Wing Structural Assembly Methodology

Paper #:
  • 982156

Published:
  • 1998-09-15
Citation:
Sarh, B., "Wing Structural Assembly Methodology," SAE Technical Paper 982156, 1998, https://doi.org/10.4271/982156.
Author(s):
Pages:
20
Abstract:
This paper reviews today's aircraft wing production assembly methodology and technologies as well as innovative ideas for advancing the high-level wing assembly state-of-the-art. Automated wing assembly systems are only being utilized to rivet/fasten first level subassemblies like panels, spars, and ribs. All other high level assembly tasks are performed manually, incurring associated increases in recurring costs due to production inefficiencies, long lead times, expensive rate tooling, and difficult assembly tasks performed inside small wing compartments. Existing assembly methods, process parameters, and the process characteristics of manual, machine, and man/machine systems provide many opportunities for improving wing assembly.
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