Drawer security attachment
    1.
    发明授权
    Drawer security attachment 失效
    抽屉安全附件

    公开(公告)号:US07547050B1

    公开(公告)日:2009-06-16

    申请号:US11809997

    申请日:2007-06-04

    IPC分类号: E05C19/06 A47B88/00

    摘要: A drawer security attachment includes an attachment flange or brackets and a cover extending from the bracket. The flange or brackets attach to the inner surface of the drawer face, and the cover extends across the width of the otherwise open top of the drawer to inhibit access to the drawer contents. The flange and cover may be a single, monolithic sheet of flexible plastic, or may comprise rigid components secured to one another by a hinge. The cover portion includes a catch engagement passage(s), with a pin(s) extending downwardly from the upper portion of the drawer opening. The panel is urged upwardly against the upper portion of the drawer opening, with the engagement passage(s) automatically catching on the pin(s) as the drawer is opened. The cover can include extendable wings to match an overall width of the cover to the drawer width.

    摘要翻译: 抽屉安全附件包括附接凸缘或支架以及从支架延伸的盖子。 法兰或支架附接到抽屉表面的内表面,盖子延伸穿过抽屉另外打开的顶部的宽度,以禁止进入抽屉内容物。 凸缘和盖可以是单一的柔性塑料片,或者可以包括通过铰链彼此固定的刚性部件。 盖部分包括卡扣接合通道,其中一个销从抽屉开口的上部向下延伸。 面板被推靠在抽屉开口的上部,当抽屉打开时,接合通道自动地卡在销上。 盖子可以包括可伸展的翼片,以将盖子的总宽度与抽屉宽度相匹配。

    Stop armature for aircraft doors
    6.
    发明授权
    Stop armature for aircraft doors 有权
    停止飞机门的电枢

    公开(公告)号:US08240722B2

    公开(公告)日:2012-08-14

    申请号:US12389641

    申请日:2009-02-20

    IPC分类号: E05C19/06

    摘要: The invention relates to a stop armature of an armature system of an aircraft door with a fuselage stop armature (10) and a door stop armature (12, 79), with a stop screw (30; 40; 60) in one of the two stop armatures (10, 12 or 79), which can be pressurized by the other stop armature (10) in the longitudinal direction of the screw (30; 40; 60; 80) on a locating face (34; 52; 70; 88). It is further developed by virtue of the fact that the screw (30; 40; 60; 80) encompasses a screw head (32; 42; 69) with a ball (36; 50; 68; 85) held therein that can rotate around its midpoint (M) as the fulcrum. The invention also relates to a stop screw for a stop armature and the use of a ball thrust screw as the stop screw.

    摘要翻译: 本发明涉及具有机身停止电枢(10)和机门电枢(12,79)的飞行器门的电枢系统的停止电枢,其中两个中的一个中具有止动螺钉(30; 40; 60) 停止电枢(10,12或79),所述电枢可以在所述螺钉(30; 40; 60; 80)的纵向方向上被所述另一停止电枢(10)加压在定位面(34; 52; 70; 88 )。 螺杆(30; 40; 60; 80)包围螺钉头(32; 42; 69)进一步发展,所述螺钉头(32; 42; 69)具有保持在其中的球(36; 50; 68; 85) 其中点(M)为支点。 本发明还涉及用于停止电枢的止动螺钉以及使用球推力螺钉作为止动螺钉。