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US5159808A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine engine fuel and hydraulic fluid pumping system

Assignee: General Electric Co
•
Filing: 1990-07-09
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Granted: 1992-11-03
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Expires: 2010-07-09
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Abstract

Abstract An arrangement for a main fuel pump, a backup fuel pump, a main hydraulic pump, and a backup hydraulic pump, typically for a gas turbine engine in an aircraft, includes an isolated fuel and hydraulic fluid system and a backup pumping arranngement employing two mechanically-coupled gear-type reversible pump-motors and appropriate control valves.

Inventors

  • 👤 Howard B. Kast

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 10:09
CPC Classifications
F; F02; F02M; F02M37/00; F02M37/04; F02M37/18; F02C; F02C7/00; F02C7/22; F02C7/236; F02C7/32

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 167 words
A gas turbine engine fuel and hydraulic fluid pumping apparatus comprising: a fuel circuit and a hydraulic fluid circuit isolated from said fuel circuit. a first means for pressurizing the fuel in said fuel circuit and a first means for pressurizing the hydraulic fluid in said hydraulic fluid circuit. a second means for pressurizing the fuel in said fuel circuit and a second means for pressurizing the hydraulic fluid in said hydraulic fluid circuit. wherein said second means for pressurizing the fuel and hydraulic fluid in their respective circuits include fuel and hydraulic fluid reversible pump-motors in their respective circuits, means for switching said pump-motors to their pump or motor modes, and means to drive one of said pump-motors in its pump mode by other of said pump-motors in its motor mode. wherein said means for switching said pump-motors to their pump and motor modes includes a hydraulic slide valve interposed in said hydraulic fluid circuit between said first and second means for pressurizing the hydraulic fluid.
Claim 2
Dependent Claim 167 words
A gas turbine engine fuel and hydraulic fluid pumping apparatus comprising: a fuel circuit and a hydraulic fluid circuit isolated from said fuel circuit. a first means for pressurizing the fuel in said fuel circuit and a first means for pressurizing the hydraulic fluid in said hydraulic fluid circuit. a second means for pressurizing the fuel in said fuel circuit and a second means for pressurizing the hydraulic fluid in said hydraulic fluid circuit. wherein said second means for pressurizing the fuel and hydraulic fluid in their respective circuits include fuel and hydraulic fluid reversible pump-motors in their respective circuits, means for switching said pump-motors to their pump or motor modes, and means to drive one of said pump-motors in its pump mode by other of said pump-motors in its motor mode. wherein said means for switching said pump-motors to their pump and motor modes includes a hydraulic slide valve interposed in said hydraulic fluid circuit between said first and second means for pressurizing the hydraulic fluid.
Claim 3
Dependent Claim 33 words
The apparatus of claim 1 wherein said means for switching said pump-motors to their pump or motor modes includes a hydraulic slide valve actuation means responsive to a pressure in said fuel circuit.
Claim 4
Dependent Claim 33 words
The apparatus of claim 1 wherein said means for switching said pump-motors to their pump or motor modes included a fuel slide valve actuation means responsive to a pressure in said fuel circuit.
Claim 5
Dependent Claim 46 words
The apparatus of claim 1 wherein said means for switching said pump-motors to their pump or motor modes includes a fuel slide valve actuation means and a hydraulic slide valve actuation means responsive to a pressure failure signal generated by a pump failure signal generating means.
Claim 6
Dependent Claim 32 words
The apparatus of claim 4 wherein said a first means for pressurizing the fuel and said first means for pressurizing the hydraulic fluid are driven by the engine through an engine gearbox.

References Cited (Backward Citations)

US3369491A Cited
US4291532A Cited
US4546745A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-11-03 1996-05-04 1996-11-03 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-11-03 2000-05-04 2000-11-03 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-11-03 2004-05-04 2004-11-03 $7700.00 Window Closed / Lapsed

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