Wing Structural Assembly Methodology

982156

09/15/1998

Event
Aerofast Conference & Exposition
Authors Abstract
Content
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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DOI
https://doi.org/10.4271/982156
Pages
20
Citation
Sarh, B., "Wing Structural Assembly Methodology," SAE Technical Paper 982156, 1998, https://doi.org/10.4271/982156.
Additional Details
Publisher
Published
Sep 15, 1998
Product Code
982156
Content Type
Technical Paper
Language
English