公开(公告)号：US09114880B2

公开(公告)日：2015-08-25

申请号：US14090882

申请日：2013-11-26

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

Inventor： Bernard Guering

IPC: B60N2/24 ,  B64D11/06 ,  A47C7/40 ,  B60N2/64 ,  B60N2/68 ,  A47C7/44

CPC classification number: B64D11/06 ,  A47C7/405 ,  A47C7/445 ,  B60N2/643 ,  B60N2/68 ,  B64D11/0649

Abstract: The invention relates to a seat back for an aircraft comprising a structural column bearing a plurality of devices for supporting an occupant of the seat, these devices being distributed along the structural column and oriented transversely relatively to the structural column so as to each protrude on either side of this column. This solution can reduce the mass and dimensions, while providing satisfactory comfort for the occupant.

Abstract translation: 本发明涉及一种用于飞行器的座椅靠背，其包括具有多个用于支撑座椅乘员的装置的结构柱，这些装置沿结构柱分布并相对于结构柱横向定向， 这一列的一边。 该解决方案可以降低质量和尺寸，同时为乘客提供令人满意的舒适感。

公开(公告)号：US20150217857A1

公开(公告)日：2015-08-06

申请号：US14171425

申请日：2014-02-03

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

Inventor： Mael MESGUEN ,  François BURON ,  Thibaut POUX

IPC: B64C19/00

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：US20150203214A1

公开(公告)日：2015-07-23

申请号：US14586433

申请日：2014-12-30

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

Inventor： Thierry Bourret ,  Kenji AHUALLE HORIMOTO

IPC: B64D45/04 ,  B64C13/18 ,  G01C23/00 ,  G05D1/04

CPC classification number: B64D45/04 ,  B64C13/18 ,  G01C23/005 ,  G05D1/042 ,  G05D1/0676

Abstract: A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the aircraft with respect to the terrain, using at least one measurement taken by a radar altimeter, a unit for computing a first current altitude of the aircraft, using the terrain height and the current height, a unit for computing a second current altitude of the aircraft, corresponding to an altitude on an approach profile of the current position of the aircraft and a unit for computing the difference between the first and second current altitudes, the difference being transmitted to a guidance unit to vertically guide the aircraft.

Abstract translation: 一种包括提取存储在存储器中的线性地形剖面的单元的方法和装置，飞行器当前距离的地形高度，用于使用至少一次测量来确定飞机相对于地形的当前高度的单元 通过雷达高度计，用于使用地形高度和当前高度来计算飞行器的第一当前高度的单元，用于计算飞行器的第二当前高度的单元，其对应于当前位置的接近轮廓上的高度 并且用于计算第一和第二当前高度之间的差异的单元，差异被传送到引导单元以垂直地引导飞行器。

公开(公告)号：US20150196986A1

公开(公告)日：2015-07-16

申请号：US14595702

申请日：2015-01-13

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

Inventor： Nicolas Cabanac ,  Jean-Pascal Cabot ,  Alexandre Lestruhaut

IPC: B23Q15/013 ,  B23B49/02 ,  B23Q5/32 ,  B23B45/00

CPC classification number: B23B49/02 ,  B23B45/00 ,  B23B49/008 ,  B23B2215/04 ,  B23B2260/07 ,  B23B2260/128 ,  B23B2260/138 ,  B23Q5/326 ,  B23Q17/00 ,  B25F5/003 ,  B25H1/0035 ,  B25H1/0078 ,  Y10T408/17 ,  Y10T408/172 ,  Y10T408/21 ,  Y10T408/5647

Abstract: A manual drilling apparatus equipped with a device for control of advance, which includes a fixed part and a mobile part with movement of translation relative to the fixed part during the drilling, as well as a system for control of the movement of translation of the mobile part relative to the fixed part, wherein the fixed part and the mobile part comprise respectively at least one fixed tube and at least one mobile tube which slide relative to one another, the fixed and mobile tubes being coaxial to the axis of rotation of the tool supported by the apparatus.

