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    DEVICE FOR TRANSPORTING A PASSENGER FROM DOOR TO DOOR
    34.
    发明申请
    DEVICE FOR TRANSPORTING A PASSENGER FROM DOOR TO DOOR 审中-公开

    公开(公告)号：US20170327244A1

    公开(公告)日：2017-11-16

    申请号：US15525047

    申请日：2015-11-05

    Applicant: AIRBUS GROUP SAS

    Inventor： EMMANUEL BLANVILLAIN

    IPC: B64F1/30

    CPC classification number: B64F1/30

    Abstract: A transportation device to transport a passenger from door to door. The device includes a platform equipped with wheels to move along the ground, and at least one private seat having a power source and a connector. The private seat is secured to the platform. The transportation device further includes a connected virtual reality unit that can construct a virtual environment for the passenger. Additionally, a method for transporting a passenger using the transportation device.

    METHOD AND ASSEMBLY FOR LOCATING ELECTROSTATIC DISCHARGES ON AIRCRAFT IN FLIGHT
    37.
    发明申请
    METHOD AND ASSEMBLY FOR LOCATING ELECTROSTATIC DISCHARGES ON AIRCRAFT IN FLIGHT 审中-公开

    公开(公告)号：US20170261539A1

    公开(公告)日：2017-09-14

    申请号：US15531895

    申请日：2015-11-30

    Applicant: AIRBUS GROUP SAS

    Inventor： Ivan REVEL ,  Gilles PERES

    IPC: G01R31/00

    CPC classification number: G01R31/001 ,  G01R31/008

    Abstract: A method for locating electrostatic discharges occurring on an aircraft in flight including a step of recording, during the flight of the aircraft, electromagnetic signals resulting in the electrostatic discharges and received by a plurality of detectors arranged at different places on an exterior surface of the aircraft, a step of analyzing the signals recorded during the flight, each of the signals, received by the various detectors and corresponding to one and the same electrostatic discharge, are processed to identify at least one zone of an exterior surface of the aircraft, determining a structural part in which the electrostatic discharge probably occurred.

    PROCESS FOR MANUFACTURING A THERMOPLASTIC COMPOSITE PART
    39.
    发明申请
    PROCESS FOR MANUFACTURING A THERMOPLASTIC COMPOSITE PART 审中-公开
    制造热塑性复合材料部件的工艺

    公开(公告)号：US20160311180A1

    公开(公告)日：2016-10-27

    申请号：US15103679

    申请日：2014-12-12

    Applicant: AIRBUS GROUP SAS

    Inventor： Eric SOCCARD

    IPC: B29C70/54 ,  B29C71/02 ,  B29C70/88 ,  B29C33/16 ,  B29C70/30

    Abstract: This process for producing a thermoplastic composite part by laying of at least one thermoplastic composite layer on a tool includes laying on the tool a hardened first ply before the laying of the thermoplastic composite layer. The first ply is produced beforehand to the shape of the tool and includes a first material able to experience an attractive force when it is subjected to a magnetic field, and/or to an electrical potential difference, and includes a second material of a thermoplastic resin that is chemically compatible with the resin of the thermoplastic composite layer. The first ply is clamped to the tool by the effect of a magnetic field, and/or of an electrical potential difference, established at the level of the tool. In one form of implementation, the first ply is produced on a first-ply mold that is preferably of convex shape.

    Abstract translation: 用于通过在工具上铺设至少一个热塑性复合材料层来生产热塑性复合材料部件的该方法包括在铺设热塑复合材料层之前在工具上铺设硬化的第一层。 第一层预先制成工具的形状，并且包括能够在经受磁场和/或电位差时经受吸引力的第一材料，并且包括热塑性树脂的第二材料 其与热塑性复合层的树脂化学相容。 通过在工具水平上建立的磁场和/或电位差的作用将第一层夹紧到工具上。 在一种实施方式中，第一层是在优选为凸形的第一层模上生产的。

    METHOD FOR THE NON-DESTRUCTIVE ULTRASONIC TESTING OF A PART BY ECHO ANALYSIS
    40.
    发明申请
    METHOD FOR THE NON-DESTRUCTIVE ULTRASONIC TESTING OF A PART BY ECHO ANALYSIS 审中-公开
    通过ECHO分析进行部分非破坏性超声波测试的方法

    公开(公告)号：US20160223495A1

    公开(公告)日：2016-08-04

    申请号：US14917739

    申请日：2014-09-09

    Applicant: AIRBUS GROUP SAS

    Inventor： Nicolas DOMINGUEZ ,  Frank GUIBERT

    IPC: G01N29/14 ,  G01N29/36 ,  G01N29/07

    CPC classification number: G01N29/14 ,  G01N29/07 ,  G01N29/11 ,  G01N29/30 ,  G01N29/36 ,  G01N29/4463 ,  G01N29/46 ,  G01N2291/011 ,  G01N2291/015 ,  G01N2291/044

    Abstract: A method for the non-destructive ultrasonic testing of a part by the analysis of echoes returned by the part in response to the emission of an ultrasonic wave via an ultrasonic transducer, includes a step of determining a variable gain curve and a step of correcting the amplitude of the echoes returned by the part according to the variable gain curve and the moments of reception of the echoes. The method further includes steps of: producing a wave function representative of an ultrasonic transducer; producing transfer functions Fm representative of the frequency responses of reference samples Rm of the material forming the part; and calculating reference attenuation values between the wave function and the results of calculations of filtering of the wave function by the respective transfer functions Fm of the reference samples Rm.

    Abstract translation: 通过分析响应于通过超声波换能器发射超声波的部分返回的回波而对部分进行非破坏性超声波测试的方法包括确定可变增益曲线的步骤和校正步骤 根据可变增益曲线部分返回的回波振幅和回波的接收时刻。 该方法还包括以下步骤：产生代表超声换能器的波函数; 产生传递函数Fm代表构成部分的材料的参考样品Rm的频率响应; 以及通过参考样本Rm的相应传递函数Fm计算波函数和波函数的滤波计算结果之间的参考衰减值。

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