Structural Panels for Use in Aircraft Fuselages and Other Structures
    1.
    发明申请
    Structural Panels for Use in Aircraft Fuselages and Other Structures 有权
    用于飞机机身和其他结构的结构面板

    公开(公告)号:US20100223772A1

    公开(公告)日:2010-09-09

    申请号:US12762129

    申请日:2010-04-16

    Abstract: Structural panels for use in manufacturing aircraft fuselages and other structures are disclosed herein. In one embodiment, a structural panel configured in accordance with the invention includes a skin and at least first and second stiffeners. The first stiffener can have a first flange portion mated to the skin and a first raised portion projecting away from the skin. The second stiffener can have a second flange portion mated to the skin and a second raised portion projecting away from the skin. At least one of the first flange portion of the first stiffener and the second flange portion of the second stiffener can extend toward the other of the first flange portion and the second flange portion to form an at least approximately continuous support surface to which a frame can be attached.

    Abstract translation: 本文公开了用于制造飞机机身和其它结构的结构面板。 在一个实施例中,根据本发明构造的结构面板包括皮肤和至少第一和第二加强筋。 第一加强件可以具有与皮肤配合的第一凸缘部分和远离皮肤突出的第一凸起部分。 第二加强件可以具有与皮肤配合的第二凸缘部分和远离皮肤突出的第二凸起部分。 第一加强件的第一凸缘部分和第二加强件的第二凸缘部分中的至少一个可以朝向第一凸缘部分和第二凸缘部分中的另一个延伸,以形成至少近似连续的支撑表面,框架可向该支撑表面 被附上

    METHODS OF MANUFACTURING STRUCTURAL PANELS
    2.
    发明申请
    METHODS OF MANUFACTURING STRUCTURAL PANELS 有权
    制造结构面板的方法

    公开(公告)号:US20100083504A1

    公开(公告)日:2010-04-08

    申请号:US11522184

    申请日:2006-09-14

    Abstract: Structural panels for use in manufacturing aircraft fuselages and other structures are disclosed herein. In one embodiment, a structural panel configured in accordance with the invention includes a skin and at least first and second stiffeners. The first stiffener can have a first flange portion mated to the skin and a first raised portion projecting away from the skin. The second stiffener can have a second flange portion mated to the skin and a second raised portion projecting away from the skin. At least one of the first flange portion of the first stiffener and the second flange portion of the second stiffener can extend toward the other of the first flange portion and the second flange portion to form an at least approximately continuous support surface to which a frame can be attached.

    Abstract translation: 本文公开了用于制造飞机机身和其它结构的结构面板。 在一个实施例中,根据本发明构造的结构面板包括皮肤和至少第一和第二加强筋。 第一加强件可以具有与皮肤配合的第一凸缘部分和远离皮肤突出的第一凸起部分。 第二加强件可以具有与皮肤配合的第二凸缘部分和远离皮肤突出的第二凸起部分。 第一加强件的第一凸缘部分和第二加强件的第二凸缘部分中的至少一个可以朝向第一凸缘部分和第二凸缘部分中的另一个延伸,以形成至少近似连续的支撑表面,框架可向该支撑表面 被附上

    Dual pump assembly
    7.
    发明授权
    Dual pump assembly 有权
    双泵总成

    公开(公告)号:US07695250B2

    公开(公告)日:2010-04-13

    申请号:US11265776

    申请日:2005-11-02

    CPC classification number: F04C11/00

    Abstract: The apparatus of the present invention provides a compact dual-pump assembly for an automotive transmission. The dual-pump assembly preferably includes a housing having a valve assembly mounted thereto. The valve assembly includes a shuttle valve disposed in fluid communication with a pressure regulating valve. An on-axis pump is mounted to the housing in fluid communication with the shuttle valve and the pressure regulating valve. An off-axis pump in fluid communication with the shuttle valve is mounted to the housing in close proximity to the on-axis pump such that the dual-pump assembly is compact.

    Abstract translation: 本发明的装置提供了一种用于汽车变速箱的紧凑型双泵组件。 双泵组件优选地包括具有安装到其上的阀组件的壳体。 阀组件包括与压力调节阀流体连通的梭阀。 轴上泵安装到壳体上,与梭阀和调压阀流体连通。 与梭阀流体连通的离轴泵安装在紧邻轴上泵的壳体上,使得双泵组件紧凑。

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