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Method of Accurate Countersinking and Rivet Shaving
ISSN: 0148-7191, e-ISSN: 2688-3627
Published September 10, 2001 by SAE International in United States
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Wing skin riveting and bolting requires the surface to be flush to +/–.025mm(.001″) to produce an acceptable finish. Using the method described in this paper, automated wing riveting technology and panel assembly techniques can achieve better shave height and countersink accuracies than have previously been possible in production.
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CitationRudberg, T., Smith, S., and Smith, A., "Method of Accurate Countersinking and Rivet Shaving," SAE Technical Paper 2001-01-2569, 2001, https://doi.org/10.4271/2001-01-2569.
- Hartmann, John Meeker, Chris “Automated Wing Panel Assembly for the A340-600” SAE Aerospace Automated Fastening Conference and Exposition New Orleans, Louisiana September 20–22 2000
- “The Art of Wing Assembly” Aerospace Engineering July 2001