Development of a Variable Delivery Positive Displacement Fuel Pump.
Final rept. 6 Jan 69-4 Mar 71,
SPERRY RAND CORP TROY MICH VICKERS AEROSPACE DIV
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A Research and Development Program was conducted to produce a variable, positive displacement pump for application to the fuel systems of turbine engines. A variable positive displacement pump complete with an electrical input signal actuation system was designed and developed to physically fit and supply the flow requirements of the J-85-7 turboject engine. Author
- Pumps, Filters, Pipes, Tubing, Fittings and Valves
- Jet and Gas Turbine Engines