公开(公告)号：US20140165285A1

公开(公告)日：2014-06-19

申请号：US14132982

申请日：2013-12-18

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64D11/02

CPC classification number: B64D11/02 ,  B64D25/08

Abstract: A toilet area for an aircraft cabin comprising an access door and housing a toilet bowl. The toilet area also comprises an evacuation exit, the access door occupying a closed position in the toilet area in a toilet configuration and a folded position in the toilet area in an evacuation configuration. Usage in particular in a flying wing aircraft is provided.

Abstract translation: 一种用于飞机机舱的卫生间区域，其包括通道门和容纳马桶。 厕所区域还包括撤离出口，进入门在马桶构造中占据马桶区域中的关闭位置，并且在抽空构造中在厕所区域中的折叠位置。 特别提供飞翼飞机的使用。

公开(公告)号：US20140159444A1

公开(公告)日：2014-06-12

申请号：US14100771

申请日：2013-12-09

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B64D11/06 ,  A47C7/46 ,  A47C1/121

CPC classification number: B64D11/06 ,  A47C9/025 ,  A47C11/005 ,  B60N2/10 ,  B60N2/14 ,  B60N2/163 ,  B60N2/3011 ,  B60N2/3031 ,  B60N2/305 ,  B60N2/77 ,  B60N2/773 ,  B60N2002/247 ,  B64D11/0611 ,  B64D11/0639

Abstract: A seating device with reduced bulk, for example for an aircraft. This seating device comprises a backrest which describes a circular translational movement towards the front and upwards of the device when the seating device is brought to the retracted configuration. A seating structure is provided comprising a bearing piece on which are fixed, side by side, a plurality of seating devices with reduced bulk. An aircraft is provided comprising a seating device with reduced bulk mounted in its cabin.

Abstract translation: 减少散装的座椅装置，例如飞机。 该座椅装置包括靠背，其当座椅装置处于缩回构型时描述朝向装置的前部和上方的圆形平移运动。 提供了一种座椅结构，包括一个轴承件，其上并排地固定有多个具有减小体积的座椅装置。 提供了一种飞机，其包括具有减小的散装安装在其舱室中的座位装置。

公开(公告)号：US20140145128A1

公开(公告)日：2014-05-29

申请号：US14087064

申请日：2013-11-22

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: H02G1/06

CPC classification number: 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.

Abstract translation: 一种在飞行器中安装线束的方法。 该方法包括使用具有固定到线束的第一端和缠绕装置的电缆，其中每个绕线装置缠绕所述电缆之一，以便通过施加张力来提升所述线束。 电缆的第一端沿着线束的至少一部分分布，以便在该部分上分布张力。

公开(公告)号：US20130259612A1

公开(公告)日：2013-10-03

申请号：US13772726

申请日：2013-02-21

Applicant: AIRBUS OPERATIONS (SAS)

Inventor： Bernard Guering

IPC: B65G1/06 ,  B64D11/00

CPC classification number: B65G1/06 ,  B64D9/00 ,  B64D11/0007 ,  B64D11/04

Abstract: The present invention relates to an automated storage cabinet for trolleys. It includes a device for automatically handling a single trolley with a handling basket including a vertical plate perpendicular to the waiting area, vertically movable between the floor of the waiting area and any one of the levels of the trolley storage cabinet, and two side flanks, connected to the vertical plate and provided with structure for supporting, on either side, two opposite sides of a trolley in the waiting area and for transferring the supported trolley through an opening of the predetermined compartment. The handling device can include structure for inserting the trolley into or extracting the trolley from the predetermined compartment.

Abstract translation: 本发明涉及一种用于手推车的自动化存储柜。 它包括用于自动处理单个手推车的装置，其具有处理筐，该操纵筐包括垂直于等待区域的垂直板，可垂直地在等待区域的地板和台车存储柜的任一层之间移动，以及两个侧翼， 连接到垂直板并且设置有用于在任一侧上在等待区域中的台车的两个相对侧支撑并且用于将支撑的小车通过预定隔间的开口传送的结构。 处理装置可以包括用于将小车插入或从预定隔间提取手推车的结构。

公开(公告)号：US11319696B2

公开(公告)日：2022-05-03

申请号：US16725324

申请日：2019-12-23

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Romain Delahaye

IPC: E03C1/01 ,  B64D11/02

Abstract: To reduce the bulk of an aircraft toilet which includes a toilet bowl and a washbasin, the washbasin is movably mounted in the toilet to be able to adopt at least two distinct positions relative to the toilet bowl, including a retracted position adopted to bring the toilet into a configuration of use of the bowl, and a deployed position adopted to bring the toilet into a washbasin configuration, a position in which the washbasin is arranged above the bowl.

公开(公告)号：US11084588B2

公开(公告)日：2021-08-10

申请号：US16224071

申请日：2018-12-18

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Laurent Saint-Marc

IPC: B64D11/06 ,  B64D25/08 ,  B64D25/04 ,  B60N2/00

Abstract: A pilot's seat offering an evacuation device. The seat comprises a ladder fixed to the rear of the back and covered by a detachable cover associated with the seat and deployable between a storage position retracted inside the cover and a deployed evacuation position, in which case the cover is detached. Thus, the evacuation device is incorporated harmoniously into the seat which offers a solid base for the evacuation ladder.

