Graphite Composite Materials Applications in Aircraft Structures

750533

02/01/1975

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
Graphite fiber-reinforced composite materials have been evaluated for use in aircraft structural components, primarily as a means of reducing the weight of selected metal parts. Control surfaces, fairings, internal structures, and landing gear have been manufactured, laboratory tested, and, in many cases, flight tested. Weight savings of 15-30% have been demonstrated; and, through less conservative design estimates, savings in excess of 40% appear feasible. Raw material cost has been the pacing item in approaching business aircraft applications; however, current trends show strong potential for cost competitive use.
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DOI
https://doi.org/10.4271/750533
Pages
12
Citation
Cross, S., "Graphite Composite Materials Applications in Aircraft Structures," SAE Technical Paper 750533, 1975, https://doi.org/10.4271/750533.
Additional Details
Publisher
Published
Feb 1, 1975
Product Code
750533
Content Type
Technical Paper
Language
English