Fibre Reinforced Composite Applications at De Havilland

810640

04/01/1981

Event
Business Aircraft Meeting and Exposition
Authors Abstract
Content
Fibre reinforced composites have been used in de Havilland aircraft since the late forties. The DHC-5 Buffalo and the DHC-6 Twin Otter continue the use of glass fibre in polyester and epoxy matrices.
The 50 passenger Dash 7 makes extensive use of aramid fibre reinforced composites. The 36 passenger Dash 8 aircraft, presently in the design stage, will probably see a greater application of composites than the Dash 7. Applications are all secondary structure, ranging from simple fairings to load carrying components.
This paper describes the de Havilland experience with fibre reinforced composites, particularly applications on the Dash 7. Interior and exterior applications, together with some design, testing and manufacturing aspects are covered. Proposed Dash 8 applications and some special applications are also briefly covered.
Meta TagsDetails
DOI
https://doi.org/10.4271/810640
Pages
12
Citation
John, L., "Fibre Reinforced Composite Applications at De Havilland," SAE Technical Paper 810640, 1981, https://doi.org/10.4271/810640.
Additional Details
Publisher
Published
Apr 1, 1981
Product Code
810640
Content Type
Technical Paper
Language
English