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Boron/aluminum fan blades for SCAR enginesProcessing procedures were developed to enhance boron/aluminum bond behavior and foreign object damage (FOD) tolerance. Design and analysis indicated that the J101 Stage 1 fan blade meets the required frequencies without a midspan shroud. The fabricability of full size J101 blades was assessed, while six blades were fabricated and finished machined.
Document ID
19770019191
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stabrylla, R. G. (General Electric Co. Cincinnati, OH, United States)
Carlson, R. G. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135184
Report Number: NASA-CR-135184
Accession Number
77N26135
Funding Number(s)
CONTRACT_GRANT: NAS3-18910
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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