• Title/Summary/Keyword: Nanofractography

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A Study on Failure Analysis of Low Pressure Turbine Blade Subject to Fatigue Load (피로하중을 받은 저압 터빈 블레이드의 파손해석에 관한 연구)

  • 홍순혁;이동우;조석수;주원식
    • Journal of Welding and Joining
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    • v.19 no.3
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    • pp.298-304
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    • 2001
  • Turbine blade is subject to force of three types ; the torsional force by torsional mount, the centrifugal force by the rotation of rotor and the cyclic bending force by steam pressure. The cyclic bending force was a main factor on fatigue strength. SEM fractography in root of turbine blade showed micro-clack width was not dependent on stress intensity factor range. Especially, fatigue did not exist on SEM photograph in root of turbine blade. To clear out the fracture mechanism of turbine blade, nanofractography was needed on 3-dimensional crack initiation and crack growth with high magnification. Fatigue striation partially existed on AFM photograph in root of turbine blade. Therefore, to find a fracture mechanism of the torsion-mounted blade in nuclear power plant, the relation between stress intensity factor range and surface roughness measured by AFM was estimated, and then the load amplitude ΔP applied to turbine blade was predicted exactly by root mean square roughness.

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A Study on Failure Analysis of Low Pressure Turbine Blade in Nuclear Plant using AFM (AFM을 이용한 발전소용 저압 터빈 블레이드의 파손해석에 관한 연구)

  • Hong, Soon-Hyeok;Choi, Woo-Sung;Moon, Sung-Jun;Cho, Seok-Swoo;Joo, Won-Sik
    • Journal of the Korean Society for Precision Engineering
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    • v.18 no.10
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    • pp.61-68
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    • 2001
  • Turbine blade in nuclear plant is subject to cyclic bending fatigue by high steam pressure. Especially, fatigue fracture is caused by low stress below yielding stress. Photograph by SEM doesn't have striation but photograph by AFM has striation on the fatigue fractured surface of 12% Cr steel used in turbine blade. Surface roughness $R_q$ has the linear relation with respect to stress intensity factor range ΔK and is increased linearly according to load amplitude $\textit{\Delta}P$. In this study loading condition applied to turbine blade is predicted by the relation between the gradient of $R_q$ to $\textit{\Delta}K$ and load amplitude $\textit{\Delta}P$.

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