Paper Title:
Tracking of Cracks in Airplane Components Using Nonlinear Surface Wave Propagation Techniques
  Abstract

Ultrasonic surface waves provide a sensitive means to detect cracks in airplane structures. Until now several obstacles remained to use ultrasonic surface waves for on-line damage detection (i.e. in-flight). In this article a method will be proposed to detect a growing fatigue crack while the aircraft is operating. In contrast to classical ultrasonic measurement methods, that use a high voltage pulse, we applied an optimized multi-sine excitation signal with an amplitude of a few volts only (this agrees better with the applicable safety regulations for aircraft). Furthermore, an indicator quantifying the nonlinearity of the ultrasonic surface wave propagation is used. By using a nonlinearity index the influence of changing operation conditions that can be observed with most linear methods is eliminated. The proposed method is validated on a steel beam that is fatigue loaded with a force signal obtained from in-flight data.

  Info
Periodical
Key Engineering Materials (Volumes 293-294)
Edited by
W.M. Ostachowicz, J.M. Dulieu-Barton, K.M. Holford, M. Krawczuk and A. Zak
Pages
549-556
DOI
10.4028/www.scientific.net/KEM.293-294.549
Citation
S. Vanlanduit, P. Guillaume, J. Vermeulen, K. Harri, "Tracking of Cracks in Airplane Components Using Nonlinear Surface Wave Propagation Techniques ", Key Engineering Materials, Vols. 293-294, pp. 549-556, 2005
Online since
September 2005
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Price
$32.00
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