公开(公告)号：US09650143B2

公开(公告)日：2017-05-16

申请号：US14566263

申请日：2014-12-10

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64D11/00 ,  B64D13/00

CPC classification number: B64D11/003 ,  B64D11/00

Abstract: A luggage system includes a luggage compartment having a base body and a flap which is movable between a closed position and an open position and is configured to make accessible or close an interior space of the base body. The flap includes a first flap element facing the interior space of the base body and a second flap element facing away from the interior space of the base body, wherein an installation space for components which are to be installed in the region of the luggage compartment is provided between the first and the second flap element.

公开(公告)号：US09428274B2

公开(公告)日：2016-08-30

申请号：US14278310

申请日：2014-05-15

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64D11/00 ,  B64D11/02 ,  B64D11/04 ,  B64C1/14

CPC classification number: B64D11/00 ,  B64C1/1423 ,  B64D11/0023 ,  B64D11/02 ,  B64D11/04

Abstract: An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module.

Abstract translation: 一种用于安装在包括第一功能模块的飞机机舱中的飞机纪念碑，所述第一功能模块包括侧壁，用于将所述第一功能模块与所述飞机机舱的与所述第一功能模块相邻的区域和/ 飞机纪念碑毗邻第一个功能模块。 侧壁可在第一和第二操作位置之间移动并且包括侧壁区域，其仅在侧壁的第二操作位置中用于将第一功能模块与第一功能模块相邻的飞机机舱的区域 模块，使得侧壁从其第一操作位置移动到其第二操作位置导致第一功能模块的基部区域的放大。

公开(公告)号：US20140339362A1

公开(公告)日：2014-11-20

申请号：US14278112

申请日：2014-05-15

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64D11/06 ,  B64C1/14 ,  B64D11/04 ,  B64D11/02

CPC classification number: B64D11/06 ,  B64C1/1438 ,  B64D11/02 ,  B64D11/04 ,  B64D11/0691 ,  Y02T50/46

Abstract: An aircraft monument for installation in an aircraft cabin comprising a sanitary module. The sanitary module comprises a toilet which is adapted to be used as a sanitary facility for passengers when an aircraft equipped with the aircraft monument is in cruising flight. The toilet is further adapted to be used as a flight attendant seat if necessary. The aircraft monument also comprises a door opening which is adapted, when the aircraft monument is installed in an aircraft, to give a person sitting on the toilet which is being used as a flight attendant seat an unimpeded view of an area of the aircraft cabin which is arranged in front of the aircraft monument in the direction of viewing of the person sitting on the toilet which is being used as a flight attendant seat.

Abstract translation: 一种用于安装在包括卫生模块的飞机机舱中的飞机纪念碑。 该卫生模块包括一个马桶，当装有飞机纪念碑的飞机正在巡航飞行时，该马桶适用于乘客的卫生设施。 如果需要，厕所还适合用作乘务员座位。 飞机纪念碑还包括门开口，当航空器纪念碑安装在飞行器中时，该门开口适于坐在正在用作乘务员座位的马桶上的人无人看见的飞机机舱的区域， 被安排在飞机纪念碑的前面，观察坐在马桶上的人正在用作乘务员座位的方向。

公开(公告)号：US20140332640A1

公开(公告)日：2014-11-13

申请号：US14444098

申请日：2014-07-28

Applicant: Airbus Operations GmbH

Inventor： Matthias Breuer ,  Wei-Chung Tuan ,  Frank Klepka

IPC: B64C1/00 ,  B64F5/00 ,  F16L3/26

CPC classification number: F16L3/26 ,  B64C1/00 ,  B64C1/064 ,  B64D11/00 ,  B64D2011/0046 ,  B64F5/10 ,  Y02T50/46 ,  Y10T29/49826

Abstract: A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements.

