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飞机紧固件孔壁裂纹的涡流无损检测 被引量:2

Eddy Current Testing of Aircraft Fastener Hole Wall Cracks
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摘要 在分析涡流无损检测技术工作原理的基础上,阐述涡流无损检测技术检测飞机紧固件孔壁裂纹的方法步骤,并对飞机紧固件孔壁裂纹的修理工作提出相关建议,以期为后续工作提供参考与借鉴。 Based on analyzing the working principle of eddy current testing technology,this paper expounds the method and procedure of detecting the aircraft fastener hole wall cracks by eddy current nondestructive testing technology,and puts forward relevant suggestions on repair work of aircraft fastener hole wall cracks in order to provide reference and experience for the follow-up work.
出处 《西安航空学院学报》 2013年第5期10-12,共3页 Journal of Xi’an Aeronautical Institute
关键词 飞机紧固件 孔壁裂纹 涡流无损检测 aircraft fasteners hole wall cracks eddy current testing
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