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    某型飞机疲劳试验中的损伤特点分析

    Analysis of Damage Characteristics in Fatigue Testing of a Aircraft

    • 摘要: 对某型民用飞机全机疲劳试验中,通过实施无损检测而发现的损伤,从损伤类型、损伤出现部位及部分裂纹的扩展进行分析,总结了该飞机的结构薄弱部位及危险裂纹扩展规律,为此类飞机无损检测检测及维修提供一定的参考依据。

       

      Abstract: Based on the damages detected by nondestructive testing(NDT) in full-scale civil aircraft structure fatigue test, the types, locations and propagation of the damage are analyzed. Through these the weak area of aircraft structure, and the dangerous crack growth behavior are pointed out. It can provide some references for the NDT and maintenance of such aircraft.

       

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