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    Aircraft galley monument structure
    2.
    发明授权
    Aircraft galley monument structure 有权

    公开(公告)号：US10029795B2

    公开(公告)日：2018-07-24

    申请号：US15164426

    申请日：2016-05-25

    Applicant: B/E Aerospace, Inc.

    Inventor： Peter John Leslie Burd

    IPC: B64D11/04 ,  B64D11/00

    Abstract: An improved monument structure combining an integrated construction system with carbon fiber reinforced composites to form an exoskeleton chassis that significantly reduces the build times, manufacturing skill level requirements, post processing activities, and overall weight of a given aircraft monument.

    Universal modular ducting for chilled aircraft galleys
    4.
    发明授权
    Universal modular ducting for chilled aircraft galleys 有权

    公开(公告)号：US09987902B2

    公开(公告)日：2018-06-05

    申请号：US14467583

    申请日：2014-08-25

    Applicant: B/E AEROSPACE, INC.

    Inventor： Peter John Leslie Burd

    IPC: B64D13/00 ,  B60H1/00 ,  B64D11/04 ,  F24F13/02 ,  F25D15/00 ,  B64D13/06

    CPC classification number: B60H1/00014 ,  B64D11/04 ,  B64D2013/0629 ,  F24F13/0263 ,  F25D15/00

    Abstract: A universal modular ducting apparatus for chilled aircraft galleys for either air over or air through carts has modular primary supply and return duct assemblies. Outlet port connection adapters are configured to connect chiller supply air duct outlet ports to either air through or air over configurations of aircraft galley food carts. The supply and return duct assemblies are internally insulated, and may be made from thermoformed plastic, prepreg, or a carbon fiber reinforced composite. Supply duct upper and lower portions may be connected by a connection adapter, and return duct upper and lower portions may be connected by a connection adapter, allowing the supply duct upper portion and the return duct upper portion to overlap.

    Intermediate Stowage Retainer for Aircraft Monument Storage Bay
    5.
    发明申请
    Intermediate Stowage Retainer for Aircraft Monument Storage Bay 审中-公开

    公开(公告)号：US20180016011A1

    公开(公告)日：2018-01-18

    申请号：US15647224

    申请日：2017-07-11

    Applicant: B/E Aerospace, Inc.

    Inventor： Peter John Leslie Burd ,  Neil R. Elshaw ,  Sam Foster ,  Venkata Prasanth Suman Neti ,  Allan Coombs ,  Donna Charlene Brownlie ,  Merv Davidson ,  Elizabeth M. Payne

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

    Abstract: In an illustrative embodiment, an intermediate retaining assembly secures a rearmost equipment item of at least two horizontally-stacked equipment items within an aircraft galley compartment. The intermediate retaining assembly may include a manual control coupled to a first end of a rod where rotation of the manual control causes rotation of the rod. A retaining lever may engage a second end of the rod upon moving the rod to an axially extended position such that rotation of the rod causes the retaining lever to rotate between a position for securing the rearmost equipment item and a position for removing the rearmost equipment item from or inserting into the compartment. A mounting plate may be secured to an interior surface of the compartment and may have a recess for receiving the retaining lever, preventing the retaining lever from interfering with the equipment item during insertion into or release from the compartment.

    Compact check valve for aircraft galley plumbing system
    8.
    发明授权
    Compact check valve for aircraft galley plumbing system 有权
    飞机厨房管道系统紧凑型止回阀

    公开(公告)号：US09469402B2

    公开(公告)日：2016-10-18

    申请号：US14676062

    申请日：2015-04-01

    Applicant: B/E Aerospace, Inc.

    Inventor： Peter John Leslie Burd

    IPC: G05D11/00 ,  B64D11/02 ,  B64D11/04 ,  F16K17/04 ,  F16K15/06 ,  F16K31/122

    CPC classification number: B64D11/02 ,  B64D11/04 ,  F16K15/063 ,  F16K15/066 ,  F16K17/048 ,  F16K31/1221 ,  Y10T137/2617 ,  Y10T137/2663 ,  Y10T137/7922 ,  Y10T137/87877

    Abstract: A check valve for an aircraft galley plumbing system having a valve body including an inlet for a potable water supply line, and first and second outlet ports leading to a distribution manifold. In a preferred embodiment, quick disconnects that include reverse flow inhibitors seal the valve's output ports. A vertical channel extends through the valve body for draining water through the valve, which is coupled to a pressure line connection port that exerts pressure from the aircraft's pressure system. A piston reciprocating across the vertical channel and biased by a spring is in fluid communication with the pressure line connection port, such that when water pressure is introduced from a pressure line to the connection port of sufficient pressure to collapse said spring, the piston blocks said channel, and when the water pressure is insufficient to collapse said spring then the piston retracts to open said channel.

