Thrust reversing cascade assembly
    1.
    发明授权
    Thrust reversing cascade assembly 失效
    扭转CASCADE装配

    公开(公告)号:US3794246A

    公开(公告)日:1974-02-26

    申请号:US3794246D

    申请日:1973-04-11

    申请人: AERONCA INC

    发明人: WEISE C

    IPC分类号: F02K1/56 F02K1/20 B64C15/06

    CPC分类号: F02K1/56 Y02T50/671

    摘要: A lightweight, easily manufactured and assembled thrust reversing cascade assembly for jet engines. The assembly includes a plurality of turning vanes positioned in spaced relation and locatable aft of a jet engine exhaust. Each turning vane is rigidly supported in fixed spacial relation to other such turning vanes by a support assembly which includes a plurality of planar spacer members. Each spacer member includes a tab portion which extends from the spacer body a distance sufficient to pass through a slot in a turning vane. Each spacer also includes a notch on the end opposite the tab to receive the tab projecting through a turning vane from another spacer member. A pair of straps are positioned on both sides of the planar spacer members and also extend through the slots in each turning vane. Tensioning means is provided at opposite ends of the straps to place the straps in tension while providing compression forces on the spacers and turning vanes to rigidly support the turning vanes in spaced relation.

    摘要翻译: 轻型,易于制造和组装的用于喷气发动机的推力反向级联组件。 组件包括多个转动叶片,该转动叶片以喷气发动机排气的间隔关系和可定位的后部定位。 每个转动叶片通过包括多个平面间隔件的支撑组件与其它这样的转动叶片以固定的空间关系被刚性地支撑。 每个间隔件包括一个突片部分,其从间隔件主体延伸出足以穿过转动叶片中的狭槽的距离。 每个间隔件还包括在与突片相对的端部上的凹口,以接收通过来自另一隔离构件的转动叶片突出的突出部。 一对带子定位在平面间隔件的两侧,并且还延伸穿过每个转动叶片中的狭槽。 张紧装置设置在带的相对端处,以使带子处于张紧状态,同时在间隔件和转动叶片上提供压缩力,以间隔的关系刚性地支撑转动叶片。