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Turbotip Lift Fan Design FREE

[+] Author Affiliations
W. W. Thomas

General Electric Co., Cincinnati, OH

Paper No. 72-GT-111, pp. V001T01A109; 15 pages
doi:10.1115/72-GT-111
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

This paper discusses the basic design approach and features of the turbotip lift fan concept, initially developed for application in the XV-5 VTOL research aircraft. Design changes necessary to meet the requirements of the proposed NASA V/STOL transport research aircraft and future commercial transport systems are reviewed. Emphasis is placed on the effects of acoustic, installation, control response and life/maintenance objectives on component design and lift fan geometry.

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

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