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Cost analysis of composite fan blade manufacturing processesThe relative manufacturing costs were estimated for large high technology fan blades prepared by advanced composite fabrication methods using seven candidate materials/process systems. These systems were identified as laminated resin matrix composite, filament wound resin matrix composite, superhybrid solid laminate, superhybrid spar/shell, metal matrix composite, metal matrix composite with a spar and shell, and hollow titanium. The costs were calculated utilizing analytical process models and all cost data are presented as normalized relative values where 100 was the cost of a conventionally forged solid titanium fan blade whose geometry corresponded to a size typical of 42 blades per disc. Four costs were calculated for each of the seven candidate systems to relate the variation of cost on blade size. Geometries typical of blade designs at 24, 30, 36 and 42 blades per disc were used. The impact of individual process yield factors on costs was also assessed as well as effects of process parameters, raw materials, labor rates and consumable items.
Document ID
19800022892
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stelson, T. S.
(TRW, Inc. Cleveland, OH, United States)
Barth, C. F.
(TRW, Inc. Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159876
TRW-ER-8064
Report Number: NASA-CR-159876
Report Number: TRW-ER-8064
Accession Number
80N31398
Funding Number(s)
CONTRACT_GRANT: NAS3-21352
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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