摘要
强5飞机减摆器是防止前轮摆振的关键构件。本文用疲劳断裂理论估算该构件的安全寿命和裂纹扩展寿命，并提出维修及设计改进建议。
The shimmy damper of A5 aircraft is a critical component used to prevent the nose wheel from shimmying This paper estimates the safety life and fracture extension life of the component with the fatigue fracture theory, and puts forward recommendations for the maintenance and design improvement.
出处
《洪都科技》
1995年第4期20-23,共4页
Hongdu Science and Technology
关键词
飞机减摆器
疲劳断裂
安全寿命
强击机
Aircraft Shimmy
Damper Fatigue Fracture
Theory Safety Life
