Ultrasonic imaging of corrosion and fatigue cracks in multilayered airplane structures

Igor N. Komsky*, Jan D. Achenbach

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Scopus citations

Abstract

Application of ultrasonic imaging to the inspection of multilayered airplane structures can provide comprehensive information on possible defects such as corrosion and cracks. A quantitative assessment of defects in internal layers of airplane structures using this technique can be accomplished form an external surface of the airplane skin. No disassembly is required for component evaluation. Therefore this ultrasonic technique can be extremely useful for cost-effective maintenance of airplanes. Three different ultrasonic techniques developed for inspection of the DC-9 and DC-10 airplanes are discussed in this paper. One of the techniques was used for evaluation of corrosion and stress corrosion cracks in a DC-9 tee cap, other techniques have been developed for fatigue crack characterization in a DC-9 rear spar and a DC-10 spar-cap/strap connection, respectively. All three techniques were developed to be applied with the same type of data acquisition and imaging system. However for each kind of flaw and structural configuration substantial modifications of the scanning and the data acquisition procedures have been made. Peculiarities of each ultrasonic technique will be discussed. The ultrasonic technique for the inspection of the DC-9 tee cap has been approved by the FAA as an alternate means of compliance to meet the requirements of the DC-9 Service Bulletin.

Original languageEnglish (US)
Title of host publicationProceedings of SPIE - The International Society for Optical Engineering
EditorsRaymond D. Rempt, Alfred L. Broz
Pages380-388
Number of pages9
Volume2945
StatePublished - Dec 1 1996
EventNondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware - Scottsdale, AZ, USA
Duration: Dec 3 1996Dec 5 1996

Other

OtherNondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware
CityScottsdale, AZ, USA
Period12/3/9612/5/96

ASJC Scopus subject areas

  • Electronic, Optical and Magnetic Materials
  • Condensed Matter Physics
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

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    Komsky, I. N., & Achenbach, J. D. (1996). Ultrasonic imaging of corrosion and fatigue cracks in multilayered airplane structures. In R. D. Rempt, & A. L. Broz (Eds.), Proceedings of SPIE - The International Society for Optical Engineering (Vol. 2945, pp. 380-388)