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    小型航空发动机叶片的原位涡流检测

    In-situ eddy current testing of one mini-aeroengine blades

    • 摘要: 针对某小型航空发动机动力涡轮转子叶片上产生的疲劳裂纹,采用涡流检测的方法对其进行原位检测,但现有的涡流检测探头在结构和性能方面均无法满足动力涡轮转子叶片原位检测的需求。为此,研制了一种专用涡流探头,并通过厂内试验和外场原位检测应用,验证该探头的检测可靠性和有效性。试验结果表明,所提检测方法与研制的探头在厂内试验中成功检出人工刻槽,外场应用中能检出真实疲劳裂纹,与金相检验结果吻合,基本满足涡轮转子叶片的原位检测需求。

       

      Abstract: Aiming at the fatigue cracks generated on the power turbine rotor blades of a certain small aero-engine, the eddy current testing method was used for in-situ inspection. However, the existing eddy current testing probes could not meet the requirements for in-situ inspection of power turbine rotor blades in terms of structure and performance. Therefore, a specialized eddy current probe was developed. Through in-factory tests and field in-situ inspection applications, the detection reliability and effectiveness of the developed specialized eddy current probe were verified. Test results showed that the proposed detection method and developed probe successfully detected artificial notches in the in-factory tests and could detect real fatigue cracks in field applications, which were consistent with metallographic examination results, basically meeting the in-situ inspection needs of power turbine rotor blades.

       

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