The invention provides a device for erecting and overturning an aircraft. The device comprises a gantry type lifting arm, a hanging assembly, an erecting driving and adjusting assembly and an erecting telescopic assembly. The hanging assembly is connected to the gantry type lifting arm and used for hanging and lifting the gantry type lifting arm. The erecting driving adjusting assembly is used for being connected to a corresponding connecting point of the aircraft body and driving the aircraft body to rotate in the Z direction so as to adjust the erecting posture of the aircraft body. One end of the erecting telescopic assembly is connected to the erecting drive adjusting assembly, and the other end of the erecting telescopic assembly is connected to the gantry type suspension arm and used for buffering the impact of the dead weight of the device on the aircraft body. According to the device for erecting and overturning the aircraft, the erecting posture of the aircraft can be adjusted, and the weight and the gravity center of the aircraft can be measured.
本发明提供了一种用于飞行器起竖翻转的装置,包括龙门式吊臂、吊挂组件、起竖驱动调整组件以及起竖伸缩组件;吊挂组件连接于龙门式吊臂,用于悬挂吊起龙门式吊臂;起竖驱动调整组件用于连接于飞行器机机体的对应连接点,并驱动飞行器机体沿Z向转动,以调整飞行器机体的起竖位姿;起竖伸缩组件的一端连接于起竖驱动调整组件,起竖伸缩组件的另一端连接于龙门式吊臂,用于缓冲装置自重对飞行器机机体的冲击。本发明提供的用于飞行器起竖翻转的装置能实现飞行器起竖姿态的调整、以及实现对飞行器的重量和重心的测量。
Device for erecting and overturning aircraft
用于飞行器起竖翻转的装置
2025-02-14
Patent
Electronic Resource
Chinese
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