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Method of Accurate Countersinking and Rivet Shaving
Technical Paper
2001-01-2569
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
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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Citation
Rudberg, 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.Also In
References
- 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