公开(公告)号：US10186848B2

公开(公告)日：2019-01-22

申请号：US14087064

申请日：2013-11-22

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: H02G1/06 ,  H02G1/00

Abstract: A method for installing a wiring harness in an aircraft. The method comprises using cables having first ends secured to the harness and winding means onto each of which is wound one of said cables so as to lift up said harness by exerting a tensile force. The first ends of the cables are distributed along at least a section of the harness so as to distribute the tensile forces over the section.

公开(公告)号：US20180305028A1

公开(公告)日：2018-10-25

申请号：US15959899

申请日：2018-04-23

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Laurent SAINT-MARC

IPC: B64D13/06

CPC classification number: B64D13/06 ,  B64C7/00 ,  B64D2013/0618 ,  B64D2231/02 ,  B64F1/362

Abstract: An air intake system for an aircraft having a ventral fairing and comprising a scoop having a ventral wall with a first coupling and an opening. The scoop is movable between a flush position in which the ventral wall is flush with the ventral fairing and a catchment position in which the opening is beneath the ventral fairing, and the ventral wall is pierced by a through hole designed to be connected to a flexible pipe of an air conditioning unit. A hatch is movably mounted on the scoop between an open position not blocking the opening and a closed position blocking the opening, the open position can be attained only when the scoop is in the catchment position. A return element forces the hatch into the closed position, and a plug has a second coupling which cooperates with the first coupling to removably secure the plug.

公开(公告)号：US09359084B2

公开(公告)日：2016-06-07

申请号：US14138588

申请日：2013-12-23

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64C1/00 ,  B64D43/00 ,  B64C1/18 ,  B64F5/00

CPC classification number: B64D43/00 ,  B64C1/18 ,  B64C2001/009 ,  B64F5/10 ,  Y10T29/49826

Abstract: An integral avionics bay module. The module has a structure that has an integral cabin floor on top that closes the structure. Installing such an integral avionics bay structure in a single operation inside a primary fuselage structure considerably reduces the integration time on the final assembly line for the aircraft.

Abstract translation: 一个完整的航空电子海湾模块。 该模块具有在顶部具有整体的舱室结构的结构，其关闭结构。 在主机身结构内的单一操作中安装这样一个整体的航空电子设备舱结构大大减少了飞机最终装配线上的集成时间。

公开(公告)号：US09216809B2

公开(公告)日：2015-12-22

申请号：US13628153

申请日：2012-09-27

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Yves Durand

IPC: B64C1/00 ,  B64C1/18 ,  B64D13/00 ,  H05K7/20 ,  B64D13/06

CPC classification number: B64C1/18 ,  B64D13/00 ,  B64D2013/0614 ,  H05K7/20554

Abstract: A ventilation system for an avionics bay has two strut assemblies for stiffening the floor of the cockpit, each strut assembly being arranged symmetrically regarding to the central plane of the aircraft, and means of distribution of the blowing air in the cabinets of the bay from the strut assemblies. The extraction circuit includes exhaust ducts integrated in the cabinets and couples together by tight inter-cabinets junctions in an overall configuration of maximized compactness.

Abstract translation: 用于航空电子设备舱的通风系统具有两个用于加强驾驶舱地板的支柱组件，每个支柱组件关于飞行器的中心平面对称地布置，以及将吹风空气分配在舱的机柜中的装置， 支柱组件。 提取电路包括集成在机柜中的排气管道，并通过紧密的机柜间连接在一起，以最大的紧凑性的整体结构。

公开(公告)号：US09203168B2

公开(公告)日：2015-12-01

申请号：US14332636

申请日：2014-07-16

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: H01R9/26 ,  H01R9/24 ,  H01R9/22 ,  H01R11/09

CPC classification number: H01R9/223 ,  H01R9/2408 ,  H01R9/26 ,  H01R11/09 ,  H01R2201/26

Abstract: A power breaker strip comprising a strip support and a plurality of interphase spacer elements, and a plurality of interline spacer elements, assembled with the plurality of interphase spacer elements such that each interline spacer element extends at least partly between two consecutive interphase spacer elements. The interphase spacer elements and the interline spacer elements together delimit a plurality of per pitch zones of the strip in which connection terminals of several lines of electrical cables can be inserted.

Abstract translation: 一种电力断路器条，包括带状支撑件和多个相间隔元件，以及多个间隔元件，其与所述多个相间隔元件组装，使得每个线间间隔元件至少部分地延伸在两个连续的相间隔元件之间。 相间间隔元件和间隔元件一起限定了条带的多个每间距区域，其中可以插入多条电缆线的连接端子。

公开(公告)号：US08967538B2

公开(公告)日：2015-03-03

申请号：US13708167

申请日：2012-12-07

Applicant: Airbus Operations SAS

Inventor： Bernard Guering

IPC: B64D11/06 ,  B64D10/00 ,  A62B25/00

CPC classification number: B64D11/0689 ,  A62B25/005 ,  B64D10/00 ,  B64D11/062 ,  B64D2231/025

Abstract: A headrest includes a first part referred to as the lower part, equipped with a connecting unit enabling an adjustable connection of the headrest to the seat back of a pilot seat, and a second part referred to as the upper part, located opposite the lower part, as well as a front face intended to serve as a support surface for the head of a user. A receptacle, connected to the mask, stores an oxygen mask and/or a supply line. The upper part of the headrest forms a hinged cover on the lower part of the headrest and it closes the receptacle. A seat, a cockpit, and an aircraft include such headrest.

