• DocumentCode
    3208369
  • Title

    Health monitoring of aircraft wiring by acoustic method

  • Author

    Saha, S. ; Xu, Z. ; Koltsov, D. ; Richardson, A. ; Sutherland, A.

  • Author_Institution
    Dept. of Eng., Lancaster Univ., Lancaster
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    Reliability and dependability challenges within the aerospace, military and civil aviation industries are driving the need for advances in health and usage monitoring technology. One promising method with the potential to complement conventional inspection and electrical test techniques for wiring is acoustic methods. In this paper modelling and experimental results for acoustic signal propagation in various wire systems is reported that includes methods for locating mechanical, electrical and thermal discontinuities in wiring. Simulation results for the pulse echo mode of propagation has provided us a new perspective on the sensitivity achievable. Experimental results support these conclusions. An optimization of the acoustic mode of propagation in a wire by using shear longitudinal and shear transverse excitation are also discussed.
  • Keywords
    acoustic signal detection; aircraft maintenance; aircraft power systems; condition monitoring; inspection; optimisation; reliability; wiring; acoustic method; acoustic signal propagation; aircraft wiring system; electrical discontinuity; electrical test technique; health monitoring technology; inspection; mechanical discontinuity; optimization; pulse echo mode test; reliability; shear longitudinal excitation; shear transverse excitation; thermal discontinuity; Acoustic propagation; Acoustic testing; Aerospace industry; Aerospace testing; Defense industry; Inspection; Military aircraft; Monitoring; Wire; Wiring;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839677
  • Filename
    4839677