The modeling of multi-state deformation in aircraft panel automated riveting system

Xiaoge Li, Zhang Kaifu, Yuan Li

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

2 Scopus citations

Abstract

Automatic drilling and riveting process, in order to improve the quality of drilling and riveting aircraft panel deformation are needed for compensation. Due to panels in automatic drilling and riveting process with more posture, therefore, solving panel deformation of plates under more posture is important. This paper establishes aircraft panel in the automatic drilling riveting process multiple posture deformation model. Firstly, simplify the manner of support, locate and clamping between the panel and the splints, supportive of integral panel at each location are calculated using three-moment theory to provide data reference for spacing between splints. Then, deformation results are calculated using flat shell theory to provide data reference for error compensation in automated riveting system, thus, drilling and riveting quality are improved.

Original languageEnglish
Title of host publicationIndustrial Design and Mechanical Power
Pages123-127
Number of pages5
DOIs
StatePublished - 2012
Event2012 International Conference on Industrial Design and Mechanical Power, ICIDMP 2012 - Huangshan, China
Duration: 10 Jul 201211 Jul 2012

Publication series

NameApplied Mechanics and Materials
Volume224
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2012 International Conference on Industrial Design and Mechanical Power, ICIDMP 2012
Country/TerritoryChina
CityHuangshan
Period10/07/1211/07/12

Keywords

  • Automated riveting system
  • Deformation of aircraft panel
  • Splint loading

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