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    Luggage Compartment Actuation
    1.
    发明申请
    Luggage Compartment Actuation 有权
    行李箱动作

    公开(公告)号：US20080295407A1

    公开(公告)日：2008-12-04

    申请号：US11630308

    申请日：2005-06-14

    Applicant: Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

    Inventor： Olaf Von Wieding ,  Lars Rowold ,  Bodo Wisch ,  Bruno Alquier

    IPC: B64D11/00 ,  E05F15/00 ,  G01R27/26

    CPC classification number: G05G15/08 ,  B64D11/003

    Abstract: This device is provided for a luggage compartment designed to be placed overhead. The compartment comprises a mobile part (4) between an open position and a closed position and a mechanism for acting on said mobile part (4) to promote its closing. Said mobile part (4) presents an opening (14) designed for introducing and retrieving luggage as well as a lower exterior surface (12). The control device comprises detection means reacting when pressure is exerted on a predetermined zone of the lower exterior surface (12) of the mobile part (4) as well as for sending a control signal to the mechanism acting on the mobile part (4) to close the part when pressure is exerted on said detection means. The detection means are disposed at the lower exterior surface (12) of the mobile part (4).

    Abstract translation: 该设备提供用于设置在顶部的行李舱。 隔间包括在打开位置和关闭位置之间的可移动部件（4）和用于作用在所述移动部件（4）上以促进其关闭的机构。 所述移动部件（4）具有用于引入和取回行李以及下部外表面（12）的开口（14）。 控制装置包括当压力施加在可移动部件（4）的下部外表面（12）的预定区域上并且用于向作用在移动部件（4）上的机构发送控制信号时响应的检测装置 当对所述检测装置施加压力时，关闭该部件。 检测装置设置在移动部件（4）的下外表面（12）处。

    Externally accessible, clutching adjustable keeper mechanism
    2.
    发明授权
    Externally accessible, clutching adjustable keeper mechanism 失效
    外部可接近的，可调节的保持机构

    公开(公告)号：US4906037A

    公开(公告)日：1990-03-06

    申请号：US325084

    申请日：1989-03-17

    Applicant: John C. Stammreich ,  William Bourne, Jr. ,  Raymond Harmon

    Inventor： John C. Stammreich ,  William Bourne, Jr. ,  Raymond Harmon

    IPC: F16B31/02 ,  F16D7/04 ,  F16H35/10 ,  G05G15/08

    CPC classification number: G05G15/08 ,  F16B31/02 ,  F16D7/044 ,  F16H35/10 ,  Y10S292/60 ,  Y10T292/705 ,  Y10T74/2101

    Abstract: An externally accessible, clutching adjustable latching mechanism is provided having an adjusting assembly which permits the latching mechanism to be mounted over a greater range of depths than conventional adjusting mechanisms and controls the amount of pre-load which is possible by the adjustment feature, and protects the aircraft skin from being damaged during such adjustment. An internal clutching mechanism insures the accomplishment of proper, minimum preload on the structures connected by the latching mechanism. The adjusting assembly includes a two-part driver (14a, 14b) and a drive unit (15) which translates rotational movement of the driver into linear movement of a connecting element (10), allowing infinitely small, non-incremental adjustment of the position of the connecting element (10) relative to the structures joined by the mechanism. The driver further includes clutching plates (36, 39) and springs (72) which provide a disengaging feature when a pre-selected pre-load has been achieved as a result of adjustment of the connecting element. The disengagement prevents any additional pre-load from being applied to the structures by the rotation of the mechanism.

    Abstract translation: 提供了一种外部可接近的离合可调闭锁机构，其具有调节组件，该调节组件允许闭锁机构安装在比常规调节机构更大的深度范围内，并且通过调节特征来控制可能的预负荷量，并保护 飞机皮肤在这种调整过程中被损坏。 内部的夹紧机构确保在通过闩锁机构连接的结构上实现适当的最小预载荷。 调节组件包括两部分驱动器（14a，14b）和驱动单元（15），该驱动单元将驱动器的旋转运动转换成连接元件（10）的线性运动，允许无限小的非增量调节位置 的连接元件（10）相对于通过机构连接的结构。 驱动器还包括当由于连接元件的调节而实现了预先选择的预加载时提供脱离特征的离合板（36,39）和弹簧（72）。 分离防止通过机构的旋转而将任何额外的预加载施加到结构上。

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