中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

222 records (took 0.019 seconds)

    Coaxial pressure lock assembly of an aircraft door
    1.
    发明授权
    Coaxial pressure lock assembly of an aircraft door 有权

    公开(公告)号：US11661166B2

    公开(公告)日：2023-05-30

    申请号：US17450136

    申请日：2021-10-06

    Applicant: The Boeing Company

    Inventor： Michael T. Mortland

    IPC: B64C1/14 ,  B64C1/00

    CPC classification number: B64C1/1423 ,  B64C2001/009

    Abstract: A coaxial pressure lock assembly of an aircraft door, the coaxial pressure lock assembly comprises a pressure panel positioned adjacent an opening formed in the aircraft door such that the pressure panel is seated in the opening when the pressure panel is in a closed position, and a latch shaft extending through a clevis of the pressure panel. The latch shaft is configured to rotate about a latch shaft rotational axis extending through the latch shaft. The pressure panel is rotatable between the closed position and an open position about the latch shaft rotational axis. The latch shaft is a portion of a latch assembly configured to allow or prevent unlatching the aircraft door.

    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。

    PRESSURE RELIEF PANEL GUARD
    4.
    发明申请
    PRESSURE RELIEF PANEL GUARD 审中-公开
    压力扶梯板

    公开(公告)号：US20150225068A1

    公开(公告)日：2015-08-13

    申请号：US14601126

    申请日：2015-01-20

    Applicant: William J. Boyer

    Inventor： William J. Boyer

    IPC: B64C1/22 ,  B64C1/00

    CPC classification number: B64C1/1446 ,  B64C1/1461 ,  B64C1/18 ,  B64C2001/009

    Abstract: A pressure relief panel guard for use with a pressure relief ceiling panel having a perimeter and positioned in an aircraft cargo bay ceiling. The panel guard including a mounting structure attachable to the cargo bay ceiling, and having a mounting portion and a guard support portion, and a guard structure releasably supported by the guard support portion of the mounting structure. The guard structure having a perimeter wall and a central opening between the perimeter wall sized such that when supported by the guard support portion of the mounting structure at the pressure relief ceiling panel the pressure relief ceiling panel is vertically aligned with the central opening with the perimeter wall extending about the perimeter of the pressure relief ceiling panel and the perimeter wall does not overlap the pressure relief ceiling panel or otherwise restrict operational access to the pressure relief ceiling panel from below.

    Abstract translation: 一个压力释放面板防护罩，用于具有周边并位于飞机货舱顶棚的减压天花板面板。 所述面板护罩包括可安装在所述货舱顶板上的安装结构，并且具有安装部分和防护支撑部分，以及由所述安装结构的所述保护支撑部分可释放地支撑的防护结构。 防护结构具有周边壁和在周边壁之间的中心开口，其尺寸设计成使得当在压力释放天花板面板处由安装结构的保护支撑部支撑时，压力释放顶板与中心开口垂直对齐，其周长 围绕减压天花板的周边延伸的壁和周壁不与减压天花板相重叠，或以其它方式限制从下方到达减压天花板的操作通路。

    DOOR ASSEMBLY FOR AIRCRAFT INTERIOR
    5.
    发明申请
    DOOR ASSEMBLY FOR AIRCRAFT INTERIOR 审中-公开
    飞机内部门组件

    公开(公告)号：US20150210373A1

    公开(公告)日：2015-07-30

    申请号：US14421625

    申请日：2012-08-17

    Applicant: Jean-Francois Guimont ,  Yvan Rosa ,  Benjamin Tremblay ,  Usher Boxer

    Inventor： Jean-Francois Guimont ,  Yvan Rosa ,  Benjamin Tremblay ,  Usher Boxer

    IPC: B64C1/14 ,  E06B7/16 ,  E06B7/28 ,  B64D25/00

    CPC classification number: B64C1/1438 ,  B64C1/1469 ,  B64C2001/009 ,  B64D25/00 ,  E06B7/16 ,  E06B7/28

    Abstract: Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door for opening and closing an aperture between zones of the aircraft interior and an interface configured to couple the door to the aircraft interior. A pressure-relief element may form at least a portion of the door wherein the pressure-relief element is retained by a magnetic force calibrated to permit release of the pressure-relief element upon presence of a predetermined pressure differential across the pressure-relief element. Components and mechanisms useful in reducing light bleed across doors for aircraft interiors are also disclosed.

