公开(公告)号：US09457893B2

公开(公告)日：2016-10-04

申请号：US14171425

申请日：2014-02-03

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

Inventor： Mael Mesguen ,  François Buron ,  Thibaut Poux

IPC: B64C19/02 ,  B64C19/00 ,  B64D43/00 ,  B64D45/00

CPC classification number: B64C19/02 ,  B60L2250/16 ,  B64C19/00 ,  B64D43/00 ,  B64D2045/0085 ,  B64D2221/00

Abstract: Methods, systems, and computer readable media are disclosed for managing an aircraft's systems through a dedicated interface. One aspect of a method for implementing the subject matter described herein includes at least one interactive interface configured for managing an aircraft system, displaying at least one or more graphic object representing at least one or more system component, displaying at least one or more energy flow icon representing the direction of circulation of an energy flow, and interacting with the at least one or more system component through a user action on the at least one or more graphic object.

Abstract translation: 公开了用于通过专用接口管理飞行器系统的方法，系统和计算机可读介质。 用于实现本文描述的主题的方法的一个方面包括配置用于管理飞行器系统的至少一个交互式界面，显示表示至少一个或多个系统组件的至少一个或多个图形对象，显示至少一个或多个能量流 图标表示能量流的循环方向，并且通过在至少一个或多个图形对象上的用户动作与至少一个或多个系统组件相互作用。

公开(公告)号：US09454908B2

公开(公告)日：2016-09-27

申请号：US14049291

申请日：2013-10-09

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Marie-Claire Moune ,  Jean Muller ,  Stéphane Cote

IPC: G08G5/02 ,  G05D1/00

CPC classification number: G08G5/02 ,  G05D1/0072

Abstract: A method and system for managing automatic guidance of an aircraft during a complete engine failure. Said system includes means for monitoring engines so as to be able to detect a complete failure of the engines; means for detecting whether the aircraft is in flight; means for detecting whether the aircraft is in a different guidance mode from a guidance mode configured to make the aircraft descend with a reduced engine thrust and a fixed speed; and control means for automatically bringing guidance means of the aircraft into a guidance configuration compatible with the situation associated with the complete failure of the engines.

Abstract translation: 一种用于在整个发动机故障期间管理飞行器的自动引导的方法和系统。 所述系统包括用于监测发动机以便能够检测发动机的完全故障的装置; 检测飞机是否飞行的手段; 用于检测飞行器是否处于与引导模式不同的引导模式的装置，所述引导模式被配置为使飞行器以降低的发动机推力和固定速度下降; 以及用于将飞行器的引导装置自动引导到与发动机完全失效相关的情况相一致的引导配置的控制装置。

公开(公告)号：US09453770B2

公开(公告)日：2016-09-27

申请号：US14080858

申请日：2013-11-15

Applicant: Airbus Operations S.A.S.

Inventor： Marc Sartor ,  Patricia Morgue ,  Manuel Paredes

IPC: G01L1/24 ,  G01M11/08 ,  G01D5/353 ,  G01B11/16 ,  G01M5/00

CPC classification number: G01B11/165 ,  G01B11/18 ,  G01D5/35316 ,  G01L1/246 ,  G01M5/0025 ,  G01M5/0041 ,  G01M5/0091 ,  G01M11/086

Abstract: A strain measurement device is provided. The strain measurement device includes at least one filiform strain sensor and a support of longilinear shape on which the filiform strain sensor is positioned. The strain measurement device also includes a stiffener.

Abstract translation: 提供了应变测量装置。 应变测量装置包括至少一个丝状应变传感器和丝状应变传感器所在的长线形支撑。 应变测量装置还包括加强件。

公开(公告)号：US09452818B2

公开(公告)日：2016-09-27

申请号：US14100853

申请日：2013-12-09

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Francois Loyant ,  Alexandre Legardez

IPC: B64C1/26

CPC classification number: B64C1/26

Abstract: An aircraft comprising a wing box and a fuselage provided with a connecting device configured to be connected to the wing box and to transmit thereto stresses undergone by the fuselage during maneuvers of the aircraft are provided. The connecting device is formed by a keel beam and a keel beam panel connected to the beam via a connecting portion of the beam, that is moreover provided with a main portion extending in a first, generally longitudinal direction and a transfer portion extending in a second direction different from the first direction and configured to be connected to the box. The main, transfer and connecting portions are configured to direct a major part of the stresses received by the beam in the second direction and transmit said major part of the stresses to the box by compression.

