Nondestructive Evaluation of Temporarily Repaired CFRP Laminates Subjected to Delaminations due to Localized Heating and Cyclic Loading Combined

  • Han, Tae-Young (Graduate School, Department of Mechanical Engineering, Inha University) ;
  • Kwon, Oh-Yang (Department of Mechanical Engineering, Inha University)
  • 발행 : 2007.06.30

초록

The reliability of cold-bonding repair technique of carbon-fiber reinforced plastics (CFRP) laminates, often used as a temporary repair for the airplane maintenance, has been evaluated during cyclic loading and localized heating by nondestructive methods. Major concern was given to the evolution of damage after repair in the form of delaminations due to localized heating and cyclic loading combined. An area of interest both on the specimen repaired by cold-bonding and the specimen without repair where delaminations were induced by localized heating and cyclic loading was monitored by acoustic emission (AE) testing and further examined by pitch-catch low-frequency bond testing, and pulse-echo high-frequency ultrasonic testing. The results showed that the reliability of cold-bonding repair would be significantly reduced by the localized heating and cyclic loading combined rather than by the cyclic loading only. AE monitoring appeared to be an effective and reliable tool to monitor the integrity of temporarily repaired CFRP laminates in terms of the structural health monitoring (SHM) philosophy.

키워드

참고문헌

  1. BAC5337 (2000) Boeing Process Spec.: Application of Nonstructural Wet Lay-Up Plies to Composite Panels
  2. BAC5578 (2002) Boeing Process Spec.: Manufacture of Advanced Carbon Fiber Reinforced Advanced Composite Structure with Toughened Epoxy Systems, + 350 F Cure
  3. BAC5980 (2002) Boeing Process Spec.: Nondestructive Inspection of Composite Parts and Structures
  4. Boeing SRM (2007) Structural Repair Manual for B777-200, D634W201
  5. Bolotin, V. V. (1996) Delaminations in Composite Structures: Its Origin, Buckling, Growth and Stability, Composites Structure, pp. 129-145
  6. Fitch, C. E., Jr. (1991) Pulsed Low Frequency Ultrasonic Bond and Thickness Testing, Air Transport Association NDT Forum
  7. Galella, D. (2006) FAA Inspection Research Activities for Composite Materials, The 2006 Composite Damage Tolerance & Maintenance Workshop
  8. Hall, S. R. and Conquest, T. J. (1999) The Total Data Integrity Initiative Structural Health Monitoring; The Next Generation, Proc. the USAF ASIP, 2nd Ed
  9. Kessler, S. S., Spearing S. M., Atalla, M. J., Cesnik, C. E. S. and Soutis, C. (2001) Structural Health Monitoring in Composite Materials Using Frequency Response Methods, accepted for publication by Composites - Part B
  10. Kessler, S. S. (2002) Piezoelectric-Based In-Situ Damage Detection of Composite Materials for Structural Health Monitoring Systems, Ph. D. Thesis, Massachusetts Institute of Technology
  11. Kim, Sung-Jin, Kwon, Oh-Yang and Jang, Yong-Joon Fatigue Crack Growth Behavior of and Recognition of AE Signals from Composite Patch-Repaired Aluminum Panel, J. KSNT, Vol. 27, No. 1, pp. 48-57
  12. Marantidis C., Van Way, C. B. and Kudva, J. N. (1994) Acoustic Emission Sensing in an On-Board Smart Structural Health Monitoring System for Military Aircraft, Proc. the SPIE Conference on Smart Structures and Integrated Systems, Vol. 2191, pp. 258-264
  13. Matsuzaki, R. and Todoroki, A. (2006) Wireless Detection of Internal Delamination Cracks in CFRP Laminates Using Oscillating Frequency Changes, Composites Science and Technology, Vol. 66, pp. 407-416 https://doi.org/10.1016/j.compscitech.2005.07.016
  14. Matt, H. M. (2006) Structural Diagnostics of CFRP Composite Aircraft Components by Ultrasonic Guided Waves and Built-In Piezoelectric Transducers, U. of California, pp. 35-43
  15. MIL-HDBK-17 (1999) Guidelines for of Structural Materials, Vol. 1, Materials, U.S. Department of Characterization The Composite Defense
  16. Teller, C., Dierks, K., Bar-Cohen, Y., and Shaw, N. (1987) Nondestructive Evaluation of Adhesive Bonds, Proc. 16th Symposium on Nondestructive Evaluation, San Antonio, Texas
  17. Worlton, D. C. (1961) Experimental Confirmation of Lamb Waves at Megacycle Frequencies, J. of Applied Physics, Vol. 32, pp. 967-971 https://doi.org/10.1063/1.1736196