Fuel system for gas turbine engines

Details Fuel system for gas turbine engines Fuel system for gas turbine engines

1976-08-27

1978-02-14

Gordon, Clarence R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3909D, F02C 910

Patent

active

040731367

ABSTRACT:
A fuel system for a gas turbine engine has in flow series a low pressure pump, a filter and a high pressure pump, latter being connected to a delivery duct leading to the engine. The low pressure pump is a jet pump wherein the jet is produced by spill flow from the delivery duct. The spill flow is heated to prevent ice formation in the filter.

REFERENCES:
patent: 2670082 (1954-02-01), Dunn
patent: 3627239 (1971-12-01), Hull
patent: 3645094 (1972-02-01), Suggs
patent: 3736072 (1973-05-01), Turner
patent: 3779007 (1973-12-01), Lavash
patent: 3874168 (1975-04-01), Toure

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