• 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