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RESEARCH PAPERS

Sizing of an Aircraft Fuel Pump

[+] Author and Article Information
U. S. Rohatgi

Brookhaven National Laboratory, Department of Advanced Technology, Building 475B, Upton, NY 11973

J. Fluids Eng 117(2), 298-302 (Jun 01, 1995) (5 pages) doi:10.1115/1.2817144 History: Received March 19, 1993; Revised June 06, 1994; Online December 04, 2007

Abstract

A need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.

Copyright © 1995 by The American Society of Mechanical Engineers
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