The invention provides an aircraft transmission structure, comprising: an input end assembly, the input end assembly comprising an input flange, a main rotor brake adapter and an input shaft connected in sequence, the main rotor brake adapter being arranged between the input flange and the input shaft; the output end assembly comprises an output shaft, a tail rotor brake adapter and an output flange which are connected in sequence, and the tail rotor brake adapter is arranged between the output shaft and the output flange; the joint assembly comprises a clutch connected with the input shaft and the output shaft; the input shaft and the output shaft are rotationally connected with the cartridge receiver assembly, the joint assembly is arranged in the cartridge receiver assembly, and the main rotor brake adapter and the tail rotor brake adapter are arranged on the two sides of the cartridge receiver assembly respectively. Clutch and brake of the aircraft are integrally designed, the transmission efficiency is high, the transmission torque is large, and the response speed is high.
本发明提供一种飞行器传动结构,包括:输入端组件,所述输入端组件包括依次连接的输入法兰、主旋翼刹车转接盘以及输入轴,主旋翼刹车转接盘设于输入法兰和输入轴之间;输出端组件,所述输出端组件包括依次连接的输出轴、尾旋翼刹车转接盘以及输出法兰,尾旋翼刹车转接盘设于输出轴和输出法兰之间;接合组件,所述接合组件包括连接输入轴和输出轴的离合器;机匣组件,所述输入轴和输出轴分别和机匣组件转动连接,接合组件设于机匣组件内部,主旋翼刹车转接盘和尾旋翼刹车转接盘分别设于机匣组件的两侧。本发明将飞行器的离合和刹车集成设计,传动效率高,传递扭矩大,响应速度快。
Aircraft transmission structure
一种飞行器传动结构
2024-03-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft floor longitudinal beam course load transmission structure
European Patent Office | 2020
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