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Aircraft Gas Turbine Engine Fuel Pumping Systems in the 21st Century FREE

[+] Author Affiliations
Lowell D. Hansen, Gregory D. Kucera, Jeffrey S. Clemons, Jinkook Lee

Argo-Tech Corporation, Cleveland, OH

Paper No. 96-GT-148, pp. V005T15A018; 9 pages
doi:10.1115/96-GT-148
From:
  • ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General
  • Birmingham, UK, June 10–13, 1996
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7876-7
  • Copyright © 1996 by ASME

abstract

Since their introduction, main engine fuel pumping systems for aircraft gas turbine engines have remained relatively unchanged. The main engine fuel pump has been an engine accessory gearbox driven, positive displacement pump (except for the Concorde), until recently when centrifugal pumps were introduced on Pratt-Whitney and General Electric military engines. This paper describes some of the issues which must be addressed as pumping system technology moves into the 21st century and gives a description of two programs which address these issues.

Copyright © 1996 by ASME
This article is only available in the PDF format.

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