This paper presents a description of the development of a full-scale filament wound aircraft fuselage shell. Included is a description of the structural details such as floor reinforcements, window reinforcements, and ring frames. The contributions of several sub-components of constant diameter are presented, in tooling development, process development, and to the structural design of the shell.
Development of a full-scale filament wound fuselage shell
Entwicklung eines wickelgeformten Rumpfmantels in natuerlicher Groesse
Technical Paper. Society of Manufacturing Engineers ; Jun ; 1-24
1987
24 Seiten, 23 Bilder, 3 Tabellen
Conference paper
English
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