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Improved Fastener Systems For Fatigue and Sealing Redundancy of Low Shear Transfer Joints
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English
Abstract
A brief summary is presented of general fatigue characteristics of low-shear transfer aircraft joints and discussion of some improved fastening systems for providing fatigue and sealing redundancy of these joints.
Citation
Ruhl, J. and Hurd, R., "Improved Fastener Systems For Fatigue and Sealing Redundancy of Low Shear Transfer Joints," SAE Technical Paper 730901, 1973, https://doi.org/10.4271/730901.Also In
References
- “Cold Expansion of Fastener Holes For Fatigue Improvement.” The Boeing Company
- “An Evaluation of Fatigue Resistant Fasteners Systems in Aluminum Joints.” The Boeing Company
- “Fatigue and Stress-Corrosion Test of Selected Fasteners/Hole Processes.” Aeronautical System Division, Wright-Patterson Air Force Base
- “Military Standardization Handbook.”