The invention provides an aircraft gravity center solid-state adjusting device which comprises a guide rail fixedly connected with an aircraft structure, and continuous racks are integrated on the guide rail; the sliding mechanism is installed on the guide rail, and the sliding mechanism can move in the first direction of the guide rail; the limiting device is used for limiting the sliding mechanism to move in the second direction, and the first direction is different from the second direction; meanwhile, the invention further provides an aircraft gravity center solid-state adjusting method. By means of the device and method, the gravity center of the aircraft can be adjusted with high efficiency.
本申请提供了一种飞行器重心固态调节装置,所述调节装置包括:导轨,与飞行器结构固定连接,所述导轨上集成有连续的齿条;滑动机构,安装于所述导轨上,所述滑动机构能够沿所述导轨的第一方向移动;限位装置,用于限制滑动机构沿第二方向运动,所述第一方向与所述第二方向不同;同时,本申请还提供了一种飞行器重心固态调节方法;本发明所述装置与方法能够以较高的效率实现飞行器重心的调节。
Solid-state adjusting device and method for gravity center of aircraft
一种飞行器重心固态调节装置和方法
01.03.2024
Patent
Elektronische Ressource
Chinesisch
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