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Composite hub/metal blade compressor rotorA low cost compressor rotor was designed and fabricated for a small jet engine. The rotor hub and blade keepers were compression molded with graphite epoxy. Each pair of metallic blades was held in the hub by a keeper. All keepers were locked in the hub with circumferential windings. Feasibility of fabrication was demonstrated in this program.
Document ID
19780010188
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yao, S.
(Fiber Science, Inc. Gardena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-135343
Report Number: NASA-CR-135343
Accession Number
78N18131
Funding Number(s)
CONTRACT_GRANT: NAS3-18926
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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