DocumentCode :
3202500
Title :
Eddy Current Array Instrument and Probe for Crack Detection of Aircraft Tubes
Author :
Bo, Liu ; Feilu, Luo ; Zhongqing, Jin ; Jiali, Liu
Author_Institution :
Nat. Univ. of Defense Technol., Changsha, China
Volume :
2
fYear :
2010
fDate :
11-12 May 2010
Firstpage :
177
Lastpage :
180
Abstract :
Failure of aircraft tubes inspections is decidedly hazardous. However, conventional eddy current testing for tubes is very time-consuming. Eddy current array technology can dramatically decrease the inspection time by reducing to one the number of rotations needed to completely cover the tube surface. A new eddy current array instrument and probe was presented, the ECA imaging principle and the hardware frame of the system was described. By means of FEM simulation, optimize the parameter of the eddy current array probe. Based on the instrument and probe, the aircraft oil deliver EDM north with an axial crack was detected. The experimental results show that not only the instrument and probe are able to identify the existence of cracks quickly and effectively, but also estimate the location of cracks. Further studies have shown that the inspection resolution is the length of cracks with tolerance ±2 mm and the depth of cracks with tolerance ±20%.
Keywords :
aircraft maintenance; crack detection; eddy current testing; finite element analysis; inspection; pipes; FEM simulation; aircraft oil; aircraft tubes inspections; axial crack detection; eddy current array imaging principle; eddy current array instrument; probe; Aircraft; Circuits; Eddy currents; Frequency synthesizers; Inspection; Instruments; Petroleum; Probes; Pulse amplifiers; Signal generators; Aircraft Tubes; Crack Detection; Eddy Current Array; Probe Design;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2010 International Conference on
Conference_Location :
Changsha
Print_ISBN :
978-1-4244-7279-6
Electronic_ISBN :
978-1-4244-7280-2
Type :
conf
DOI :
10.1109/ICICTA.2010.85
Filename :
5523212
Link To Document :
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