Fuselage inspection of Boeing-737 using lock-in thermography

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 6939, Issue , 2008, Pages

  Tarin, Markus ^a   Kasper, André ^b  

^a MoviTHERM   (United States)

^b Automation Technology GmbH   (Germany)

Author keywords

Delamination; Disbonding; Lock in thermography; Rivets; Thermal radioscopy; Thermal waves; Water inclusion

Indexed keywords

DEFECTS; ELASTIC WAVES; FUSELAGES; HEAT RADIATION; IMAGE RECORDING;

DISBONDING; LOCK-IN THERMOGRAPHY; THERMAL WAVES; WATER INCLUSION;

THERMOGRAPHY (IMAGING);

EID: 43249087835     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.777008     Document Type: Conference Paper

References (8)

1. Mukesh V. Gandhi, Brian S. Thompson, "Smart Materials and Structures", (1992), p. 122
2. http://www.boeing.com/commercial/737family/background.html
3. J.Lo, T.Nishino, S.V.Hoa, H. Hamada, A. Nakai, C. Poon, "Design, Manufacturing and Applications of Composites", Proceedings of the sixth joint Canada-Japan workshop on composites; August 2006, Toronto, Canada
4. Airbus Deutschland GmbH, Kretslag 10, Quality Assurance, Material Testing, D-21129 Hamburg, Germany
5. Lufthansa Technik AG, Aircraft Overhaul, NDT Workshop, Weg beim Jaeger 193, D-22335 Hamburg, Germany
6. The Boeing Company, Customer Service Division, Seattle, WA 98124-2207, USA
7. Subhesh L. Shindé, Jitenda Groela, "High Thermal Conductivity Materials", Springer 2006
8. National Transportation Safety Board; www.ntsb.gov