The invention relates to the technical field of aircrafts, in particular to a mounting assembly for an empennage of an aircraft, comprising: a connecting assembly comprising a connecting hole and a connecting pin; the limiting assembly comprises a limiting screw rod, an inserting groove, a threaded sleeve and a non-return assembly; and the pre-tightening assembly is connected with the threaded sleeve and the non-return assembly, and when the threaded sleeve rotates, the pre-tightening assembly can be driven to move to apply pre-tightening force to the non-return assembly. In the whole using process, a limiting screw rod and a connecting pin only need to be inserted into an inserting groove and a connecting hole correspondingly, then fixation can be automatically kept under the action of a limiting assembly and a pre-tightening assembly, and a user only needs to hold a fuselage and an empennage mounting part of the aircraft with the two hands to conduct opposite insertion operation; the three parts do not need to be operated by two hands at the same time, the operation process is greatly simplified, and use is more convenient.
本发明涉及飞行器技术领域,特别是涉及一种用于飞行器尾翼的安装组件,包括:连接组件,连接组件包括连接孔和连接销;限位组件,限位组件包括限位螺杆、插槽、螺纹套以及止回组件;预紧组件,预紧组件与螺纹套、止回组件连接,且螺纹套转动时可驱动预紧组件运动来对止回组件施加预紧力。本发明,在整个使用过程中,只需将限位螺杆、连接销分别插入插槽和连接孔,之后便会在限位组件以及预紧组件的作用下自动保持固定,使用者只需双手分别拿住飞行器的机身和尾翼安装部进行对插操作即可,不需要在两只手同时操作三个部件,大大简化了操作流程,使用起来更加方便。
Mounting assembly for empennage of aircraft
一种用于飞行器尾翼的安装组件
2025-04-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Mounting assembly for aircraft empennage and aircraft empennage
European Patent Office | 2024
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