The invention relates to the technical field of aviation technologies, in particular to a self-locking structure for double-motor parallel driving and a steering engine. The self-locking structure for double-motor parallel driving comprises a base, a first motor and a second motor which are arranged on the base, and further comprises a first oscillating tooth assembly, a second oscillating tooth assembly and an output gear. The first oscillating tooth assembly is arranged at the driving end of the first motor, the second oscillating tooth assembly is arranged at the driving end of the second motor, the first oscillating tooth assembly and/or the second oscillating tooth assembly are/is used for driving the output gear to rotate, and the self-locking structure can improve the reliability of the steering engine under the condition that redundant electric control is not added and more failure assemblies are not introduced.
本发明涉及航空技术的技术领域,具体涉及一种用于双电机并联驱动的自锁结构及舵机。其中,一种用于双电机并联驱动的自锁结构包括基座以及设置于基座上的第一电机和第二电机,还包括:第一活齿组件、第二活齿组件和输出齿轮;第一活齿组件设置于第一电机的驱动端上,第二活齿组件设置于第二电机的驱动端上,第一活齿组件和/或第二活齿组件用于驱动输出齿轮转动,该自锁结构能够在不增加多余的电控及引入引入更多失效组件的情况下,提升舵机的可靠性。
Self-locking structure for double-motor parallel driving and steering engine
一种用于双电机并联驱动的自锁结构及舵机
2025-01-07
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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