Abstract translation: 一种用于将飞机系统部件安装在飞机的冠部区域中的系统，包括第一纵向载体元件，第二纵向载体元件和将第一纵向载体元件连接到第二纵向载体元件的桥接元件。 该系统可安装在飞行器的冠部区域中，使得第一和第二纵向载体元件基本上平行于飞行器的纵向轴线延伸。 用于容纳电线的多个电缆导管设置在第一和/或第二纵向载体元件上。

公开(公告)号：US09457903B2

公开(公告)日：2016-10-04

申请号：US14277304

申请日：2014-05-14

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64D11/00 ,  B64D13/00 ,  B64D11/02 ,  B64D11/04

CPC classification number: B64D11/00 ,  B64D11/02 ,  B64D11/04 ,  B64D2011/0046

Abstract: An aircraft monument for installation in an aircraft cabin comprising a first functional module, a second functional module and a side wall for delimiting the first module from at least one of a region of the aircraft cabin adjacent to the first module and a region of the aircraft monument adjacent to the first module. The side wall is movable between a first and a second operational position and comprises a first side-wall region separating the first and second functional modules and in the second operational position, the side wall is displaced in the direction of the second module relative to its position in the first operational position, so that a movement of the side wall from its first operational position into its second operational position results in an enlargement of a base area of the first module and a corresponding diminution of a base area of the second module.

Abstract translation: 一种用于安装在飞机机舱中的飞机纪念碑，包括第一功能模块，第二功能模块和侧壁，用于将第一模块与第一模块相邻的飞机机舱的区域中的至少一个和飞机的区域 纪念碑毗邻第一个模块。 侧壁可在第一和第二操作位置之间移动，并且包括分隔第一和第二功能模块的第一侧壁区域，并且在第二操作位置，侧壁相对于第二模块的第二模块的方向移位 位置处于第一操作位置，使得侧壁从其第一操作位置移动到其第二操作位置导致第一模块的基础面积的扩大和第二模块的基础面积的相应减小。

公开(公告)号：US20140339361A1

公开(公告)日：2014-11-20

申请号：US14278018

申请日：2014-05-15

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64D11/00 ,  B64D11/06 ,  B64D11/04 ,  B64D9/00 ,  B64D11/02

CPC classification number: B64D11/0023 ,  B64D9/00 ,  B64D11/00 ,  B64D11/02 ,  B64D11/04 ,  B64D11/06 ,  B64D11/0691 ,  B64D2011/0046

Abstract: An aircraft area comprises at least one main aisle which extends along a longitudinal axis of an aircraft cabin, a door aisle which extends, substantially perpendicularly to the at least one main aisle, along a transverse axis of the aircraft cabin between a first and a second aircraft door, and an aircraft monument which is arranged substantially centrally in the door aisle.

Abstract translation: 飞机区域包括至少一个沿着飞机机舱的纵向轴线延伸的主通道，大门垂直于至少一个主通道的门通道沿飞机机舱的横向轴线在第一和第二通道之间延伸 飞机门，以及大致在门通道中央布置的飞机纪念碑。

公开(公告)号：US10343779B2

公开(公告)日：2019-07-09

申请号：US15114740

申请日：2015-01-29

Applicant: Airbus Operations GmbH

Inventor： Matthias Breuer ,  Sabrina Moje

IPC: B64C1/14 ,  B64D11/02

Abstract: An aircraft interior door assembly (10, 20, 30) for selectively increasing usable space within an aircraft lavatory (1) adjacent a passenger doorway area (2) of the aircraft or in the passenger doorway area (2) adjacent the lavatory (1) comprises a door element (12, 22, 32) and a door element supporting structure (13, 23, 33). The door element (12, 22, 32) is rotatably mounted to the door element supporting structure (13, 23, 33) so as to be at least rotatable between first and second closed positions relative to the door element supporting structure (13, 23, 33). The door element (12, 22, 32) has the same configuration in both of its closed positions. A door rotation space which is encompassed by the door element (12, 22, 32) when positioned in its first and second closed positions or rotated through by the door element (12, 22, 32) when rotated between its first and second closed positions is part of the aircraft lavatory interior space, when the door element (12, 22, 32) is in its first closed position, and is part of the passenger doorway area (2), when the door element (12, 22, 32) is in its second closed position.

公开(公告)号：US20160059964A1

公开(公告)日：2016-03-03

申请号：US14828671

申请日：2015-08-18

Applicant: Airbus Operations GmbH

Inventor： Matthias Breuer ,  Sabrina Moje

IPC: B64D11/00

Abstract: A separating device for separating two zones of a passenger cabin equipped with overhead luggage bins comprising a movable shell comprising a curtain element made of a flexible material and being dimensioned and shaped so as to be capable of at least partially covering an area extending below an overhead luggage bin with its movable shell being in its closed position in a direction substantially perpendicular to a longitudinal axis of the overhead luggage bin. The curtain element has a first edge adapted to face the movable shell of the overhead luggage bin when the separating device is mounted in the passenger cabin. The separating device further comprises a holder supporting a first end of the first edge of the curtain element and a fixing device adapted to fix a second end of the first edge of the curtain element to the movable shell of the overhead luggage bin.