Abstract translation: 提供了一种飞机，其包括翼盒和机身，其设置有连接装置，该连接装置被配置为连接到翼盒并且向其传送机身在飞机操作期间经受的应力。 连接装置由龙骨梁和龙骨梁板形成，该龙骨梁和梁梁通过梁的连接部分连接到梁上，其还设置有沿第一大致纵向方向延伸的主要部分和在第二纵向方向上延伸的转移部分 方向与第一方向不同，并且被配置为连接到盒子。 主要的，转移和连接部分构造成引导梁在第二方向上接收的应力的主要部分，并通过压缩将所述大部分应力传递到箱体。

公开(公告)号：US09446459B2

公开(公告)日：2016-09-20

申请号：US14691661

申请日：2015-04-21

Applicant: Airbus Operations S.A.S.

Inventor： Denis De Mattia

IPC: B23C3/30 ,  B23Q1/42 ,  B23C5/16

CPC classification number: B23C3/30 ,  B23C5/16 ,  B23C2215/04 ,  B23C2220/36 ,  B23C2220/40 ,  B23C2228/25 ,  B23C2260/04 ,  B23Q1/42 ,  Y10T409/306496 ,  Y10T409/30784 ,  Y10T409/308624

Abstract: A device for machining a slot on a surface of a cellular structure includes a machining head that includes a chassis, a rotary tool rotating about a tool axis perpendicular to the direction of the slot, two guide wheels arranged on either side of the rotary tool that have a plurality of teeth configured and positioned such that they penetrate the cells of an alignment of the cellular structure. The machining head includes a link between the chassis and at least one guide wheel that enables a degree of freedom in a lateral direction parallel to the tool axis such that the guide wheel is movable in relation to the rotary tool in the lateral direction.

Abstract translation: 用于在蜂窝状结构的表面上加工槽的装置包括：加工头，其包括底盘，围绕垂直于所述槽的方向的工具轴线旋转的旋转工具，布置在所述旋转工具的任一侧上的两个导轮， 具有配置和定位的多个齿，使得它们穿过细胞结构的对准的细胞。 加工头包括在底盘和至少一个导轮之间的连杆，其能够平行于工具轴线的横向方向上的自由度，使得导轮相对于旋转工具在横向方向上可移动。

公开(公告)号：US20160187247A1

公开(公告)日：2016-06-30

申请号：US14977963

申请日：2015-12-22

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

Inventor： Stéphane REY ,  Florent AUDOIN ,  Pierre HEBERLE ,  Isabelle MULTAN

IPC: G01N17/00 ,  G01N25/00

CPC classification number: G01N17/002 ,  G01M5/0091 ,  G01M99/002 ,  G01N25/00 ,  G01N25/72

Abstract: A device for conducting accelerated aging tests of a coating, notably an outer coating for an aircraft, in particular allowing the testing of the durability of the coating after having been subject to all kinds of stresses, is desired. An object of the disclosure thus relates to such a device including test chambers subject to different and/or independently controllable test parameters, and including light for generating photo-oxidation, the device including a support for a sample of the coating, displaceable between the chambers for generating mechanical stresses by thermal shocks. The disclosure herein finds applications in many fields of industry, and preferentially in the field of aeronautics.

Abstract translation: 期望用于进行涂层的加速老化试验的装置，特别是用于飞机的外涂层，特别是允许在经受各种应力之后测试涂层的耐久性的装置。 因此，本公开的目的涉及这样的装置，其包括经受不同和/或可独立控制的测试参数的测试室，并且包括用于产生光氧化的光，该装置包括用于涂层样品的载体，可在腔室 用于通过热冲击产生机械应力。 本文的公开内容涉及许多工业领域的应用，优选在航空领域。

公开(公告)号：US20160178352A1

公开(公告)日：2016-06-23

申请号：US14974912

申请日：2015-12-18

Applicant: AIRBUS OPERATIONS (S.A.S.) ,  AIRBUS DEFENCE AND SPACE GMBH

Inventor： MARC MARCEL WEBER ,  FRANÇOIS ANTOINE OLCHEWSKY ,  RICARDO MAIKO UEHOKA ENTZ

IPC: G01B11/06 ,  G06T11/60 ,  H04N5/235

CPC classification number: G01B11/0625 ,  B64D15/20 ,  G06T11/60 ,  H04N5/2355

Abstract: A system and method for providing an estimate of the thickness of the ice regardless of the shape of its surface at the level of the air/ice interface. To this end the system and method measure an intensity profile of a luminous pattern generated by diffusion in the ice, which enables the system to measure the thickness of the ice even when the air/ice surface is not plane.