Abstract translation: 一种装备有用于控制前进的装置的手动钻孔装置，其包括固定部件和在钻孔期间相对于固定部件的平移移动的可移动部件，以及用于控制移动装置的平移运动的系统 部分相对于固定部分，其中固定部分和可移动部分分别包括至少一个固定管和至少一个相对于彼此滑动的可移动管，固定管和可移动管与工具的旋转轴线同轴 由设备支持。

公开(公告)号：US09077164B2

公开(公告)日：2015-07-07

申请号：US14084950

申请日：2013-11-20

Applicant: Airbus Operations S.A.S.

Inventor： Christophe Casse ,  Steve Fernandez ,  Marie Bayle

IPC: H02G3/02 ,  B60R16/02 ,  H05K7/14

CPC classification number: H02G3/02 ,  B60R16/0207 ,  H05K7/1412

Abstract: A cutting plate includes a planar interface able to accept electrical connectors, two ramps for supporting harnesses and two lateral walls, the dimensions of the interface and of the two ramps in a longitudinal direction being adapted to suit the number of connectors of the cutting plate and the dimensions in the directions other than the longitudinal direction and the dimensions of the lateral walls conforming to standard dimensions.

Abstract translation: 切割板包括能够接纳电连接器的平面接口，用于支撑线束和两个侧壁的两个斜面，沿纵向方向的接口和两个斜面的尺寸适合于适合切割板的连接器的数量和 在纵向方向以外的方向上的尺寸和符合标准尺寸的侧壁的尺寸。

公开(公告)号：US20150160094A1

公开(公告)日：2015-06-11

申请号：US14560687

申请日：2014-12-04

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

Inventor： Stéphane Mateo

IPC: G01M15/02 ,  G01M15/14

CPC classification number: G01M15/02 ,  F16L55/168 ,  G01M15/14 ,  Y10T137/598

Abstract: A tool for sealing at least one opening of a fluid circuit element, the tool including a support, at least one sealing device for an opening connected to the support and positioning structure for positioning and immobilizing the support with respect to the fluid circuit element, the frame comprising a U-shaped stirrup with a base and two arms, a rod and two connections connecting the rod to each arm, each arm including a centering wedge attached to the internal face of the arm which presents a bearing surface, the bearing surfaces being spaced apart by a distance making it possible to immobilize the fluid circuit element in a first direction in a transverse plane.

Abstract translation: 一种用于密封流体回路元件的至少一个开口的工具，该工具包括支撑件，至少一个用于开口的密封装置，该密封装置连接到用于相对于流体回路元件定位和固定支撑件的支撑和定位结构， 框架包括具有基部和两个臂的U形箍筋，杆和将杆连接到每个臂的两个连接件，每个臂包括附接到臂的内表面的定心楔，其呈现轴承表面，所述支承表面为 隔开一段距离，使得可以使流体回路元件沿横向平面中的第一方向固定。

公开(公告)号：US20150147136A1

公开(公告)日：2015-05-28

申请号：US14547802

申请日：2014-11-19

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Jean-Philippe MAUREL ,  Frederic LABAL ,  Jean-Luc MARTRES

IPC: F16B33/00 ,  F16B35/00

CPC classification number: F16B33/008 ,  F16B33/06 ,  F16B35/00

Abstract: A fixing element for components of an assembly, comprising a rod which is formed by a cylindrical shaft and an end, the rod being a metal component which is at least partially surface-treated by means of anode oxidation and coated over at least a portion of the cylindrical shaft with a lubricating coating. Such a fixing element enables the electrical continuity to be ensured with the components during mounting with moderate interference in the assembly.

