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17 条记录 (耗时 0.018 秒)

    PORTABLE LIGHT HAVING A ROTATABLE HEAD
    11.
    发明申请
    PORTABLE LIGHT HAVING A ROTATABLE HEAD 有权
    便宜的灯具有可旋转的头

    公开(公告)号：US20120033415A1

    公开(公告)日：2012-02-09

    申请号：US13023010

    申请日：2011-02-08

    申请人： Raymond L. Sharrah ,  Donald J. Keeley ,  Matthew B. Dalton

    发明人： Raymond L. Sharrah ,  Donald J. Keeley ,  Matthew B. Dalton

    IPC分类号： F21L4/04

    CPC分类号： F21V21/08 ,  F21L4/027 ,  F21L4/04 ,  F21V7/0075 ,  F21V21/0885 ,  F21V21/0965 ,  F21V29/70 ,  F21V29/83 ,  F21V29/89 ,  F21Y2115/10

    摘要： A portable light may comprise a light body and a light head rotatable relative to the light body. The light head may comprise a light source that may be pivotable relative to a base of the light head. The light source may be electrically connected to the light body by rotatable coaxial connections between the light head and the light body and by rotatable coaxial electrical connections between the base of the light head and the light source. The light may optionally further comprise a hanger movable relative to the light body, or may comprise one or more magnets on the light body, or may comprise a clip on the light body, or a combination thereof.

    摘要翻译： 便携式光可以包括光体和可相对于光体旋转的光头。 光头可以包括相对于光头的基部可枢转的光源。 光源可以通过光头和光体之间的可旋转的同轴连接和光头的基座与光源之间的可旋转的同轴电连接而与灯体电连接。 光可以可选地进一步包括可相对于灯体移动的吊架，或者可以包括在灯体上的一个或多个磁体，或者可以包括在灯体上的夹子或其组合。

    Battery cell bypass switch
    14.
    发明授权
    Battery cell bypass switch 有权
    电池单元旁路开关

    公开(公告)号：US06093896A

    公开(公告)日：2000-07-25

    申请号：US286579

    申请日：1999-04-05

    申请人： Jui-Yu Wu ,  Matthew B. Dalton

    发明人： Jui-Yu Wu ,  Matthew B. Dalton

    IPC分类号： H01H71/20 ,  H01H79/00 ,  H01H35/00 ,  H01H37/74 ,  H01M14/00

    CPC分类号： H01H79/00 ,  H01H71/20

    摘要： A system (10) for establishing bypass of a failed battery cell (18) includes a failed cell sensor (26) which on sensing a failed cell generates an electric signal that destroys clamping relation of two retaining wire spools (24) to release retaining means (14,16). Such release enables a unitary plunger assembly (28) to be moved by a spring (49) to position a cylindrical pin contact (52) in electrical shorting relation to the first and second electrodes (57,58) connected across the cell (18).

    摘要翻译： 用于建立故障电池单元（18）的旁路的系统（10）包括故障单元传感器（26），其在感测到故障单元时产生电信号，该电信号破坏两个保持线芯（24）的夹紧关系，以释放保持装置 （14,16）。 这种释放使得整体式柱塞组件（28）能够通过弹簧（49）移动以将圆柱形销触点（52）定位成与穿过电池（18）连接的第一和第二电极（57,58）处于电短路关系， 。

    Resettable and redundant NEA-initiated hold-down and release mechanism for a flight termination system
    17.
    发明授权
    Resettable and redundant NEA-initiated hold-down and release mechanism for a flight termination system 有权
    NEA启动的可复位和冗余的启停和释放机制

    公开(公告)号：US06679177B1

    公开(公告)日：2004-01-20

    申请号：US10131903

    申请日：2002-04-24

    申请人： Jui-Yu Wu ,  Matthew B. Dalton ,  John D. Kisch

    发明人： Jui-Yu Wu ,  Matthew B. Dalton ,  John D. Kisch

    IPC分类号： F42B1510

    CPC分类号： F42B15/36 ,  Y10T403/581

    摘要： A hold-down and release apparatus for a flight termination system having a terminal portion for holding-down and releasing a structural object which has an arrangement for attaching to the flight termination system. The hold-down and release apparatus includes several movable clamping segments provided on the terminal portion of the flight termination system that are engageable in a complimentary fashion with the attachment arrangement on the structural object for releasably attaching the structural object to the flight termination system. The hold-down and release apparatus also includes springs for biasing the movable clamping segments means in a disengaging direction that causes the clamping segments to disengage from the attachment arrangement on the structural object to release the structural object from the flight termination system. The hold-down and release apparatus further includes a release band attached to the movable clamping segments for preventing the disengaging movement of the movable clamping segments such that they remain engaged to the attachment arrangement of the structural object for releasably attaching the structural object to the flight termination system. The release band is held in position by two non-explosive actuators (NEAs), such that either one or both actuators may initiate the release and loosen the release band which allows the movable clamping segments to move under the urge of the biasing, springs to disengage the complimentary attachment arrangement from the attachment arrangement of the structural object, to release the structural object from the flight termination system.

    摘要翻译： 一种用于飞行终点系统的按压和释放装置，具有用于按压和释放具有用于附接到飞行终点系统的装置的结构物体的终端部分。 压紧和释放装置包括设置在飞行终端系统的终端部分上的多个可移动的夹紧段，其能够以与结构物体上的附接装置互补的方式接合，以将结构物体可释放地附接到飞行终点系统。 压紧和释放装置还包括弹簧，用于使分离方向偏置可动夹紧段装置，使得夹紧段与结构物体上的附接装置分离，以将结构物体从飞行终端系统释放。 压紧和释放装置还包括附接到可动夹紧段的释放带，用于防止可动夹紧段的分离运动，使得它们保持接合到结构物体的附接装置，以将结构物件可释放地附接到飞行 终止系统。 释放带由两个非爆炸致动器（NEAs）保持就位，使得一个或两个致动器可以启动释放并松开释放带，其允许可动夹紧段在偏压的推动下移动，弹簧到 将互补的附接装置与结构物体的附接装置分离，以将结构物体从飞行终点系统释放。