64C25/32

CPC classification number: B64F1/04 ,  B64C25/32 ,  B64F1/22 ,  B64F1/228 ,  Y02T50/826

Abstract: A device for moving aircraft along the ground includes at least one runway and at least one aircraft. The aircraft is secured to a tractor element having a magnetic mass formed mainly of type II superconductor material and the runway includes stator coils arranged in the runway with at least one line of coils parallel to an axis of the runway. A command/control system supplies power to the stator coils to generate a magnetic field that levitates the tractor element, magnetized beforehand into a phase II superconducting state, above the runway.

Abstract translation: 用于沿着地面移动飞行器的装置包括至少一个跑道和至少一个飞机。 飞机被固定到具有主要由II型超导体材料形成的磁性质量的牵引器元件，并且跑道包括布置在跑道中的定子线圈，其中至少一条线圈平行于跑道的轴线。 指令/控制系统向定子线圈供电以产生使拖拉机元件悬浮的磁场，预先在跑道之上磁化成II级超导状态。

公开(公告)号：US20150356208A1

公开(公告)日：2015-12-10

申请号：US14720772

申请日：2015-05-23

Applicant: AIRBUS GROUP SAS

Inventor： NICOLAS CHEVASSUS ,  DENIS MARRAUD ,  ANTOINE TARAULT ,  XAVIER PERROTTON

IPC: G06F17/50

CPC classification number: G06F17/50 ,  G06T19/006

Abstract: A method for generating a digital mockup in three dimensions using computer-aided design (CAD) software. The digital mockup is integrated into a spatialization environment for the digital mockup allowing visualization of the digital mockup from various angles of view. The digital mockup is produced to obtain a semi-finished product. A plurality of pieces of production information is acquired. For each piece of production information, a spatial position linked to the production information is measured, and the production information is integrated into the spatialization environment on the digital mockup at a position in the digital mockup corresponding to the measured spatial position.

Abstract translation: 一种使用计算机辅助设计（CAD）软件在三维生成数字样机的方法。 数字样机被集成到数字样机的空间化环境中，允许从各种角度观察数字样机。 产生数字样机以获得半成品。 获取多条生产信息。 对于每条生产信息，测量与生产信息相关联的空间位置，并且在对应于测量的空间位置的数字样机中的位置处将生产信息整合到数字样机上的空间化环境中。

公开(公告)号：US10410759B2

公开(公告)日：2019-09-10

申请号：US15527900

申请日：2015-11-19

Applicant: AIRBUS GROUP SAS ,  Gerard Guilbert

Inventor： Didier Mesnage ,  Thierry Pelegrin

IPC: B29C70/88 ,  B32B15/088 ,  B32B15/20 ,  H01B7/00 ,  H01B7/02 ,  H01B7/04 ,  B64C1/06 ,  B29K105/24 ,  B29K77/00 ,  B29K309/08 ,  B29L31/30 ,  B64C1/00

Abstract: A conductive device to form electrical connections on the surface of a structure made of composite material. The device includes a thin interface layer having a face via which the device is fixed to the surface of the structure made of composite material. A conductive metal element is placed on the face of the interface layer opposite the face making contact with the surface of the structure. The conductive element is configured to be able to undergo tensile and compressive stresses without damage. A protective layer is configured to protect the conductive element from attack from the environment surrounding the structure. These various elements are arranged relative to one another such that the length of the conductive element can vary as a function of temperature variations independently of the amplitude of the variations undergone by the structure on which the device is mounted.