The Use of Composite Materials in Aero Engines

670333

02/01/1967

Event
National Aeronautic Meeting and 3rd International Simulation and Training Conference
Authors Abstract
Content
Laboratory investigations of materials properties show that significant reductions in aero-engine weight and cost are possible by using fiberglass reinforced composite materials. These were first applied to fabrication of compressor blades by Rolls-Royce, Ltd. Since the conclusion of the research program coincided with a new design, in which the sole engine function was to support a VTO aircraft during transition, the composites were specified for low temperature components. This paper describes properties of such materials and explains the philosophy adopted in their application. Construction of related subassemblies are fully detailed.
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DOI
https://doi.org/10.4271/670333
Pages
11
Citation
Keen, J., "The Use of Composite Materials in Aero Engines," SAE Technical Paper 670333, 1967, https://doi.org/10.4271/670333.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670333
Content Type
Technical Paper
Language
English