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    Decompression panel for use in an aircraft assembly
    2.
    发明授权
    Decompression panel for use in an aircraft assembly 有权
    用于飞机总成的减压板

    公开(公告)号：US09566759B2

    公开(公告)日：2017-02-14

    申请号：US14471161

    申请日：2014-08-28

    Applicant: The Boeing Company

    Inventor： Thomas Perkins ,  Jeremy Ryan Glaze Tatum ,  Allan A. Loken ,  Hannah Rebecca Arm

    IPC: B64C1/00 ,  B32B3/26 ,  B64C1/18

    CPC classification number: B32B3/266 ,  B64C1/18 ,  B64C2001/009 ,  Y10T29/49622 ,  Y10T428/24273

    Abstract: A decompression panel for use in an aircraft assembly that includes a body portion including a top edge and a bottom edge, and a front surface and a rear surface opposing the front surface. A plurality of openings are formed in the body portion, and a first stiffening member is formed on the rear surface below the plurality of openings. The first stiffening member extends from the rear surface towards the top edge such that the plurality of openings are at least partially obstructed by the first stiffening member.

    Abstract translation: 一种用于飞机组件的减压板，包括：主体部分，其包括顶部边缘和底部边缘;以及前表面和与前表面相对的后表面。 多个开口形成在主体部分中，第一加强构件形成在多个开口下方的后表面上。 第一加强构件从后表面朝向顶部边缘延伸，使得多个开口至少部分地被第一加强构件阻挡。

    Hatch assembly for use in a vehicle and method of assembling the same
    5.
    发明授权
    Hatch assembly for use in a vehicle and method of assembling the same 有权
    用于车辆的舱口组件及其组装方法

    公开(公告)号：US09592902B2

    公开(公告)日：2017-03-14

    申请号：US14182015

    申请日：2014-02-17

    Applicant: The Boeing Company

    Inventor： Thomas Perkins ,  David J. Hinderer ,  Kalai Ben Ho ,  Jeremy Ryan Glaze Tatum

    IPC: B64C1/14 ,  B64D11/06

    CPC classification number: B64C1/1461 ,  B64C1/1423 ,  B64C1/1484 ,  B64D11/0646

    Abstract: A hatch assembly for use in a vehicle is provided. The hatch assembly includes a hatch structure including an upper portion and a lower portion, an armrest support rail coupled to the hatch structure and defining a shade slot between the hatch structure and the armrest support rail, and a shade sized for insertion through the shade slot. The shade is configured to selectively translate between the upper portion and the lower portion of the hatch structure through the shade slot.

    Abstract translation: 提供了一种用于车辆的舱口组件。 舱口组件包括一个包括上部和下部的舱口结构，一个与舱口结构相连的扶手支撑轨道，并且在舱口结构和扶手支撑轨道之间形成一个遮蔽槽，并设有一个阴罩， 。 荫罩构造成通过遮光槽选择性地在舱口结构的上部和下部之间平移。

    DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT
    6.
    发明申请
    DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT 有权
    用于飞机使用的拆卸面板

    公开(公告)号：US20150115102A1

    公开(公告)日：2015-04-30

    申请号：US14228524

    申请日：2014-03-28

    Applicant: The Boeing Company

    Inventor： Thomas Perkins ,  Michael J. Olliges ,  Allan A. Loken ,  Hannah Rebecca Arm ,  Jeremy Ryan Glaze Tatum

    IPC: B64C1/06 ,  B32B3/06

    CPC classification number: B64C1/069 ,  B32B3/06 ,  B64C1/18 ,  B64C2001/009 ,  B64F5/10 ,  Y10T428/24777

    Abstract: A decompression panel includes a body portion having a first end and a second end opposing the first end. The decompression panel also includes a tab extending along the first end and a flange coupled to the body portion. The flange defines a slot adjacent the second end. The decompression panel is secured in an airplane cabin by the tab and slot features, such that unwanted access to areas behind such panels is prevented.

    Abstract translation: 减压板包括主体部分，其具有第一端和与第一端相对的第二端。 减压面板还包括沿着第一端延伸的突出部和连接到主体部分的凸缘。 凸缘限定了与第二端相邻的槽。 减压板通过突片和槽特征固定在飞机机舱中，使得不期望地进入这些面板后面的区域。

    DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT
    9.
    发明申请
    DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT 有权
    用于飞机的拆卸面板

    公开(公告)号：US20170043856A1

    公开(公告)日：2017-02-16

    申请号：US15336397

    申请日：2016-10-27

    Applicant: The Boeing Company

    Inventor： Thomas Perkins ,  Michael J. Olliges ,  Allan A. Loken ,  Hannah Rebecca Arm ,  Jeremy Ryan Glaze Tatum

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

    CPC classification number: B64C1/069 ,  B32B3/06 ,  B64C1/18 ,  B64C2001/009 ,  B64F5/10 ,  Y10T428/24777

    Abstract: A method of installing and replacing a plurality of decompression panels into a sidewall assembly of an aircraft includes coupling a first decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly. The method also includes inserting a tab of the first decompression panel into a slot of a second decompression panel. The slot is defined by a flange extending along a surface of the second decompression panel. The method further includes coupling the second decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly.

    Abstract translation: 将多个减压板安装和更换为飞行器的侧壁组件的方法包括将第一减压面板联接到侧壁组件的侧壁和底板中的至少一个。 该方法还包括将第一解压面板的突片插入第二减压板的槽中。 槽由沿着第二减压板的表面延伸的凸缘限定。 该方法还包括将第二减压面板耦合到侧壁组件的侧壁和底板中的至少一个。

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