公开(公告)号：US09469401B2

公开(公告)日：2016-10-18

申请号：US14132982

申请日：2013-12-18

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64D11/02 ,  B64D25/08

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：US09446850B2

公开(公告)日：2016-09-20

申请号：US13970867

申请日：2013-08-20

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Yves Durand

IPC: B64C1/00 ,  B64D13/08 ,  B64D13/00 ,  B64D13/06

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：US09387919B2

公开(公告)日：2016-07-12

申请号：US13628145

申请日：2012-09-27

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B64C1/06 ,  B64C1/14

CPC classification number: B64C1/061 ,  B64C1/1476

Abstract: An aircraft nose structure comprising 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: 一种飞机鼻梁结构，其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。

公开(公告)号：US09290259B2

公开(公告)日：2016-03-22

申请号：US14138551

申请日：2013-12-23

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64C1/00 ,  B64C1/18 ,  B64D11/00 ,  B64D43/00 ,  B64F5/00

CPC classification number: B64C1/00 ,  B64C1/18 ,  B64D11/00 ,  B64D43/00 ,  B64F5/10 ,  Y10T29/49826

Abstract: An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical and/or electronic equipment. The cockpit and the avionics bay are each made in the form of a distinct module that is suitable for being installed in a single operation inside the primary fuselage structure. The use of modules for integrating in the aircraft nose makes it possible to reduce considerably the time required for fitting out the nose on the final assembly line of the aircraft.

Abstract translation: 包括主机架结构并且容纳在所述结构内的飞行器鼻架，驾驶舱和航空电子设备舱，其包含设计成接收电和/或电子设备的多个航空电子设备架。 驾驶舱和航空电子设备舱均采用独特模块的形式，适合安装在主机身结构内的单一操作中。 使用用于集成在飞机鼻部中的模块可以大大减少在飞机的最终装配线上安装鼻子所需的时间。

公开(公告)号：US09221541B2

公开(公告)日：2015-12-29

申请号：US14106216

申请日：2013-12-13

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64D11/04 ,  B64D11/00

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。

公开(公告)号：US20140175223A1

公开(公告)日：2014-06-26

申请号：US14138581

申请日：2013-12-23

Applicant: Airbus Operations (SAS)

Inventor： Yves Durand ,  Bernard Guering

IPC: B64C25/00 ,  B64D11/00 ,  B64C1/18

CPC classification number: B64D11/00 ,  B64C1/061 ,  B64C1/068 ,  B64C1/18 ,  B64C25/04 ,  B64C25/14

Abstract: An aircraft front portion in which the landing gear storage bay is arranged under a cockpit floor. The landing gear bay is mechanically connected to the fuselage frames of the aircraft front portion in order to perform the function of taking up the mechanical forces acting on the fuselage frames under the effect of pressurization. The cockpit floor is thus simplified since it serves solely as a plane for the crew to walk on and it can be lowered so as to release space in the cockpit.

Abstract translation: 飞机前部，其中起落架存储舱布置在驾驶舱地板下方。 起落架舱机械地连接到飞行器前部的机身框架，以便在加压的作用下执行作用在机身框架上的机械力的功能。 因此，驾驶舱地板被简化，因为它仅仅作为乘员人员行走的飞机，并且可以降低以释放驾驶舱中的空间。

公开(公告)号：US20130292513A1

公开(公告)日：2013-11-07

申请号：US13857378

申请日：2013-04-05

Applicant: Airbus Operations (SAS)

Inventor： Bernard Guering

IPC: B64D11/00

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：US11597491B2

公开(公告)日：2023-03-07

申请号：US16719255

申请日：2019-12-18

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Romain Delahaye

IPC: B64C1/12 ,  B64C1/06 ,  B64C1/40

Abstract: A wall covering panel for a nose of an aircraft. The panel comprises a rigid carrying framework preferably having an alveolar structure obtained by 3-D printing, a décor carried by the carrying framework and an acoustically and thermally insulating padding fixed to the carrying framework, and also attachments for fixing the carrying framework to the primary structure of the aircraft. Preferably, the panel also integrates systems, such as electrical route portions or ventilation route portions that traverse the panel from one side to the other or lead to an outlet equipment item also integrated in the panel. Only the carrying structure of the panel, which carries the décor, the insulating padding and any route portions and equipment items, is fixed to the primary structure of the aircraft. The number of attachments is low; the kitting-out and the finishing of the nose of the aircraft are greatly simplified.

公开(公告)号：US11548618B2

公开(公告)日：2023-01-10

申请号：US16411361

申请日：2019-05-14

Applicant: Airbus Operations SAS

Inventor： Bernard Guering ,  Matthieu De Kergommeaux

IPC: B64C13/04 ,  B64C13/50 ,  B64C13/06

Abstract: A rudder bar includes a main module provided at least with pedals and with all the elements subject to maintenance, the main module being one-piece and detachable relative to a support frame integrated into the floor of the cockpit of the aircraft, so as to exhibit significant flexibility with respect to its maintainability, particularly in the event of the failure of a component, by allowing quick intervention both on a local level and an overall level.

公开(公告)号：US10737767B2

公开(公告)日：2020-08-11

申请号：US15332247

申请日：2016-10-24

Applicant: AIRBUS OPERATIONS (SAS)

Inventor： Bernard Guering ,  Laurent Saint-Marc

IPC: B64C13/04 ,  B64C13/28

Abstract: A suspended rudder bar for aircraft and aircraft having a suspended rudder bar, which includes a set of primary hinges, a set of secondary hinges including control and synchronization devices, and a set of linkages generating functional and structural links between the set of primary hinges and the set of secondary hinges, wherein the primary hinges are configured to be suspended at least on a structure supporting the instrument panel of the flight deck of the aircraft, and the secondary hinges configured to be suspended at least on a structural component of an area situated forward of the flight deck.