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Design study and performance analysis of a high-speed multistage variable-geometry fan for a variable cycle engineA design technology study was performed to identify a high speed, multistage, variable geometry fan configuration capable of achieving wide flow modulation with near optimum efficiency at the important operating condition. A parametric screening study of the front and rear block fans was conducted in which the influence of major fan design features on weight and efficiency was determined. Key design parameters were varied systematically to determine the fan configuration most suited for a double bypass, variable cycle engine. Two and three stage fans were considered for the front block. A single stage, core driven fan was studied for the rear block. Variable geometry concepts were evaluated to provide near optimum off design performance. A detailed aerodynamic design and a preliminary mechanical design were carried out for the selected fan configuration. Performance predictions were made for the front and rear block fans.
Document ID
19790016849
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sullivan, T. J.
(General Electric Co. Cincinnati, OH, United States)
Parker, D. E.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159545
Report Number: NASA-CR-159545
Accession Number
79N25020
Funding Number(s)
CONTRACT_GRANT: NAS3-20041
CONTRACT_GRANT: R79AEG288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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