公开(公告)号：US10562604B2

公开(公告)日：2020-02-18

申请号：US15375478

申请日：2016-12-12

Applicant: Airbus Operations SAS

Inventor： Bernard Guering

IPC: B64C1/10 ,  B64C1/18 ,  B64C1/06 ,  B64C1/36

Abstract: A zone is provided between the forward pressure bulkhead in an aircraft and the floor. The nose section of the aircraft in which the flat surface pressure bulkhead including at least one transverse frame comprises at least two rods, of which one of the front ends is attached to the bulkhead and/or the frame and the other rear end is attached to a structural element, the two rods further apart from the front to the rear, thus providing a work space. Therefore, the rods provide a more comfortable work area while picking up part of the loads from the bulkhead to the floor.

公开(公告)号：US10399667B2

公开(公告)日：2019-09-03

申请号：US15370037

申请日：2016-12-06

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Laurent Saint-Marc

IPC: B64C13/04 ,  B64C13/12 ,  B64C13/06 ,  G05G1/36 ,  B64C13/08 ,  B64C25/44

Abstract: The rudder bar includes two actuation arrangements, each provided with two pedals, each actuation arrangement having a frame provided with two rails arranged on either side of said frame and being in the form of a concave curve, and, associated with each one of said rails, a movable carriage, each one of said movable carriages bearing one of said pedals, each one of said movable carriages being configured such that it can be moved on the associated rail, for a direction command, under an action exerted by at least one foot of a pilot on at least one of said pedals.

公开(公告)号：US10053234B2

公开(公告)日：2018-08-21

申请号：US14637770

申请日：2015-03-04

Applicant: Airbus Operations (SAS)

Inventor： Yves Durnad ,  Bernard Guering

IPC: B64F5/10 ,  B64C1/18 ,  B64F5/00 ,  B64C1/06

CPC classification number: B64F5/10 ,  B64C1/061 ,  B64C1/18 ,  Y10T29/49622

Abstract: A device for positioning a first piece relative to a second piece. The first piece comprises a free end with a first bore and the second piece comprises an engagement part with a second bore intended to come into correspondence with the first bore. The first and second bore are drilled to the definitive diameter thereof prior to the relative positioning thereof. The device comprises one or more positioning elements, which are able to position the first bore relative to the second bore along at least one of three geometric axes.

公开(公告)号：US20180178897A1

公开(公告)日：2018-06-28

申请号：US15847125

申请日：2017-12-19

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Matthieu DE KERGOMMEAUX

IPC: B64C1/40 ,  B64F5/10

CPC classification number: B64C1/40 ,  B64C1/403 ,  B64F5/10 ,  Y02T50/46

Abstract: In order to facilitate the thermoacoustic insulation of an aircraft portion, a thermoacoustic insulation module for an aircraft comprises a mat and a load-bearing structure detachably attached to the mat and supporting the mat in a curved shape, with an axis of curvature parallel to a longitudinal direction of the mat. A thermoacoustic insulation method for insulating an aircraft portion comprises a step of inserting the thermoacoustic insulation module into the aircraft portion, followed by a step of detaching the mat from the load-bearing structure, followed by a step of attaching the mat to an aircraft structure delimiting the aircraft portion, followed by a step of removing the load-bearing structure from the aircraft portion.

公开(公告)号：US20180178894A1

公开(公告)日：2018-06-28

申请号：US15847090

申请日：2017-12-19

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Laurent SAINT-MARC

IPC: B64C1/06 ,  B64F5/10

CPC classification number: B64C1/066 ,  B64C1/063 ,  B64C1/068 ,  B64C1/40 ,  B64D2011/0046 ,  B64F5/10

Abstract: A bendable element is formed at least from an inflatable envelope, a first bendable, elongate base plate attached to a first face of the inflatable envelope, a second bendable, elongate base plate, attached to a second face of the inflatable envelope and shorter than the first base plate, and links connecting the first base plate to the second base plate. The links are slack when the inflatable envelope is in a deflated state. The action of inflating the inflatable envelope causes the first and second base plates to bend in a direction of curvature extending from the first base plate to the second base plate, by means of the tensioning of the links such that the links extend along radii of curvature common to the first and second base plates while keeping the second base plate centered longitudinally relative to the first base plate.