公开(公告)号：US10124879B2

公开(公告)日：2018-11-13

申请号：US15133745

申请日：2016-04-20

Applicant: Airbus Operations (SAS)

Inventor： Frederic Vinches ,  Bernard Guering

IPC: B64C1/20 ,  B64D11/00 ,  B64C1/10 ,  B64D9/00

Abstract: A cabin space dedicated to passengers and, beneath said cabin space, an under-cabin space which extends along the longitudinal axis of said aircraft. The under-cabin space comprises, distributed along two lines parallel to the longitudinal axis of the aircraft, two sets of systems which are able to carry out functions necessary for the operation of the aircraft. The two lines of sets of systems are disposed respectively in two lateral zones of the under-cabin space which are spaced apart transversely from one another and enclose a free central zone which extends along the longitudinal axis of the aircraft. This arrangement thus eliminates any technical zone from the under-cabin space, thereby facilitating the internal layout and maintenance.

公开(公告)号：US20180194452A1

公开(公告)日：2018-07-12

申请号：US15847078

申请日：2017-12-19

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Matthieu DE KERGOMMEAUX

IPC: B64C1/40 ,  B64C1/06

CPC classification number: B64C1/406 ,  B64C1/066 ,  B64C1/068 ,  B64C1/40 ,  B64D2011/0046 ,  B64F5/10 ,  Y02T50/46

Abstract: In order to facilitate the thermoacoustic insulation of an aircraft portion, a method for manufacturing a thermoacoustic insulation module for an aircraft comprises a step of providing a mat configured to provide thermoacoustic insulation of an aircraft portion, followed by a step of attaching a bendable structure to the mat, followed by a step of bending the bendable structure, along a bending axis parallel to a longitudinal direction of the mat, such that the bendable structure forms a load-bearing structure supporting the mat in a curved shape.

公开(公告)号：US09499259B2

公开(公告)日：2016-11-22

申请号：US14577041

申请日：2014-12-19

Applicant: AIRBUS OPERATIONS (SAS)

Inventor： Bernard Guering

IPC: B64C25/20 ,  B64C25/14 ,  B64C25/26

CPC classification number: B64C25/20 ,  B64C25/14 ,  B64C25/26

Abstract: A landing gear has a rigid structure and a gear compartment. A leg has a wheeled first end on a rolling shaft, and a second end secured on the rigid structure. The leg rotates between a rolling position, letting the aircraft rolls, and a landing gear storage position. A brace has a first end secured on the rigid structure. A guide bar has a first end pivotably secured on the leg, and a second end secured on the second end of the brace by a pivot shaft. A jack is secured between the brace by a pivot connection with a shaft parallel to the rolling shaft, and the guide bar, by a pivot connection with a shaft parallel to the rolling shaft. A locking system locks either a second end of the brace or the second end of the guide bar against the leg in the rolling position.

Abstract translation: 起落架具有刚性结构和齿轮室。 腿在滚动轴上具有轮状的第一端，并且固定在刚性结构上的第二端。 腿部在滚动位置之间旋转，使飞行器滚动，并起落架存放位置。 支架具有固定在刚性结构上的第一端。 引导杆具有可枢转地固定在腿上的第一端，以及通过枢轴固定在支架的第二端上的第二端。 通过与平行于滚动轴的轴的枢轴连接和引导杆通过与平行于滚动轴的轴的枢转连接将千斤顶固定在支架之间。 锁定系统锁定支架的第二端或引导杆的第二端在滚动位置处抵靠腿部。

公开(公告)号：US20160304186A1

公开(公告)日：2016-10-20

申请号：US15133758

申请日：2016-04-20

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering ,  Laurent Saint-Marc

IPC: B64C1/20 ,  B64D27/02 ,  B64C5/02 ,  B64C25/04 ,  B64D11/06 ,  B64D11/04

CPC classification number: B64C1/20 ,  B64C1/18 ,  B64C5/02 ,  B64C25/04 ,  B64D11/04 ,  B64D11/0696 ,  B64D27/02

Abstract: An aircraft comprising a fuselage which has a central part with a cross section of constant geometry which comprises a floor. The floor comprises two lateral portions which are fixed respectively to two opposite lateral edges of the fuselage and which enclose a central portion to which they are fixed. One of the lateral floor portions is fixed to the central portion so as to allow a relative lateral movement between the two portions in the event of a modification in pressure inside the fuselage. The cross section thus deforms homogeneously when the fuselage is pressurized and the floor is not involved in maintaining the shape of the fuselage.

Abstract translation: 一种包括机身的飞机，该机身具有包括地板的具有恒定几何形状的横截面的中心部分。 该地板包括分别固定在机身的两个相对的侧边缘上的两个侧面部分，它们围绕着固定在其上的中心部分。 在侧面底板部分中的一个固定到中心部分，以便在机身内的压力改变的情况下允许两个部分之间的相对横向移动。 当机身加压时，横截面因而变形均匀，而且地板不参与保持机身的形状。