Analysis on Fatigue for Aircraft Riveting Thin-Walled Components

Wen Liang Chen; Yue Yang; Hong Yu Wei; Hong Yu Jiang; Zhi Xiang Huang; Yu Bo Wang; Lu Yu

doi:10.4028/www.scientific.net/AMM.246-247.122

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 246-247Analysis on Fatigue for Aircraft Riveting...

Analysis on Fatigue for Aircraft Riveting Thin-Walled Components

Abstract:

Fatigue damage of airframe often caused by riveting defects, which resulting in failure of aircraft structure in service. Based on the theory of classical fatigue fracture, the effects of Interference-fit gap on capabilities of safe service are examined and a new method of measuring the dimension of Interference-fit gap under the different conditions is introduced by cutting test and fatigue test of typical aluminum alloy 2024-T3 in aero industries. And the admissible value of Interference-fit gap for riveting is given, which offered the technological basis to achieve long fatigue of the aircraft.

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Periodical:

Applied Mechanics and Materials (Volumes 246-247)

Pages:

122-126

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.246-247.122

Citation:

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Online since:

December 2012

Authors:

Wen Liang Chen, Yue Yang, Hong Yu Wei, Hong Yu Jiang, Zhi Xiang Huang, Yu Bo Wang, Lu Yu

Keywords:

Aircraft Assembly, Fatigue, Interference-Fit Gap, Riveting Components

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References

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