摘要
介绍了某型航天飞行器舵机系统传动装置中的双输入行星减速器,通过考虑齿厚偏差、中心距偏差和轴承径向游隙对回差的影响,定量分析了双输入行星减速器的回差,给出其空程回差的计算表达式。根据回差分析,采用了配凑中心距的方法控制样机回差精度,并对样机进行回差测试,实验结果与预期一致。
A certain type of two- input planetary gear of spacecraft steering gear system is described. By considering the influence of tooth thickness deviation,central distance deviation and bearing radial clearance on the backlash,the quantitative analysis of the two- input planetary gear return difference is carried out,the calculation expression of its return difference is given. According to the return difference analysis,by using the method with matching center distance to control return difference precision of prototype,through the test of prototype return difference,the experimental results are consistent with expectation.
出处
《机械传动》
CSCD
北大核心
2016年第1期132-135,共4页
Journal of Mechanical Transmission
关键词
双输入行星减速器
空程回差
样机测试
Two-input planetary gear reducer
Idle stroke return difference
Prototype test