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    飞机液压系统安全活门供压导管开裂原因

    Reasons for cracking of the pressure supply pipe of the safety valve in the aircraft hydraulic system

    • 摘要: 某飞机液压系统安全活门供压导管发生开裂。采用宏观观察、扫描电镜分析、金相检验、力学性能测试、动应力测试等方法对导管开裂的原因进行分析。结果表明:供压导管的开裂性质为高周疲劳开裂,管路刚度的储备裕度不足,使动应力偏大,最终导致导管发生疲劳开裂。

       

      Abstract: The pressure supply pipe of the safety valve in the hydraulic system of a certain aircraft cracked. The causes of catheter cracking were analyzed using macroscopic observation, scanning electron microscopy analysis, metallographic examination, mechanical property testing, dynamic stress testing. The results show that the cracking property of the pressure supply conduit was high cycle fatigue cracking, and the reserve margin of pipeline stiffness was insufficient, resulted in excessive dynamic stress and ultimately led to fatigue cracking of the pipe.

       

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