公开(公告)号：US09346540B2

公开(公告)日：2016-05-24

申请号：US14444056

申请日：2014-07-28

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Laurent Tizac ,  Cedric Lesage

IPC: B64C25/50 ,  B64C25/40

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: An elastic device for coupling between an aircraft landing gear wheel and a coaxial motorization member for motorization of the wheel. The elastic device comprises a plurality of arms to be rotationally coupled to the motorization member adjacent a first radially inner end and which are to be linked to the wheel adjacent their radially outer opposite end, the arms being substantially rigid in a plane perpendicular to the rotational axis of the wheel and flexible in directions substantially transverse to the plane.

Abstract translation: 一种用于联接飞行器起落架齿轮和用于车轮机动化的同轴电动构件的弹性装置。 所述弹性装置包括多个臂，所述多个臂可旋转地联接到所述机动构件，邻近所述第一径向内端，并且所述多个臂将被连接到邻近所述轮的径向外相对端的所述轮，所述臂在垂直于所述旋转 车轮的轴线并且基本上横向于该平面的方向是柔性的。

公开(公告)号：US09335156B2

公开(公告)日：2016-05-10

申请号：US14491767

申请日：2014-09-19

Applicant: Airbus Operations (S.A.S.)

Inventor： Benjamin Campagne ,  Franck Bentouhami

IPC: G01N21/00 ,  G01B9/02 ,  G01N29/06 ,  G01N29/22 ,  G01N29/24 ,  G01N21/17 ,  G01B11/06

CPC classification number: G01B9/02091 ,  G01B11/06 ,  G01B11/0675 ,  G01N21/1702 ,  G01N21/4795 ,  G01N29/069 ,  G01N29/225 ,  G01N29/2418 ,  G01N2201/06113 ,  G01N2201/08 ,  G01N2291/0231 ,  G01N2291/2694

Abstract: This disclosure relates to a method for the nondestructive testing, using laser ultrasonics, of a composite part having a fibrous reinforcement in a resin that optically scatters the laser, includes: a) taking a measurement of the thickness of the resin of the part on the surface that is illuminated during the laser shot, which is capable of generating a thermoelastic effect in said resin and which is referred to as an ultrasonic laser shot; b) adjusting the power of the laser of said ultrasonic shot on the basis of the thickness measurement carried out in step a) so as to eliminate any risk of a flash on the reinforcements; and c) producing the ultrasonic laser shot at the power determined during step b). The device used for implementing the method comprises a combined photoacoustic imaging and low time-coherence interferometry (OCT) system.

Abstract translation: 本公开涉及一种使用激光超声波对具有光学散射激光的树脂中的具有纤维增强材料的复合部件进行非破坏性测试的方法，包括：a）测量所述部件的树脂的厚度， 在激光射击期间被照射的表面，其能够在所述树脂中产生热弹性效应，并且被称为超声波激光射击; b）基于在步骤a）中进行的厚度测量来调整所述超声波照射的激光的功率，以消除增强件上的闪光的任何风险; 以及c）以在步骤b）中确定的功率产生所述超声波激光。 用于实现该方法的装置包括组合光声成像和低时间相干干涉测量（OCT）系统。

公开(公告)号：US20160122030A1

公开(公告)日：2016-05-05

申请号：US14926908

申请日：2015-10-29

Applicant: Airbus Operations S.A.S.

Inventor： Jacques Hervé Marche

IPC: B64D27/26

CPC classification number: B64D27/26 ,  B64D2027/262 ,  B64D2027/264 ,  B64D2027/266

Abstract: A front engine attachment, intended to fix an engine to a structure of an aircraft, includes a first attachment including a base intended to be fixed to the structure, a first fixture articulated on the base, two first connecting rods, each being articulated by a first end to the engine and by a second end to the fixture, and a first cylindrical nose mounted on the base. The front engine attachment includes a second attachment including a cradle including an orifice into which the cylindrical nose is fitted, and a second cylindrical nose being threaded into a piercing of the engine, and two second connecting rods, each being intended to be articulated by a first end to the engine, and by a second end to the cradle.