    Abstract translation: 描述了飞机内饰的门组件。 这种门组件可以包括用于打开和关闭飞机内部的区域之间的孔的门和被配置为将门连接到飞行器内部的接口。 减压元件可以形成门的至少一部分，其中减压元件通过校准的磁力保持，以允许在存在预定压力差的压力释放元件上时释放压力释放元件。 还公开了用于减少用于飞机内部的门的轻度渗流的组件和机构。

    Interlocking vent assembly for equalizing pressure in a compartment
    9.
    发明授权
    Interlocking vent assembly for equalizing pressure in a compartment 有权
    联锁排气口组件，用于均衡隔室中的压力

    公开(公告)号：US08651924B1

    公开(公告)日：2014-02-18

    申请号：US12775438

    申请日：2010-05-06

    Applicant: Timothy M. Jones ,  Russell W. Keck

    Inventor： Timothy M. Jones ,  Russell W. Keck

    IPC: B64D13/02

    CPC classification number: B64D13/02 ,  B64C2001/009

    Abstract: A method for privately transferring filtered air through a partition of a compartment in an aircraft cabin to equalize a pressure difference between the inside and outside the compartment via a vent assembly comprising two substantially structurally identical vent halves joining together in a locking manner through a vent opening in the partition. Each vent half comprising integrally molded rim, frame, plurality of louvers fixed within the frame, latch, keeper, guide prong, and a installation index key; plastic injection molded from high strength unreinforced polycarbonate.

    Abstract translation: 一种用于将过滤的空气私自转移通过飞机机舱中的隔间的隔板的方法，以通过排气组件平衡隔室内部和外部之间的压差，该排气组件包括两个基本上结构相同的排气半部，其以锁定方式连接在一起，通过排气口 在分区中。 每个排气口半部包括整体模制的轮辋，框架，固定在框架内的多个百叶窗，闩锁，保持器，引导插脚和安装索引键; 由高强度非增强聚碳酸酯注塑成型。

    METHOD AND APPARATUS FOR ESTABLISHING AN ENVIRONMENTALLY ISOLATED VOLUME
    10.
    发明申请
    METHOD AND APPARATUS FOR ESTABLISHING AN ENVIRONMENTALLY ISOLATED VOLUME 有权
    用于建立环境分离体积的方法和装置

    公开(公告)号：US20130340954A1

    公开(公告)日：2013-12-26

    申请号：US13781004

    申请日：2013-02-28

    Applicant: THE BOEING COMPANY

    Inventor： Brad A. Kauffman

    IPC: E06B5/16

    CPC classification number: E06B5/16 ,  B64C1/00 ,  B64C1/066 ,  B64C1/069 ,  B64C1/10 ,  B64C1/406 ,  B64C2001/009 ,  B64D11/0023 ,  B64D45/00

    Abstract: A method and apparatus are provided for at least partially environmentally isolating a volume, such as by environmentally isolating the cargo compartment from the passenger compartment of an aircraft. In the context of an apparatus, a barrier curtain is provided that partially defines the volume. The apparatus also includes a cable extending along one or more walls that partially define the volume. The barrier curtain is supported by the cable. The apparatus may also include a cable release mechanism attached to a respective wall. The cable is carried by the cable release mechanism and the cable release mechanism is configured to fail at a predetermined load, thereby permitting the barrier curtain to drop in response to a decompression event.

    Abstract translation: 提供了一种方法和装置，用于至少部分地环境地隔离体积，例如通过将货舱与飞行器的乘客舱环境隔离。 在设备的上下文中，提供了部分限定体积的屏障幕。 该装置还包括沿着部分限定体积的一个或多个壁延伸的电缆。 屏障由电缆支撑。 该装置还可以包括连接到相应的壁上的电缆释放机构。 电缆由电缆释放机构承载，并且电缆释放机构构造成在预定负载下失效，从而允许屏障窗响应于减压事件而下降。

Patent Agency Ranking