    Abstract translation: 一种用于飞机厨房管道系统的止回阀，其具有包括用于饮用水供应管线的入口的阀体以及通向分配歧管的第一和第二出口。 在优选实施例中，包括逆流阻止器的快速断开器密封阀的输出端口。 垂直通道延伸穿过阀体以排出水通过阀，该阀连接到压力线连接端口，该压力线连接端口施加来自飞机压力系统的压力。 横跨垂直通道往复运动并被弹簧偏压的活塞与压力线连接口流体连通，使得当压力从压力线引导到具有足够压力的连接端口以使所述弹簧塌缩时，活塞阻挡所述 并且当水压不足以使所述弹簧塌缩时，活塞缩回以打开所述通道。

    Compact aircraft galley plumbing system
    9.
    发明授权
    Compact aircraft galley plumbing system 有权
    紧凑型飞机厨房管道系统

    公开(公告)号：US09096321B2

    公开(公告)日：2015-08-04

    申请号：US13862044

    申请日：2013-04-12

    Applicant: B/E Aerospace, Inc.

    Inventor： Peter John Leslie Burd

    IPC: B60R15/00 ,  B64D11/04 ,  B64D11/02

    CPC classification number: B64D11/04 ,  B64D11/02 ,  Y02T50/46 ,  Y10T137/794 ,  Y10T137/8593

    Abstract: An aircraft galley plumbing is disclosed comprising water distribution components and assemblies to allow installation in a wet/refrigerated reduced foot print galley. The system includes a single potable water distribution manifold with quick disconnect couplings for the GAINS and built in air bleed devices facilitate rapid drainage and easy installation. The system also includes a compact pressure check valve to control filling operation and drain down of the potable water system. The use of a compact air stop valve and integrated master distribution block (manifold) and water filter system further enhance the system.

    Abstract translation: 公开了一种飞机厨房管道，其包括配水部件和组件，以允许安装在湿/冷藏的脚印厨房中。 该系统包括一个单一的饮用水分配歧管，具有用于GAINS的快速断开联轴器，并内置放气装置，便于快速排水和易于安装。 该系统还包括紧凑型压力止回阀，用于控制饮用水系统的灌装操作和排水。 使用紧凑型空气截止阀和集成主分配块（歧管）和水过滤系统进一步增强系统。

    MEAL CART FOR AN AIRCRAFT GALLEY
    10.
    发明申请
    MEAL CART FOR AN AIRCRAFT GALLEY 有权
    用于飞机货柜的美食

    公开(公告)号：US20150048581A1

    公开(公告)日：2015-02-19

    申请号：US14528835

    申请日：2014-10-30

    Applicant: B/E Aerospace, Inc.

    Inventor： Peter John Leslie Burd

    IPC: B64D11/00 ,  B62B3/00

    CPC classification number: B64D11/0007 ,  B62B3/003 ,  B62B3/004 ,  B62B3/005 ,  B62B2202/021 ,  B62B2202/67 ,  B62B2501/065 ,  Y02T50/46

    Abstract: A service cart for an aircraft is disclosed with a housing of carbon fiber reinforced composites forming a multi-compartment carrier, the carrier adapted to hold four standard airline meal carriers. The cart includes at least a pair of cap doors at opposite ends of the cart, each cap door pivoting approximately 270 degrees to bear against a side of the cart, and a plurality of guides on inner walls of the multi-compartment for retaining the standard airline meal carriers. To prevent the doors of the cart from inadvertently opening, the cart also may include a redundant paddle latch system for each door.

    Abstract translation: 公开了一种用于飞机的服务车，其具有形成多隔室载体的碳纤维增强复合材料的壳体，所述载体适于容纳四个标准的航空公司膳食载体。 该推车包括在推车的相对两端的至少一对盖帽门，每个盖帽门枢转大约270度以抵靠在该车的一侧，以及在多隔室的内壁上的多个引导件，用于保持标准 航空餐饮承运人 为了防止推车的门不经意地打开，推车还可以包括用于每个门的冗余桨形闩锁系统。

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