Abstract translation: 头枕包括称为下部的第一部件，其具有连接单元，该连接单元能够使头枕与驾驶员座椅的座椅靠背的可调连接，以及被称为上部的第二部分，位于下部 ，以及用作用户头部的支撑表面的前表面。 连接到面罩的容器存储氧气面罩和/或供应线。 头枕的上部在头枕的下部形成铰链盖，并且关闭容器。 座椅，驾驶舱和飞机包括这样的头枕。

公开(公告)号：US20140175964A1

公开(公告)日：2014-06-26

申请号：US14138543

申请日：2013-12-23

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: H05K5/02

CPC classification number: H05K5/0217 ,  B64D43/00 ,  H05K7/1412

Abstract: An electrical and electronics bay of an aircraft comprising two rows of elements, each row being separated by a single corridor and comprising at least one set of systems elements and at least one electrical power center, the systems elements being arranged in cabinets. At least one of the cabinets comprises mobile shelves for allowing access to the back of the cabinets by crossing it. This architecture makes it possible to increase the density of the elements present in the bay while observing the principles of redundancy and segregation.

Abstract translation: 包括两排元件的飞机的电气和电子舱，每排由单个走廊分开，并且包括至少一组系统元件和至少一个电力中心，所述系统元件布置在机柜中。 至少一个机柜包括用于允许通过穿过机柜的后部进入的移动货架。 这种结构使得可以增加海湾中存在的元素的密度，同时遵守冗余和分离的原理。

公开(公告)号：US20140175225A1

公开(公告)日：2014-06-26

申请号：US14138572

申请日：2013-12-23

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64D11/00 ,  B64D43/00 ,  B64C1/14 ,  B64C1/18

CPC classification number: B64D11/00 ,  B64C1/1407 ,  B64C1/1469 ,  B64C1/18 ,  B64C2001/009 ,  B64D43/00 ,  B64F5/10

Abstract: A cockpit for an aircraft nose, the cockpit having a floor that acts solely as a floor for the crew to walk on and that is lower than the height of the cabin floor situated behind the cockpit. The cockpit also has a stair connected to the floor in order to enter and leave the cockpit. This arrangement enlarges the volume of the cockpit and enables equipment to be housed therein that previously used to be housed in the zone that is difficult to access that is situated under the cockpit and that also contains the bay for storing landing gear.

Abstract translation: 驾驶舱为飞机鼻子，驾驶舱有一个地板，仅作为一个地板供船员行走，低于驾驶舱后面舱室的高度。 驾驶舱还有一个楼梯连接到地板上，以便进出驾驶舱。 这种安排扩大了驾驶舱的体积，使得以前用于容纳在驾驶舱下方难以进入的区域中的设备被容纳在其中，并且还包含用于存储起落架的托架。

公开(公告)号：US20130333857A1

公开(公告)日：2013-12-19

申请号：US13970867

申请日：2013-08-20

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Yves Durand

IPC: B64D13/08

CPC classification number: B64D13/08 ,  B64D13/00 ,  B64D2013/0614 ,  B64D2013/0674 ,  F28F2225/04 ,  Y02T50/56

Abstract: An aircraft includes at least one wall delimiting a first zone (I) of the aircraft which is thermally insulated from the outside of the aircraft and a second zone (E) contained within the aircraft which is not thermally insulated with respect to the outside of the aircraft and a heat exchanger inside which a heat transfer fluid circulates, wherein the wall includes at least one duct inside which the heat transfer fluid circulates so as to act as a heat exchanger.

Abstract translation: 飞机包括至少一个界定飞机第一区域（I）的墙壁，该第一区域（I）与飞行器的外部热绝缘;以及第二区域（E），该第二区域（E）相对于外部不相互隔热 飞机和热交换器，其中传热流体循环，其中所述壁包括至少一个管道，所述传热流体循环在所述至少一个管道中，以便用作热交换器。

公开(公告)号：US20130221156A1

公开(公告)日：2013-08-29

申请号：US13628145

申请日：2012-09-27

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B64C1/06

CPC classification number: B64C1/061 ,  B64C1/1476

Abstract: This aircraft nose structure comprises frames (2, 4, 6), a lower windshield frame member (12) and an upper windshield frame member (14) which are adapted to receive a windshield.The lower windshield frame member (12) has an arcuate shape with two branches which are connected together by a tie-rod (26).

Abstract translation: 该飞行器鼻部结构包括适于接收挡风玻璃的框架（2,4,6），下部挡风玻璃框架构件（12）和上部挡风玻璃框架构件（14）。 下挡风玻璃框架构件（12）具有弓形形状，其中两个分支通过连杆（26）连接在一起。