The invention relates to a small-space airborne hanging object launching mechanism which comprises a fixed sliding rail, a fixed sliding rail, a fixed sliding rail, a movable sliding rail and a movable sliding rail. The hanging object support is arranged at the front end of the fixed sliding rail, a sliding block is arranged on the hanging object support, the sliding block is matched with the first sliding groove, and the hanging object support is arranged in the first sliding groove through the sliding block and connected with the fixed sliding rail; the folding mechanism comprises a rocker arm arranged on the front side of the hanger bracket, and the front end of the rocker arm is hinged with the fuselage; the movable slide rail is arranged at the front end of the hanger bracket, and the side surface is hinged with the rear end of the rocker arm; a second sliding groove matched with the sliding block is formed in the movable sliding rail. The bottom face of the sliding block, the top face of the first sliding groove and the top face of the second sliding groove are obliquely arranged in the downward inclining direction from back to front edge. The locking mechanism is arranged at the front end of the hanger support and used for limiting the sliding block to slide forwards along the first sliding groove and the second sliding groove. The device is simple in structure and convenient to operate, and can be used for reducing the space size of an airborne mounting launching device and reducing the limitation on a mounted object.

    本发明涉及一种小空间机载悬挂物发射机构,包括:定滑轨,其上端与机身固定,其侧面上设有第一滑槽;悬挂物支架设置在定滑轨的前端,悬挂物支架上设有滑块,滑块与第一滑槽相适配,悬挂物支架通过滑块设置在第一滑槽内,与定滑轨连接;折叠机构包括摇臂,摇臂设置在悬挂物支架的前侧,其前端与机身铰接;动滑轨设置在悬挂物支架的前端,其侧面与摇臂的后端铰接;动滑轨上设有与滑块相适配的第二滑槽,滑块的底面、第一滑槽及第二滑槽的顶面自后向前沿向下倾斜的方向倾斜设置;锁定机构设置在悬挂物支架的前端,用于限制滑块沿第一滑槽和第二滑槽向前滑动。本发明结构简单,操作方便,可用于缩小机载挂载发射装置的空间尺寸,减小对挂载物的限制。


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    Titel :

    Small-space airborne suspension launching mechanism


    Weitere Titelangaben:

    小空间机载悬挂物发射机构


    Beteiligte:
    REN KUN (Autor:in) / ZHANG ZHIXIAN (Autor:in) / QIAO YUHANG (Autor:in) / A RONG (Autor:in) / ZHANG YUJIA (Autor:in)

    Erscheinungsdatum :

    2024-01-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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