Abstract translation: 一种用于组件的部件的固定元件，包括由圆柱形轴和端部形成的杆，所述杆是金属部件，所述金属部件通过阳极氧化被至少部分地表面处理并涂覆在至少一部分 圆柱轴具有润滑涂层。 这样的固定元件能够在组装中以适度干涉的安装期间确保组件的电连续性。

公开(公告)号：US20150132010A1

公开(公告)日：2015-05-14

申请号：US14535833

申请日：2014-11-07

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

Inventor： Nicholas Brownjohn ,  Stefan Osternack ,  Stéphane Poulain ,  Xavier Valancogne ,  Nils Fischer

IPC: H04B10/27 ,  H04L29/08

CPC classification number: H04B10/27 ,  H04L12/40176 ,  H04L45/28 ,  H04L67/12 ,  H04L2012/4028

Abstract: A data network, especially a data network for an aircraft or spacecraft, includes a primary data grid, and at least one secondary data grid, the primary data grid including primary data nodes, wherein the primary data nodes are directly or indirectly coupled in data communication with each other, and the at least one secondary data grid comprising secondary data nodes, wherein the at least one secondary data grid is configured to connect the secondary data nodes in a data communication chain and to connect the first secondary data node of the data communication chain to a first respective primary data node and/or the last secondary data node of the data communication chain to a second respective primary data node.

Abstract translation: 数据网络，特别是用于飞行器或航天器的数据网络包括主数据网格和至少一个辅助数据网格，主数据网格包括主数据节点，其中主数据节点直接或间接耦合在数据通信中 并且所述至少一个辅助数据网格包括辅助数据节点，其中所述至少一个辅助数据网格被配置为连接数据通信链中的次要数据节点并连接数据通信的第一辅助数据节点 链路连接到数据通信链路的第一相应主数据节点和/或最后次数据节点到第二相应的主数据节点。

公开(公告)号：US20150090047A1

公开(公告)日：2015-04-02

申请号：US14494670

申请日：2014-09-24

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Denis De Mattia

IPC: G01N3/18

CPC classification number: G01N3/18 ,  B29C70/20 ,  B29C70/54 ,  G01B21/32 ,  G01N2203/0017

Abstract: A method for testing a batch of material used to obtain layers of fibres includes taking a specimen from the batch of material, exerting a tensile force on the specimen, heating the specimen so as to relax the fibres if the specimen contains stresses, after a predetermined period of time, no longer heating and no longer exerting the tensile force on the specimen, measuring a residual extension of the specimen which corresponds to a variation in length of at least a part of the specimen in the direction of the tensile force, before and after the tensile force, and considering the batch of material not to be compliant if the residual extension exceeds a given threshold.

Abstract translation: 用于测试用于获得纤维层的一批材料的方法包括从批料中取出样品，对试样施加张力，加热试样以便在试样含有应力后放松纤维，在预定的 一段时间，不再加热并且不再对试样施加拉力，测量样品的剩余延伸率，其对应于试样在至少一部分拉伸方向上长度的变化， 在拉伸力之后，并且如果残余延伸超过给定阈值，则考虑该批材料不符合。

公开(公告)号：US20150039551A1

公开(公告)日：2015-02-05

申请号：US14341272

申请日：2014-07-25

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

Inventor： Jean-Max HUET ,  Stéphane BESSEAU ,  Bruno MAILLARD ,  François MICHAUD

IPC: G06N7/00

CPC classification number: G06N7/00 ,  G05B23/0283 ,  G05B2219/45071

Abstract: According to a first aspect, the subject matter disclosed herein relates to a decision aid method for maintenance operations of aircraft equipment, the aircraft including a maintenance system arranged to make a record of equipment failure messages and of equipment failure warning messages emitted during a flight, the method comprising extracting at least one combination of failure messages corresponding to failure messages recorded by the maintenance system during a flight and a set of previous flights; determining, as a function of the at least one extracted combination, a probability of occurrence of at least one warning message possibly accompanied by one or more failure messages.

Abstract translation: 根据第一方面，本文公开的主题涉及用于飞机设备的维护操作的决策辅助方法，所述飞行器包括维护系统，所述维护系统被布置成在飞行期间发出设备故障消息和设备故障警告消息的记录， 所述方法包括：提取在飞行期间和一组先前飞行中对应于维护系统记录的故障消息的故障消息的至少一个组合; 根据所述至少一个提取的组合确定可能伴随有一个或多个故障消息的至少一个警告消息的发生概率。