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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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  • 1廉纪祥,沈跃.管道远场涡流检测技术的进展[J].油气储运,2004,23(7):14-16. 被引量:28
  • 2王春艳,陈铁群,张欣宇.脉冲涡流检测技术的某些进展[J].无损探伤,2005,29(4):1-4. 被引量:20
  • 3林俊明.第一专题 多频涡流检测原理及应用[J].无损检测,1996,18(1):23-26. 被引量:21
  • 4刘宝,徐彦霖,王增勇,孙朝明.涡流检测技术及进展[J].兵工自动化,2006,25(3):80-82. 被引量:14
  • 5民航无损检测人员资格鉴定与认证委员会.航空器涡流检测.北京:中国民航出版社,2009.
  • 6Moulder J C, Bieber J A, Ward W W, et al. Scanned pulsed-eddy-current instrument for non-destructive inspection of aging aircraft[J]. SPIE, 1996, 2945: 2-13.
  • 7Smith R A,Hugo G R. Transient eddy current NDE for ageing aircraft-capabilities and limitations[J]. Insight,2001,43(1): 14-25.
  • 8Clauzon T, Thollon F, Nicolas A. Flaws Characterization with Pulsed Eddy Currents N. D. T[J]. IEEE Transactions on Magnetics, 1999, 35(3): 1873-1876.
  • 9Dai X W, Ludwig R, Palanisamy R. Numerical Simulation of pulsed Eddy-Current Nondestructive Testing Phenomena[J]. IEEE Transactions on Magnetics, 1990, 26(6): 3089-3096.
  • 10Sophin A, Tian G Y, Taylor D, et al. A feature extraction technique based on principal component analysis for pulsed eddy current NDT[J]. NDT & E International, 2003, 36: 37-41.

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