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    AIRCRAFT AND METHOD OF FITTING OUT SUCH AN AIRCRAFT
    61.
    发明申请
    AIRCRAFT AND METHOD OF FITTING OUT SUCH AN AIRCRAFT 有权
    飞机和搭载这种飞机的方法

    公开(公告)号：US20160167796A1

    公开(公告)日：2016-06-16

    申请号：US14966028

    申请日：2015-12-11

    Applicant: AIRBUS GROUP SAS

    Inventor： Emmanuel JOUBERT ,  Benoit FERRAN ,  Antonin SANITAS ,  Germain MORIN

    IPC: B64D27/24 ,  F02B61/06 ,  F02B65/00 ,  B64D37/02

    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.

    Abstract translation: 飞机（10）包括：至少一个电动机（135）; 向所述电动马达供电的至少一个独立电源（110,120）; 被称为“辅助推进元件”的推进元件（130）包括：向电动机供电的独立电源（130），将热能转换成电能并将电力供应到 电动机和内燃机; 以及构造成将每个电动机，每个独立电源和辅助推进元件集成的结构（100），所述结构的参数基本上相同，而与辅助推进元件无关。 还描述了装配这种飞行器的方法。

    AIRBAG PROTECTION SYSTEM
    62.
    发明申请
    AIRBAG PROTECTION SYSTEM 审中-公开
    安全气囊保护系统

    公开(公告)号：US20160167793A1

    公开(公告)日：2016-06-16

    申请号：US14970570

    申请日：2015-12-16

    Applicant: AIRBUS GROUP SAS

    Inventor： Jean-Francois GENESTE

    IPC: B64D25/02 ,  B60R21/231

    CPC classification number: B64D25/02 ,  B60R19/205 ,  B60R21/231 ,  B64D25/00 ,  B64D2201/00 ,  B64G1/62

    Abstract: A protection system (15) includes an inflatable bag (16) connected to inflation elements able and intended to be activated so as to inflate the inflatable bag in the event of and/or upon the prediction of an impact. The inflatable bag (16) has a substantially annular overall shape when inflated. Such a protection system (15) is advantageously intended to protect the passengers in a helicopter.

    Abstract translation: 保护系统（15）包括连接到能够且预期被启动的充气元件的充气袋（16），以便在预测碰撞和/或预测碰撞的情况下使充气袋膨胀。 充气袋（16）在膨胀时具有基本环形的整体形状。 这种保护系统（15）有利地用于保护直升机中的乘客。

    ELECTRIC PROPULSION ASSEMBLY FOR AN AIRCRAFT
    63.
    发明申请
    ELECTRIC PROPULSION ASSEMBLY FOR AN AIRCRAFT 审中-公开
    电动推进装置

    公开(公告)号：US20160137305A1

    公开(公告)日：2016-05-19

    申请号：US14898127

    申请日：2014-06-13

    Applicant: AIRBUS GROUP SAS

    Inventor： EMMANUEL JOUBERT ,  HICHEM SMAOUI ,  CHARLES NESPOULOUS ,  BRUNO RECHAIN

    IPC: B64D27/24 ,  B64D33/10 ,  B64D29/02

    CPC classification number: F04D29/5813 ,  B64D27/24 ,  B64D29/02 ,  B64D33/08 ,  B64D33/10 ,  B64D2033/024 ,  F04D25/068 ,  F04D25/0693 ,  F04D25/08 ,  F04D25/082 ,  F04D25/12 ,  F04D29/5806 ,  F04D29/584 ,  Y02T50/44 ,  Y02T50/64

    Abstract: An electric propulsion assembly for an aircraft includes a nacelle having a nacelle cowl which defines an inner space for arranging an electric propulsion unit, which includes a blower, of the aircraft. An electric motor assembly is placed in the inner space and connected to the propulsion unit to supply power to the propulsion unit. An airflow generated by the blower flows in a space between the motor assembly and the nacelle cowl defining a duct to supply thrust to the aircraft. A power electronics system has at least one heat exchanger to transfer thermal energy from the system to a work fluid to cool the system. The heat exchanger is placed to project at least partially into the duct, so that the work fluid consists of the air flow generated by the blower.

