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Design concepts for low-cost composite engine framesDesign concepts for low-cost, lightweight composite engine frames were applied to the design requirements for the frame of commercial, high-bypass turbine engines. The concepts consist of generic-type components and subcomponents that could be adapted for use in different locations in the engine and to different engine sizes. A variety of materials and manufacturing methods were assessed with a goal of having the lowest number of parts possible at the lowest possible cost. The evaluation of the design concepts resulted in the identification of a hybrid composite frame which would weigh about 70 percent of the state-of-the-art metal frame and cost would be about 60 percent.
Document ID
19840008118
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:83544
E-1916
NASA-TM-83544
Report Number: NAS 1.15:83544
Report Number: E-1916
Report Number: NASA-TM-83544
Meeting Information
Meeting: Aircraft Design Systems and Operations Meeting
Location: Fort Worth, TX
Country: United States
Start Date: October 17, 1983
End Date: October 19, 1983
Sponsors: AHS, AIAA
Accession Number
84N16186
Funding Number(s)
PROJECT: RTOP 505-33-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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