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Propulsion Control Considerations for V/STOL Aircraft FREE

[+] Author Affiliations
T. G. Lenox

Pratt & Whitney Aircraft, East Hartford, CT

Paper No. 72-GT-79, pp. V001T01A078; 8 pages
doi:10.1115/72-GT-79
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

Potential control requirements of various propulsion systems are currently being studied for V/STOL aircraft applications. This paper identifies the considerations which will affect the design of propulsion control systems for both military and commercial aircraft. Of the requirements common to all configurations, the need for improved thrust control is emphasized as requiring total aircraft system trades to establish an approach which provides the desired power management performance with minimum weight and with maximum reliability and maintainability.

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

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