The invention discloses a multi-mode airplane all-electric braking device, which relates to the technical field of aviation braking, and comprises a shell, a self-locking motor, a braking assembly, a transmission assembly and an unlocking assembly, the self-locking motor is arranged in the shell and is used for providing power required by braking; the brake assembly is arranged in the shell, can move in the shell and is used for pressing a brake disc of the airplane wheel to generate brake; the transmission assembly is connected with the output end of the self-locking motor and the brake assembly and used for transmitting power generated by the self-locking motor; and the unlocking assembly is arranged in the brake assembly and used for releasing the pressure generated by the brake assembly in emergency. Through the arrangement, the braking efficiency and safety of the braking device are improved.
本发明公开了一种多模式飞机全电刹车制动装置,涉及航空制动技术领域,包括:壳体、自锁电机、制动组件、传动组件和解锁组件;自锁电机,设于壳体内部,用于提供制动所需动力;制动组件,设于壳体内部,且能够在壳体内移动用于压紧机轮的刹车盘产生制动;传动组件,连接自锁电机的输出端和制动组件,用于传递自锁电机所产生的动力;解锁组件,设于制动组件内部,用于应急释放制动组件所产生的压力。如此设置,提高了制动装置的制动效率以及安全性。
Multi-mode airplane all-electric brake device
一种多模式飞机全电刹车制动装置
2024-03-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Engineering Index Backfile | 1939
|Airplane wheel brake control valve group and airplane brake system
European Patent Office | 2024
|NTIS | 1978
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