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飞机操纵机构设计中经常采用三角摇臂结构形式的传力构件,其作用是改变操纵力传力方向,保证操纵机构正常工作。这种结构形式的部件对其疲劳性能要求高,需满足机体寿命指标。
The design of aircraft control mechanism often adopts the structure of the triangular rocker arm transmission force component, its role is to change the direction of force transmission force to ensure the normal operation of the control mechanism. This form of structural components of its fatigue performance requirements, to meet the body life index.