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US4073136A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel system for gas turbine engines

Assignee: Rolls Royce PLC
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Filing: 1976-08-27
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Granted: 1978-02-14
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Expires: 1996-08-27
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Abstract

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.

Inventors

  • 👤 Roger J. Symon

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 09:19
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/22

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 118 words
A fuel system for a gas turbine engine, comprising a fuel source, a low pressure jet pump having an inlet chamber connected to said fuel source, said pump including a nozzle for energizing the fluid in the chamber and an outlet for the energized fluid, a filter, a high pressure pump, conduit means connecting in series said outlet of said jet pump said filter said high pressure pump and the engine, and a branch conduit extending from said high pressure pump to said nozzle of the jet pump to supply energizing fluid thereto, said branch including a heater for the fluid passing through said branch thereby to heat the fluid supplied by said jet pump to said filter.
Claim 2
Dependent Claim 118 words
A fuel system for a gas turbine engine, comprising a fuel source, a low pressure jet pump having an inlet chamber connected to said fuel source, said pump including a nozzle for energizing the fluid in the chamber and an outlet for the energized fluid, a filter, a high pressure pump, conduit means connecting in series said outlet of said jet pump said filter said high pressure pump and the engine, and a branch conduit extending from said high pressure pump to said nozzle of the jet pump to supply energizing fluid thereto, said branch including a heater for the fluid passing through said branch thereby to heat the fluid supplied by said jet pump to said filter.

References Cited (Backward Citations)

US2670082A Cited
US3627239A Cited
US3645094A Cited
US3736072A Cited
US3779007A Cited
US3874168A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-02-13 1981-08-15 1982-02-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-02-13 1985-08-15 1986-02-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-02-13 1989-08-15 1990-02-14 $7700.00 Window Closed / Lapsed

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