Abstract translation: 用于将发动机固定在飞行器结构上的前部发动机附件包括：第一附件，其包括用于固定在该结构上的基座;铰接在基座上的第一固定件;两个第一连接杆， 第一端连接到发动机，第二端连接到固定装置，以及安装在基座上的第一圆柱形鼻。 前部发动机附件包括第二附件，其包括支架，该支架包括圆柱形鼻部装配到其中的孔口，以及第二圆柱形鼻部，该第二圆柱形鼻部被拧入发动机的穿孔中，以及两个第二连接杆，每个连接杆旨在由一个 第一端到发动机，第二端到支架。

公开(公告)号：US20160091296A1

公开(公告)日：2016-03-31

申请号：US14859714

申请日：2015-09-21

Applicant: Airbus Operations S.A.S.

Inventor： Denis De Mattia ,  Christian Vivier

IPC: G01B7/14 ,  G01N27/02

CPC classification number: G01B7/14 ,  G01N27/02 ,  G01N27/902

Abstract: A method for detecting a spacing defect between two adjacent strands of a layer of a fiber fabric includes displacement of an inductive sensor relative to the fiber fabric, and identification of a defect based on a signal generated by the inductive sensor. The invention also relates to a device for its implementation.

Abstract translation: 用于检测纤维织物层的两个相邻股线之间的间隔缺陷的方法包括感应传感器相对于纤维织物的位移，以及基于由感应传感器产生的信号来识别缺陷。 本发明还涉及一种用于其实现的装置。

公开(公告)号：US09281555B2

公开(公告)日：2016-03-08

申请号：US14186737

申请日：2014-02-21

Applicant: AIRBUS OPERATIONS (S.A.S.) ,  ONERA (Office national d'études et de recherches aérospatiales)

Inventor： Hervé Jeuland

IPC: H01Q1/36 ,  H01Q1/42 ,  H01Q9/40

CPC classification number: H01Q1/36 ,  H01Q1/421 ,  H01Q9/40 ,  Y10T29/49016

Abstract: Method and monopole antenna for making uniform the radiation of the antenna, when disposed inside a radome. According to the invention, on the surface of the monopole antenna is formed a protruding longitudinal ridge which is disposed at least approximately opposite an area of the radiating pattern of the assembly radome (1)-monopole antenna having a reduced gain in comparison with the radiating pattern of said monopole antenna alone.

Abstract translation: 方法和单极天线，用于在天线罩内放置天线的辐射均匀时。 根据本发明，在单极天线的表面上形成有突出的纵向脊，该突起纵向脊与散热器（1） - 单极天线的辐射图案的至少大致相反地设置，其具有与辐射相比减小的增益 单极天线的图案。

公开(公告)号：US09262927B2

公开(公告)日：2016-02-16

申请号：US14488562

申请日：2014-09-17

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Frédérique Populus ,  Eric Petit

IPC: G08G5/00 ,  G10L15/26 ,  G06F17/27

CPC classification number: G08G5/0004 ,  G06F17/277 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0095 ,  G10L15/26

Abstract: Methods and devices for automatically managing audio air control messages on an aircraft are described. The device comprises a unit for automatically transcribing an audio message received on board an aircraft into a textual message, a unit for automatically processing the textual message in order to extract all the indications included in this message, and a unit for automatically displaying, for each extracted indication, on at least one screen of the aircraft cockpit, an information message relating to the indication and a validation request for the pilot.

Abstract translation: 描述了用于在飞机上自动管理音频空中控制消息的方法和装置。 该装置包括用于将飞行器上接收的音频消息自动转录成文本消息的单元，用于自动处理文本消息以便提取包含在该消息中的所有指示的单元，以及用于自动显示该消息的单元 在飞行器驾驶舱的至少一个屏幕上提取与指示有关的信息消息和对飞行员的验证请求。

公开(公告)号：US20160023749A1

公开(公告)日：2016-01-28

申请号：US14807014

申请日：2015-07-23

Applicant: Airbus Operations S.A.S.

Inventor： Mathieu CARTON ,  Pierre DEBUSSCHERE ,  David CHABE

IPC: B64C13/00 ,  B64D39/00 ,  G05D1/08

CPC classification number: B64C13/00 ,  B64D39/00 ,  G05D1/0607 ,  G05D1/0808

Abstract: The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.

Abstract translation: 该系统包括至少一个提升发电机元件，该升降机发电机元件能够直接修改飞行器的升降机，以及用于在飞行器的飞行员致动之后定义偏转指令的装置，该飞行器的飞行器产生垂直载荷系数控制值， 将其施加到电梯并同时定义命令指令并将其施加到电梯发电机元件以产生直接电梯。

公开(公告)号：US20150371544A1

公开(公告)日：2015-12-24

申请号：US14743823

申请日：2015-06-18

Applicant: AIRBUS OPERATIONS (S.A.S.)

