The invention provides a counterweight device and a counterweight method for an aircraft panel, and belongs to the technical field of aviation. The counterweight device for the aircraft panel comprises a front end frame, a panel, a counterweight platform, a rear end frame, a counterweight box, a box cover, at least one counterweight block and a limiting piece; wherein the counterweight platform is fixedly connected with the front end frame, the wall plate and the rear end frame; the counterweight box is fixedly connected with the counterweight platform; all the balancing weights are located in the weight box, and each balancing weight can be limited through a limiting piece. And the weight box is fixedly connected with the box cover. The device has the advantages of being good in structural stability, convenient to adjust the balance weight, convenient to disassemble and assemble in the later period, high in expansibility and the like, and the problems that an existing balance weight is inconvenient to adjust and large in local stress can be solved.
本发明提供一种用于飞机壁板的配重装置及配重方法,属于航空技术领域,该用于飞机壁板的配重装置包括:前端框,壁板,配重平台,后端框,配重箱,箱盖,至少一个配重块,以及限位件;其中,配重平台与前端框,壁板,后端框固定连接;配重箱与配重平台固定连接;所有配重块位于配重箱内,每个配重块可通过限位件完成限位;配重箱和箱盖固定连接。本发明具有结构稳定性好,配重调整方便,后期拆装方便,拓展性强等特点,能解决现有配重调整不便,局部受力较大等问题。
Counterweight device and counterweight method for aircraft panel
一种用于飞机壁板的配重装置及配重方法
2025-01-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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