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method for detecting a crack of turbomachinery blades and systems

机译:涡轮机叶片裂纹的检测方法及系统

摘要

PROBLEM TO BE SOLVED: To detect a potential crack during operation of a turbomachine.;SOLUTION: A method of detecting a potential crack on a blade of a compressor section of the turbomachine provides real-time monitoring of the compressor section 105 to determine the possibility of a crack forming on the blade 110, 115. The present invention does not require the shutdown of the machine 100. The present invention is configured to automatically raise an alarm if an acoustic signature of the compressor section 105 changes in way that may be consistent with the cracking of the blade 110, 115.;COPYRIGHT: (C)2011,JPO&INPIT
机译:解决的问题:在涡轮机的运行过程中检测潜在的裂纹;解决方案:检测涡轮机的压缩机部分的叶片上的潜在裂纹的方法提供了对压缩机部分105的实时监控,以确定可能性在叶片110、115上形成裂纹的情况。本发明不需要关闭机器100。本发明被配置为如果压缩机部分105的声学特征以可能一致的方式改变,则自动发出警报。刀片110、115破裂。;版权所有:(C)2011,日本特许厅&INPIT

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