Inventor： Jean-Claude MERE

IPC: G08G5/00

CPC classification number: G08G5/0039 ,  G01C21/20 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0091

Abstract: A method and device for determining and presenting cost impacts generated by lateral route deviations of an aircraft. The device includes a computation unit for determining different flight trajectories, called alternative trajectories, each of which is offset laterally in the horizontal plane relative to a reference trajectory, notably the current trajectory of the aircraft, and a computation unit configured to compute, for each of the alternative trajectories, an associated overall cost which provides an indication of the cost generated by a flight of the aircraft along this alternative trajectory, the device also includes a display unit configured to present, on a navigation screen, indication elements which provide indications concerning the position and the associated overall cost for at least some of the alternative trajectories.

Abstract translation: 一种用于确定和呈现由飞行器的侧向路线偏差产生的成本影响的方法和装置。 该装置包括用于确定不同飞行轨迹的计算单元，称为替代轨迹，每个轨迹相对于参考轨迹横向偏移在水平平面内，特别是飞行器的当前轨迹，以及计算单元， 替代轨迹的相关总体成本，其提供由沿着该替代轨迹的飞行器飞行产生的成本的指示，该设备还包括显示单元，其被配置为在导航屏幕上呈现指示元件，其提供关于 至少一些替代轨迹的位置和相关的整体成本。

公开(公告)号：US20150284100A1

公开(公告)日：2015-10-08

申请号：US14680701

申请日：2015-04-07

Applicant: Airbus Operations (S.A.S.)

Inventor： Florent BONNEAU ,  Julien LEZERAC

IPC: B64D29/06

CPC classification number: B64D29/06

Abstract: An aircraft nacelle comprising a spacing system to maintain two cowls spaced apart. A nacelle comprises two cowls each having a lower edge and an indexer in the region of the lower edge, the two cowls being mounted to be movable in terms of rotation about an opening axis between a closed position and an open position, a spacing system comprising a base fixed to a fixed portion of the nacelle. For each cowl, a lever which is independent of the lever associated with the other cowl and which has a housing in which the indexer is received in a closed position, and a stop against which the indexer is positioned in an open position, the lever being movable in terms of rotation on the base between an engagement position and a disengagement position, and for each lever, a return intended to urge the lever into the engagement position.

Abstract translation: 包括间隔系统的飞机机舱，以保持间隔开的两个整流罩。 机舱包括两个整流罩，每个整流罩在下边缘的区域中具有下边缘和分度器，两个整流罩安装成可以围绕关闭位置和打开位置之间的开口轴线旋转移动;间隔系统，包括 固定在机舱的固定部分上的基座。 对于每个整流罩，杠杆独立于与另一整流罩相关联的杠杆，并且具有壳体，分度器容纳在关闭位置，并且分度器位于打开位置，所述杠杆为 在接合位置和分离位置之间在基座上的旋转方面可移动，并且对于每个杠杆，旨在将杆推动到接合位置的返回件。

公开(公告)号：US09142135B2

公开(公告)日：2015-09-22

申请号：US14279418

申请日：2014-05-16

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Virginie Le Gall ,  Alexandre Buisson ,  Pierre-Xavier Catinat ,  Valentin Vincent

IPC: G08G5/02 ,  B64C19/00 ,  G05D1/06

CPC classification number: G08G5/02 ,  B64C19/00 ,  G05D1/0676

Abstract: A method and device for automatically determining an optimized approach and/or descent profile for an aircraft are provided. The device comprises means for optimizing an approach and/or descent profile of an aircraft avoiding long and steep geometric segments, the device to this end inserting an idle segment, if it satisfies the restrictions, in the profile relating to the descent phase and/or to the approach phase, wherein said idle segment can be followed by a geometric segment.

Abstract translation: 提供一种用于自动确定飞行器的优化进近和/或下降轮廓的方法和装置。 该装置包括用于优化飞行器的接近和/或下降轮廓以避免长而陡峭的几何段的装置，该装置为此在与下降相和/或下降相关的轮廓中满足限制时插入空闲段 到接近阶段，其中所述空闲段可以跟随几何段。