Abstract translation: 一种分离装置，用于分离配备有架空行李箱的客舱的两个区域，所述分离装置包括可移动壳体，所述可移动壳体包括由柔性材料制成的帘式元件，并且其尺寸和形状使得能够至少部分地覆盖在顶部下方延伸的区域 行李箱的可动壳体处于其基本上垂直于架空行李箱的纵向轴线的方向上的关闭位置。 当分离装置安装在客舱中时，窗帘元件具有适于面向高架行李箱的可移动外壳的第一边缘。 所述分离装置还包括支撑所述帘式元件的所述第一边缘的第一端的保持器和适于将所述帘式元件的所述第一边缘的第二端固定到所述架空行李箱的可移动壳体的固定装置。

公开(公告)号：US09073619B2

公开(公告)日：2015-07-07

申请号：US14065671

申请日：2013-10-29

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

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

CPC classification number: B64C1/1469 ,  B64D45/0015 ,  E06B3/906

Abstract: A security door comprises a frame structure, having a lateral surface in which a plurality of doorways are constructed. A first doorway has a first width along an inner circumference of the frame structure, and lateral surface portions delimiting the first doorway in a first direction and a second direction, opposing the first direction, along the inner circumference of the frame structure have a second width. A lock element is received in the frame structure and comprises a first segment, movable along the frame structure inner circumference relative to the frame structure, and a second segment, movable independently of the first segment along the inner circumference relative to the frame structure. The first segment is dimensioned so that, in a position in which it closes the first doorway, it also closes a second doorway adjacent to the first doorway in the first direction along the frame structure inner circumference.

Abstract translation: 安全门包括框架结构，其具有构造多个门口的侧表面。 第一门口沿着框架结构的内周具有第一宽度，并且沿框架结构的内圆周沿与第一方向相反的第一方向和第二方向限定第一门口的侧表面部分具有第二宽度 。 锁定元件被容纳在框架结构中并且包括可相对于框架结构沿着框架结构内圆周移动的第一段，以及第二段，其可相对于框架结构沿着内圆周独立于第一段移动。 第一段的尺寸使得在其关闭第一门口的位置中，它还沿着框架结构的内周在第一方向上关闭与第一门口相邻的第二门口。

公开(公告)号：US20140115966A1

公开(公告)日：2014-05-01

申请号：US14065671

申请日：2013-10-29

Applicant: Airbus Operations GmbH

Inventor： Sabrina Moje ,  Matthias Breuer

IPC: B64C1/14 ,  B64D45/00

CPC classification number: B64C1/1469 ,  B64D45/0015 ,  E06B3/906

Abstract: A security door comprises a frame structure, having a lateral surface in which a plurality of doorways are constructed. A first doorway has a first width along an inner circumference of the frame structure, and lateral surface portions delimiting the first doorway in a first direction and a second direction, opposing the first direction, along the inner circumference of the frame structure have a second width. A lock element is received in the frame structure and comprises a first segment, movable along the frame structure inner circumference relative to the frame structure, and a second segment, movable independently of the first segment along the inner circumference relative to the frame structure. The first segment is dimensioned so that, in a position in which it closes the first doorway, it also closes a second doorway adjacent to the first doorway in the first direction along the frame structure inner circumference.

Abstract translation: 安全门包括框架结构，其具有构造多个门口的侧表面。 第一门口沿着框架结构的内周具有第一宽度，并且沿框架结构的内圆周沿与第一方向相反的第一方向和第二方向限定第一门口的侧表面部分具有第二宽度 。 锁定元件被容纳在框架结构中并且包括可相对于框架结构沿着框架结构内圆周移动的第一段，以及第二段，其可相对于框架结构沿着内圆周独立于第一段移动。 第一段的尺寸使得在其关闭第一门口的位置中，它还沿着框架结构的内周在第一方向上关闭与第一门口相邻的第二门口。