Deformation Analysis Method for Aeronautical Thin Walled Structures with Automated Riveting

Hui Cheng; Yuan Li; Kai Fu Zhang; Feng Guo

doi:10.4028/www.scientific.net/AMM.271-272.1526

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 271-272Deformation Analysis Method for Aeronautical Thin...

Deformation Analysis Method for Aeronautical Thin Walled Structures with Automated Riveting

Abstract:

The assembly variation of Aeronautical Thin Walled Structure (ATWS) with automated riveting is inevitable. The deformations of drilling, riveting and releasing are ralated to the final assembly variation. This paper represents a new method for deformation analysis of ATWS with automated riveting. Drilling deformation is modeled by the relationship among deflexion, strain and stress, riveting deformation is modeled by uilibrium equation, and releseaing deformation is modeled by releasing force. The comparison between computing result and expriment proves that the purposed deformation analysis method can solve the problem for ATWS automated riveting efficiently.

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Periodical:

Applied Mechanics and Materials (Volumes 271-272)

Pages:

1526-1530

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.271-272.1526

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Online since:

December 2012

Authors:

Hui Cheng, Yuan Li, Kai Fu Zhang, Feng Guo

Keywords:

Aeronautical Thin-Walled Structures, Automated Riveting, Deformation, Error

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