Gap volume prediction for aircraft wing assembly

Research output: Contribution to journalArticlepeer-review

65 Downloads (Pure)

Abstract

In this work, two methods for predictive shimming based on laser scan technology and point cloud processing software have been presented. The first one is direct measurement method in PolyWorks, and the second one is feature-based modelling method in SolidWorks. Firstly, both component-level and assembly-level scans are collected by a laser scanner. Then, the point clouds are post-processed and registered in PolyWorks. Thirdly, gap information (shape and thickness) is obtained either in PolyWorks or in SolidWorks. Results show that the proposed methods can obtain gap information successfully based on current hardware and software.
Original languageEnglish
Pages (from-to)227-232
Number of pages6
JournalProcedia Manufacturing
Volume54
Early online date30 Jul 2021
DOIs
Publication statusEarly online date - 30 Jul 2021

Keywords

  • Predictive shimming
  • Laser scan
  • Point cloud data
  • Gap volume prediction
  • Aircraft assembly

Fingerprint

Dive into the research topics of 'Gap volume prediction for aircraft wing assembly'. Together they form a unique fingerprint.

Cite this