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Failure analysis of gas turbine blades in a thermal power plant

机译:火力发电厂燃气轮机叶片的故障分析

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A case study of failure analysis of a 40 MW gas turbine blade made of Udimet 500 is presented. The cause of failure is found to be intergranular cracks which started during exposure to high temperature. The cracks initiated from the grain boundaries and propagated to the critical length to result in catastrophic fracture. In many locations M_6C type secondary carbides were found agglomerated on grain boundaries. Also micro-cavities were found on fracture surfaces which served as an origin of creeping failure mechanism.
机译:介绍了一个由Udimet 500制成的40 MW燃气轮机叶片故障分析的案例研究。发现失败的原因是在暴露于高温期间开始的晶间裂纹。裂纹从晶界开始并扩展到临界长度,导致灾难性的断裂。在许多位置,发现M_6C型二次碳化物在晶界聚集。在断裂表面上还发现了微腔,这是蠕变破坏机理的起源。

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