公开(公告)号：US20170247121A1

公开(公告)日：2017-08-31

申请号：US15442129

申请日：2017-02-24

Applicant: Airbus Operations SAS

Inventor： Bernard Guering

IPC: B64F5/10 ,  B66C13/18 ,  B66C19/00 ,  B64C1/18

CPC classification number: B64C1/18 ,  B64C1/065 ,  B64C1/20 ,  B64F5/10 ,  B64F5/50 ,  B66C13/18 ,  B66C19/00

Abstract: A tooling making it possible to mount a module directly in an aircraft without making any modifications to the module. This tooling is made up of upper beams connected to the structure of the aircraft, lower beams secured to the module, lift elements connecting the lower beams to the upper beams and a drive system. The lift elements can move along the upper beams. The drive system makes it possible to convey the module to its functional location in the aircraft, by moving it along the upper beams via the lift elements. The principle of this tooling is to suspend the module in order to ensure and control its movement in the aircraft.

公开(公告)号：US09505483B2

公开(公告)日：2016-11-29

申请号：US14348093

申请日：2012-09-27

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering ,  Yves Durand

IPC: B64C1/14 ,  B64C1/06 ,  B64C25/14 ,  B64C1/10 ,  B64C1/36 ,  B64C25/04 ,  B64C25/10

CPC classification number: B64C1/14 ,  B64C1/061 ,  B64C1/10 ,  B64C1/36 ,  B64C25/04 ,  B64C25/10 ,  B64C25/14

Abstract: A forward part of an aircraft comprising a fuselage and a landing gear well housing a forward landing gear comprising a breaker strut designed to adopt an extended configuration when the landing gear is extended, configuration in which said breaker strut lies in a strut plane parallel to the transverse direction of the forward part. The forward part comprises a transverse beam resisting strut reactions located above the landing gear well and mounted on the fuselage at its two ends, the beam having a globally rectangular cross-section, in which the median plane parallel to the length of the rectangle is coincident with said strut plane.

Abstract translation: 一种飞机的前部，其包括机身和起落架井，该起落架井容纳前起落架，该前起落架包括设计成当起落架延伸时采用延伸构型的断路器支柱，其中所述断路器支柱位于平行于 前部横向。 前部包括位于起落架井上方的横向梁抵抗支柱反应，并在其两端安装在机身上，该梁具有全局矩形横截面，其中平行于矩形长度的中间平面重合 与支柱平面。

公开(公告)号：US09399517B2

公开(公告)日：2016-07-26

申请号：US14100771

申请日：2013-12-09

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B60N2/14 ,  B60N2/30 ,  B64D11/06 ,  A47C9/02 ,  B60N2/46 ,  B60N2/16 ,  B60N2/24

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：US09079666B2

公开(公告)日：2015-07-14

申请号：US13857378

申请日：2013-04-05

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B64D11/00 ,  B64C1/14 ,  B64D45/00 ,  E06B3/90

CPC classification number: B64D11/0023 ,  B64C1/1469 ,  B64D45/0015 ,  E06B3/903

Abstract: The invention relates to a secure access airlock enabling the communication between several rooms of an aircraft, the secure airlock being installed in an area of the aircraft between a first room and at least one second room, characterized in that it includes two mobile partitions provided in the form of portions of concentric cylinders, each of the partitions being capable of being moved, separately from one another, about a common axis, so as to provide a single opening therebetween which makes it possible to access either of the rooms, the two partitions being capable of moving over two concentric cylinders having different diameters.

Abstract translation: 本发明涉及一种能够在飞机的几个房间之间进行通信的安全通道气闸，所述安全气锁被安装在第一房间和至少一个第二房间之间的飞机区域中，其特征在于，它包括设置在 同心圆筒部分的形式，每个隔板能够彼此分开地围绕公共轴线移动，以便在其间提供单个开口，这使得可以进入任何一个房间，两个隔板 能够移动具有不同直径的两个同心圆柱体。

公开(公告)号：US20140166806A1

公开(公告)日：2014-06-19

申请号：US14106216

申请日：2013-12-13

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64D11/04

CPC classification number: B64D11/04 ,  B64D11/0007

Abstract: A piece of furniture for an aircraft, including a plurality of carriages a first section forming an interface of use for a user with which at least one carriage may be taken and/or deposited in the piece of furniture and a second section allowing the said carriages to be circulated along at least first and second main directions substantially perpendicular to each other, at least in a plane of the aircraft for storing and/or delivering to the user at least one carriage, the first section and/or the second section including an arrangement for distributing at least one carriage from the second section towards the first section and vice versa.

Abstract translation: 一种用于飞行器的家具，包括多个滑架，第一部分形成用于使用者的接口，至少一个托架可以与该家具相连和/或放置在该家具中;以及第二部分，允许所述托架 至少在飞行器的平面中沿着至少基本上彼此垂直的至少第一和第二主方向循环，以便向用户存储和/或传送至少一个滑架，第一部分和/或第二部分包括 用于从第二部分向第一部分分配至少一个托架的布置，反之亦然。