When this method is applied to the spiral bevel gears of an airplane engine, the results show that it is more reasonable than TCA and the precontrol method.

提出了一种在初始段就可保证弧齿锥齿轮具有预期载接触性能的主动方法，并将某航空发动机中央传动弧齿锥齿轮的齿面综合。