Composite laminates in significant numbers are rendered unacceptable due to delamination that occurs during the drilling operation. Thrust generated during the drilling operation is identified as responsible for delamination. Expressions developed for critical thrusts and critical feed rates, by modeling the delamination zone as an elliptical plate in unidirectional laminates, appear to be fairly accurate. It has been demonstrated that the critical thrusts and feed rates obtained for unidirectional laminates can be conservatively used for multi-directional laminates. With regard to the tool geometry, the chisel edge width appears to be the single most important factor contributing to the thrust force and hence delamination. A diamond-impregnated tubular drill tool was designed and tested. This tool resulted in a much smaller thrust and much better hole quality as compared with the standard twist drills.
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November 1994
This article was originally published in
Journal of Engineering for Industry
Research Papers
Delamination-Free Drilling of Composite Laminates
S. Jain,
S. Jain
United Technologies Research Center, East Hartford, CT 06108
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D. C. H. Yang
D. C. H. Yang
Mechanical, Aerospace and Nuclear Engineering Department, University of California, Los Angeles, Los Angeles, CA 90024
Search for other works by this author on:
S. Jain
United Technologies Research Center, East Hartford, CT 06108
D. C. H. Yang
Mechanical, Aerospace and Nuclear Engineering Department, University of California, Los Angeles, Los Angeles, CA 90024
J. Eng. Ind. Nov 1994, 116(4): 475-481
Published Online: November 1, 1994
Article history
Received:
November 1, 1992
Revised:
December 1, 1993
Online:
April 8, 2008
Citation
Jain, S., and Yang, D. C. H. (November 1, 1994). "Delamination-Free Drilling of Composite Laminates." ASME. J. Eng. Ind. November 1994; 116(4): 475–481. https://doi.org/10.1115/1.2902131
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