Abstract translation: 一种用于提供冰的厚度的估计的系统和方法，而不管其表面的形状在空气/冰界面的水平。 为此，系统和方法测量由冰中扩散产生的发光图案的强度分布，这使得系统即使当空/冰表面不是平面时也能够测量冰的厚度。

公开(公告)号：US20160171700A1

公开(公告)日：2016-06-16

申请号：US14965124

申请日：2015-12-10

Applicant: Airbus Operations S.A.S.

Inventor： Stephane GAUTHIER

IPC: G06T7/00 ,  G06T7/20 ,  G06T7/60 ,  G06K9/62 ,  H04N7/18 ,  G06K9/52

CPC classification number: G06K9/52 ,  G06K9/6201 ,  G06T7/246 ,  G06T7/33 ,  G06T7/60 ,  G06T7/73 ,  G06T7/80 ,  G06T2207/10016 ,  G06T2207/20228 ,  G06T2207/30252 ,  H04N7/185

Abstract: A detection system comprises an analysis unit for analyzing successive images generated by a monitoring sensor to determine in an image a position of an axis representative of the displacement of the aircraft between two successive images, the so-called real position, a computation unit for computing, on the basis of data relating to a displacement of an aircraft between the generations of these two images and of the positioning of the monitoring sensor on the aircraft, a position in an image of an axis representative of the displacement of the aircraft, the theoretical position, an estimation unit for estimating the angular disparity between the real position and the theoretical position, and a comparison unit for comparing this angular disparity with at least one predefined tolerance value so as to detect a misalignment when this angular disparity is greater than this tolerance value.

Abstract translation: 检测系统包括分析单元，用于分析由监测传感器产生的连续图像，以在图像中确定代表飞机在两个连续图像之间的位移的轴的位置，即所谓的实际位置，用于计算的计算单元 基于与这两个图像的代数之间的飞行器的位移以及监视传感器在飞机上的位置的数据相关的数据，代表飞行器的位移的轴的图像中的位置，理论上 位置，用于估计实际位置和理论位置之间的角度差异的估计单元，以及比较单元，用于将该角度视差与至少一个预定义的公差值进行比较，以便当该角度视差大于该公差时检测未对准 值。

公开(公告)号：US09361804B2

公开(公告)日：2016-06-07

申请号：US14222195

申请日：2014-03-21

Applicant: AIRBUS OPERATIONS (S.A.S)

Inventor： Jean-Claude Mere ,  Matthieu Aribert ,  Mathieu Versini

IPC: G06G7/70 ,  G06F19/00 ,  G08G5/00 ,  G01C21/20

CPC classification number: G08G5/003 ,  G01C21/20 ,  G08G5/0039

Abstract: The device comprises a flight management system which comprises means for generating requests, for requesting the results of performance functions and a performance function server which is external with respect to the flight management system and comprises means for calculating predictions which are capable of processing the requests and transmitting the results to the flight management system.

Abstract translation: 该装置包括飞行管理系统，其包括用于生成请求的装置，用于请求性能功能的结果和对于飞行管理系统是外部的执行功能服务器，并且包括用于计算能够处理请求的预测的装置， 将结果传输到飞行管理系统。

公开(公告)号：US20160156878A1

公开(公告)日：2016-06-02

申请号：US14948064

申请日：2015-11-20

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

Inventor： Erwan LE-BOUEDEC

IPC: H04N7/18 ,  H04N5/232 ,  H04N5/76 ,  H04L29/06

CPC classification number: H04N7/181 ,  H04H20/62 ,  H04L67/42 ,  H04N5/23206 ,  H04N5/7605

Abstract: Systems and methods are disclosed allowing a passenger of a vehicle to use a personal electronic device to control a saving, on a storage device, of image data of video streams arising from cameras of the vehicle. The system includes at least one client/server module configured to receive and retransmit image data of a video stream received from one of the cameras to the storage device. The client/server module includes a processor configured to connect the personal electronic device to the client/server module, a receiver for receiving a request, originating from the personal electronic device, including an item representative of a set of images of the video stream to be saved and a transmitter for transmitting to the storage device image data of the video stream corresponding to the item, with a view to their saving.

Abstract translation: 公开了允许车辆乘客使用个人电子设备来控制在存储设备上保存由车辆的照相机产生的视频流的图像数据的系统和方法。 该系统包括至少一个客户端/服务器模块，被配置为接收并重传从一个摄像机接收的视频流的图像数据到存储设备。 客户机/服务器模块包括被配置为将个人电子设备连接到客户端/服务器模块的处理器，用于从个人电子设备接收来自个人电子设备的请求的接收器，包括表示视频流的一组图像的项目， 以及用于向存储装置发送对应于该项目的视频流的图像数据的发送器，以便保存。