According to the anti-swing structure and the anti-swing method of the airborne suspension object, the airborne suspension object is installed below an aircraft hanging frame through a hook, the hook is installed on a wall plate of the hanging frame, the anti-swing structure is installed between the aircraft hanging frame and the suspension object, and the anti-swing structure comprises a torsional spring, a pressing rod and a positioning block; the upper end of the pressing rod is installed between wall plates on the two sides of an aircraft pylon through a rotating shaft, the torsion spring is arranged between the pressing rod and the wall plates of the aircraft pylon, the positioning block is of a flat plate structure, a connecting lug is arranged in the middle of the upper end of the positioning block, the connecting lug of the positioning block is hinged to the lower end of the pressing rod through a connecting shaft, and the connecting shaft is parallel to the rotating shaft. And the lower surface of the positioning block corresponds to the surface of the hanging object in shape.
一种机载悬挂物的防摆结构及防摆方法,机载悬挂物通过挂钩安装在飞机挂架的下方,挂钩安装在挂架的壁板上,防摆结构安装在飞机挂架和悬挂物之间,防摆结构含有扭簧、压杆和定位块,所述的压杆的上端通过转轴安装在飞机挂架的两侧壁板之间,扭簧设在压杆与飞机挂架的壁板之间,所述的定位块为平板结构,其上端中部设有连接耳片,定位块的连接耳片通过连接轴与压杆的下端铰接,所述的连接轴和转轴相互平行,定位块的下表面与悬挂物的表面形状对应。
Anti-swing structure and anti-swing method for airborne suspender
一种机载悬挂物的防摆结构及防摆方法
2024-09-17
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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