    Abstract translation: 用于飞机的电推进组件包括具有机舱罩的机舱，其限定用于布置飞机的包括鼓风机的电推进单元的内部空间。 电动机组件放置在内部空间中并连接到推进单元以向推进单元供电。 由鼓风机产生的气流在电动机组件和机舱罩之间的空间中流动，限定出一个管道以向飞行器提供推力。 电力电子系统具有至少一个热交换器以将热能从系统传递到工作流体以冷却系统。 热交换器被放置成至少部分地投入到管道中，使得工作流体由鼓风机产生的气流组成。

    Marking of the tool center and of the orientation of an acoustic probe in a reference frame, by ultrasound method
    66.
    发明授权
    Marking of the tool center and of the orientation of an acoustic probe in a reference frame, by ultrasound method 有权

    公开(公告)号：US10201899B2

    公开(公告)日：2019-02-12

    申请号：US15106809

    申请日：2014-12-22

    Applicant: AIRBUS GROUP SAS

    Inventor： Louis Le Pinru ,  Nicolas Colin ,  Guillaume Ithurralde

    IPC: B25J9/16

    Abstract: A process for marking the real position and real orientation of a tool in relation to the manipulator arm of a robot. The process utilizes the amplitude measurements of acoustic signals and the flight time measurement of the acoustic waves emitted by an acoustic probe of the tool and reflected by the fixed reference elements. The position of the center of reference of the probe relative to the end of the manipulator arm is determined. The axes X and Y defining the plane of the probe along reference axes X′ and Y′ of known orientations are oriented so that the modification of the position and of the orientation of the probe in the reference frame can be defined. The displacements of the manipulator arm are managed by the controller based on the position of the probe in relation to the manipulator arm and the reference orientation of the probe.

    MARKING OF THE TOOL CENTER AND OF THE ORIENTATION OF AN ACOUSTIC PROBE IN A REFERENCE FRAME, BY ULTRASOUND METHOD
    70.
    发明申请
    MARKING OF THE TOOL CENTER AND OF THE ORIENTATION OF AN ACOUSTIC PROBE IN A REFERENCE FRAME, BY ULTRASOUND METHOD 审中-公开
    工具中心的标记和参考框架中的声学探针的方向，通过超声方法

    公开(公告)号：US20170008173A1

    公开(公告)日：2017-01-12

    申请号：US15106809

    申请日：2014-12-22

    Applicant: AIRBUS GROUP SAS

    Inventor： LOUIS LE PINRU ,  NICOLAS COLIN ,  GUILLAUME ITHURRALDE

    IPC: B25J9/16

    CPC classification number: B25J9/1692 ,  B25J9/1694 ,  G05B2219/37014 ,  G05B2219/37269 ,  G05B2219/39022 ,  Y10S901/09

    Abstract: A process for marking the real position and real orientation of a tool in relation to the manipulator arm of a robot. The process utilizes the amplitude measurements of acoustic signals and the flight time measurement of the acoustic waves emitted by an acoustic probe of the tool and reflected by the fixed reference elements. The position of the center of reference of the probe relative to the end of the manipulator arm is determined. The axes X and Y defining the plane of the probe along reference axes X′ and Y′ of known orientations are oriented so that the modification of the position and of the orientation of the probe in the reference frame can be defined. The displacements of the manipulator arm are managed by the controller based on the position of the probe in relation to the manipulator arm and the reference orientation of the probe.

    Abstract translation: 用于标记相对于机器人的操纵臂的工具的实际位置和实际取向的过程。 该过程利用声学信号的幅度测量和由工具的声学探针发射并由固定参考元件反射的声波的飞行时间测量。 确定探头相对于机械手臂端部的参考点的位置。 沿着已知取向的参考轴X'和Y'限定探头的平面的轴线X和Y被定向成可以限定探针在参考系中的位置和取向的修改。 基于探针相对于操纵臂的位置和探针的参考方位，由控制器管理操纵臂的位移。

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