Deformation analysis method for aeronautical thin walled structures with automated riveting

Hui Cheng, Yuan Li, Kaifu Zhang, Feng Guo

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

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.

Original languageEnglish
Title of host publicationFrontiers of Manufacturing and Design Science III
Pages1526-1530
Number of pages5
EditionPART 1
DOIs
StatePublished - 2013
Event3rd International Conference on Frontiers of Manufacturing and Design Science, ICFMD 2012 - , Hong Kong
Duration: 11 Dec 201213 Dec 2012

Publication series

NameApplied Mechanics and Materials
NumberPART 1
Volume271
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference3rd International Conference on Frontiers of Manufacturing and Design Science, ICFMD 2012
Country/TerritoryHong Kong
Period11/12/1213/12/12

Keywords

  • Aeronautical thin-walled structures
  • Automated riveting
  • Deformation
  • Error

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