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Design Studies of Lift Fan Engines Suitable for Use in Civilian VTOL Aircraft FREE

[+] Author Affiliations
R. J. Roelke

National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH

Steve Zigan

General Electric Co., Cincinnati, OH

Paper No. 72-GT-65, pp. V001T01A064; 8 pages
doi:10.1115/72-GT-65
From:
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • San Francisco, California, USA, March 26–30, 1972
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7981-8
  • Copyright © 1972 by ASME

abstract

Low pressure ratio fan engines are receiving increasing attention as a means to provide low speed lift for civilian VTOL transports. Two general types of fan lift engines that are being studied are integral fans and remote powered fans. Preliminary engine design studies of both types of lift fan systems have been made. This paper summarizes a portion of the results of the engine design studies, including the crucial engine requirements, and some of the characteristics of the emerging engine designs of each type.

Copyright © 1972 by ASME
Topics: Engines , Design , Aircraft
This article is only available in the PDF format.

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