Eddy Current Testing Method for Rotor Blades of Stage Ⅱ Compressor
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摘要: 压气机叶片是飞机发动机的重要部件,根据叶片的特点,从原位探伤的角度出发,设计了最佳的涡流探伤方法。给出了合适的检测频率。根据叶片的安装部位,设计了专用的传感器。实际探伤结果表明,该方法探伤效果良好。Abstract: The blade of aircraft engine compressor is an important component. The best method of eddy current testing was designed, and the appropriate testing frequency from the perspective of in-situ testing was given according to the characteristics of blades. Special sensor was designed based on the installation of blade parts. Actual testing results showed that the testing method was suitable.
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Keywords:
- Compressor /
- Eddy current testing /
- Blade
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[1] 陶旺斌,周在杞.电磁检测[M].北京:航空工业出版社,1995:152-166. [2] 孙金立,陈新波.放置式探头检测工件时特征频率的计算[J].无损检测,2001,23(5):185-189. [3] 任吉林,林俊明.电磁检测[M].北京:机械工业出版社,2000:57-79.
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