Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Detecting Location and Depth of Cracks in Rotor using Critical Speed

임계속도를 이용한 로터의 결함 위치와 크기 판별

  • Published : 2006.05.31
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Abstract

Structural health monitoring has been conducted by non-destructive evaluation method when a turbine rotor system of an aircraft engine has cracks. Local stiffness of a turbine rotor system is degraded and critical speed is changed due to the presence of cracks in rotor. Critical speed which is affected by location and depth of crack, is obtained using compliance matrix of cracked rotor. The database of the obtained critical speed is used to evaluate structural health monitoring of a rotor system of a gas turbine engine.

항공기의 가스터빈 엔진에서 축에 결함이 있을 경우에 대한 건전성 평가를 비파괴방법으로 접근했다. 로터의 축에 결함이 있을 경우에는 국지적으로 강성이 약화되어 임계속도가 달라진다. 결함이 있는 축의 순응도(compliance)행렬을 이용해서 각각의 결함의 위치와 깊이에 따른 임계속도를 구하고 이러한 결과들을 이용해 역 문제에 대한 자료를 구축함으로써 엔진 축의 건전성 평가를 수행하였다.

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References

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