公开(公告)号：WO2015153682A1

公开(公告)日：2015-10-08

申请号：PCT/US2015/023707

申请日：2015-03-31

Applicant: B/E AEROSPACE, INC.

Inventor： CLAFLIN, Shawn A. ,  HAUSER, James Brian

IPC: B64D11/00 ,  F16J3/06 ,  F15B15/10

CPC classification number: F15B15/149 ,  B64D11/00 ,  B64D11/003 ,  B64D11/04 ,  F15B15/10 ,  F15B2211/411 ,  F15B2211/41581 ,  F15B2211/7052 ,  F15B2211/7053 ,  F15B2211/89 ,  F16J3/06 ,  F16M13/022

Abstract: A vacuum powered system (20) for moving a movable component, such as for raising and lowering a stowage container (22a, 22b, 22c), includes a vacuum actuator (34) connected between a fixed structure and a movable component. The vacuum actuator (34) includes one or more intake ports that are configured to connect with a source of vacuum for moving the movable component in a first direction to a first position, and one or more bleed valve ports for venting the vacuum actuator to move the movable component in a second direction to a second position. The vacuum actuator (34) may be an air bellows, a single acting linear vacuum actuator, or a dual acting linear vacuum actuator. A guiding system is further provided that includes elongated tracks in a stationary stowage container housing that houses the movable component, and corresponding guide elements on the movable component that slidably engage with the elongated tracks for moving the movable component.

Abstract translation: 用于移动可移动部件的真空动力系统（20），诸如用于升高和降低存放容器（22a，22b，22c）的装置包括连接在固定结构和可移动部件之间的真空致动器（34）。 真空致动器（34）包括一个或多个进气口，其被构造成与用于将可移动部件沿第一方向移动到第一位置的真空源连接，以及一个或多个排气阀端口，用于使真空致动器移动 所述可移动部件在第二方向上到达第二位置。 真空致动器（34）可以是空气波纹管，单作用线性真空致动器或双作用线性真空致动器。 还提供了一种引导系统，其包括容纳可移动部件的固定存放容器壳体中的细长轨道，以及可移动部件上的相应引导元件，其可滑动地与细长轨道接合以移动可移动部件。

公开(公告)号：WO2014138706A1

公开(公告)日：2014-09-12

申请号：PCT/US2014/022142

申请日：2014-03-07

Applicant: B/E AEROSPACE, INC.

Inventor： JOHNSON, Wade ,  HAUSER, James Brian

IPC: B64D11/06

CPC classification number: B64D11/0691 ,  B60N2/24 ,  B60N2/242 ,  B60N2/30 ,  B64D11/06 ,  B64D11/0639 ,  B64D11/0689

Abstract: A retractable flight attendant chair (161) includes an anchor box (180), a sled (200) coupled to the anchor box (180) for horizontal translation of the retractable chair (161) into and out of the stowage compartment (160), and a chair (161) mounted on the sled (200). The chair (161) includes an expanding/folding backrest (190) and seat portion (195) that allows the chair (180) to be stowed in a small envelope compartment (160) when not in use.

Abstract translation: 伸缩式乘务员座椅（161）包括锚固箱（180），联接到锚固箱（180）的滑雪板（200），用于可伸缩椅子（161）进入和离开装载室（160）的水平平移， 以及安装在所述滑板（200）上的椅子（161）。 椅子（161）包括在不使用时允许椅子（180）被收纳在小信封隔间（160）中的展开/折叠靠背（190）和座部（195）。

公开(公告)号：WO2014124381A1

公开(公告)日：2014-08-14

申请号：PCT/US2014/015605

申请日：2014-02-10

Applicant: B/E AEROSPACE, INC.

Inventor： IVESTER, Clarence ,  MCKEE, Jeffery ,  JOHNSON, Wade ,  HAUSER, James Brian ,  PAPKE, Robert ,  BENTON, David R. ,  HASHBERGER, Frank E.

IPC: B64D11/02 ,  B64D11/04

CPC classification number: B64D11/02 ,  B64D11/04

Abstract: A combination lavatory and galley arrangement (120) for aircraft includes a lavatory portion (128) having adjacent inboard and outboard lavatories, and a galley portion (124), and can be located aft of aft aircraft aft doors (26, 28), and can at least partially rearwardly extend into the aircraft's aft pressure dome (38). The inboard and outboard lavatories can be separated by a movable wall or partition (176) to provide access for persons with restricted mobility, and can be provided in a modular housing to facilitate retrofit assembly within an aircraft. The movable wall (176) can be an articulating movable lavatory partition movable between a first, linearly extended configuration and a second, folded configuration in a stowed position to provide entry for persons with restricted mobility.

Abstract translation: 用于飞行器的组合式卫生间和厨房布置（120）包括具有相邻的内侧和外侧盥洗室的卫生间部分（128）和厨房部分（124），并且可以位于后部飞机后部门（26,28）的后方，以及 可以至少部分地向后延伸到飞机的后压力圆顶（38）中。 内侧和外侧盥洗室可以由可移动的墙壁或隔板（176）分开，以便对具有限制的移动性的人提供通道，并且可以设置在模块化的壳体中以便于在飞行器内进行改装。 可移动壁（176）可以是可在第一线性延伸构造和第二折叠构型之间移动的铰接式可移动盥洗间隔，该构型位于收起位置以为具有受限移动性的人提供入口。

公开(公告)号：WO2017003814A1

公开(公告)日：2017-01-05

申请号：PCT/US2016/038980

申请日：2016-06-23

Applicant: B/E AEROSPACE, INC.

Inventor： CLAFLIN, Shawn A. ,  PAPKE, Robert ,  HAUSER, James Brian ,  MCKEE, Jefferey

IPC: B64D11/04

CPC classification number: B64D11/003 ,  B64D11/04 ,  B64D47/02 ,  E05C1/085 ,  E05C9/10 ,  F04B45/0536 ,  Y02T50/46

Abstract: An aircraft overhead stowage system for a cross-aisle galley complex. The aircraft overhead stowage system includes a stowage compartment housing disposed above a ceiling of the galley complex that is supported above the ceiling by a stowage support structure. A first stowage compartment and a second stowage compartment are each movably engaged with and disposed inside the stowage compartment housing, and each stowage compartment is movable between a stowed position and a deployed position relative to the stowage compartment housing using a vacuum system. A vacuum generator that creates a vacuum force is mounted on the stowage compartment housing, and a plurality of vacuum bellows connected to each stowage compartment are in fluid communication with the vacuum generator. The vacuum system causes the stowage compartments to move between the stowed position and the deployed position. Vacuum-driven and manually-driven latching assemblies and removable extensions for each stowage compartment are also provided.

Abstract translation: 用于跨通道厨房综合体的飞机架空装载系统。 飞机架空存储系统包括：设置在厨房组合体的天花板上方的装载舱室，其通过一个装载支撑结构支撑在天花板上方。 第一装载隔间和第二存放舱各自可移动地接合并设置在装载舱室内，并且每个存放隔间可使用真空系统相对于装载舱室在收起位置和展开位置之间移动。 产生真空力的真空发生器安装在储存箱壳体上，并且连接到每个装载室的多个真空波纹管与真空发生器流体连通。 真空系统使得存放隔间在收起位置和展开位置之间移动。 还提供了用于每个存放隔间的真空驱动和手动驱动的闩锁组件和可移除的延伸部。