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US3600889A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel control system for gas turbine engines

Assignee: ZF International UK Ltd
•
Filing: 1969-06-17
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Granted: 1971-08-24
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Expires: 1989-06-17
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Abstract

Abstract A system for controlling the fuel supply to a gas turbine engine includes a valve between the fuel pump and the burners of the engine and arranged to spill fuel delivered by the pump. Fuel flows to the burners via a venturi and the spill valve is urged in a direction to spill fuel by the pressure upstream of the venturi and in the other direction by a spring-assisted piston subjected to the pressure at the venturi throat. Cooperating with the spring-assisted piston is a lever actuated by a diaphragm forming one wall of a chamber which is subjected to an air pressure signal derived from the output of the engine compressor and modified by a blade movable in a kinetic orifice. The blade is movable by a governor mechanism and a linkage coupled to the engine throttle control, so that the blade is moved to reduce the pressure in the chamber when the desired engine speed is greater than the actual speed, and thereby move the lever so that the spill valve may operate to increase spillage of fuel. The valve is similarly operated to reduce spillage when the desired speed is greater than the actual speed. An opposite wall of the chamber is formed by a smaller diaphragm biased towards the first diaphragm by a spring. Stops on the respective diaphragms maintain them in spaced relationship. These stops separate at a predetermined pressure to ensure that a sufficient margin for acceleration exists at all engine speeds.

Inventors

  • 👤 Richard J Ifield

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 20:35
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28; F02C9/263; F02C9/32; F02D; F02D1/00; F02D1/02; F05; F05D; F05D2270/00; F05D2270/30; F05D2270/301; F05D2270/3015

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 185 words
A fuel control system for a gas turbine engine having a compressor, comprising a fuel pump, a venturi connected between the fuel pump and the engine, fuel flowing from the pump to the engine passing through said venturi, a fuel pressure control device sensitive to the fuel pressures upstream of said venturi and at the throat of said venturi for varying the fuel pressure upstream of the venturi, loading means providing a bias for said fuel pressure control device against which the difference between said fuel pressures is balanced, said loading device being responsive to an air pressure signal applied thereto from the engine compressor, a governor mechanism driven by the engine at a speed proportional to the engine speed for modifying the air pressure signal applied to said loading device in accordance with the relationship between the desired and actual running speeds of the engine and causing the engine speed to approach the desired speed and a temperature sensitive resilient device acting on said loading means to further modify the bias applied thereby to the fuel pressure control device in accordance with ambient temperature.
Claim 2
Dependent Claim 185 words
A fuel control system for a gas turbine engine having a compressor, comprising a fuel pump, a venturi connected between the fuel pump and the engine, fuel flowing from the pump to the engine passing through said venturi, a fuel pressure control device sensitive to the fuel pressures upstream of said venturi and at the throat of said venturi for varying the fuel pressure upstream of the venturi, loading means providing a bias for said fuel pressure control device against which the difference between said fuel pressures is balanced, said loading device being responsive to an air pressure signal applied thereto from the engine compressor, a governor mechanism driven by the engine at a speed proportional to the engine speed for modifying the air pressure signal applied to said loading device in accordance with the relationship between the desired and actual running speeds of the engine and causing the engine speed to approach the desired speed and a temperature sensitive resilient device acting on said loading means to further modify the bias applied thereby to the fuel pressure control device in accordance with ambient temperature.
Claim 3
Dependent Claim 22 words
A system as claimed in claim 1 in which the fuel pressure control device comprises a spill valve upstream of the venturi.
Claim 4
Dependent Claim 51 words
A system as claimed in claim 2 in which the spill valve is actuated in a direction to increase spillage by the said pressure upstream of the venturi and in a direction to decrease spillage by the said loading means and by the said pressure at the throat of the venturi.
Claim 5
Dependent Claim 17 words
A system as claimed in claim 1 in which the temperature sensitive device comprises a bimetallic spring.
Claim 6
Dependent Claim 34 words
A system as claimed in claim 1 in which the loading means includes a pair of diaphragms which define between them a volume to which, in use, the said air pressure signal is applied.
Claim 7
Dependent Claim 23 words
A system as claimed in claim 5 in which one of the said diaphragms has an area greater than that of the other.
Claim 8
Dependent Claim 90 words
A system as claimed in claim 6 in which said one diaphragm is coupled to the fuel pressure control device and said other diaphragm is urged towards said one diaphragm by biasing means and a further comprising a pair of abutments carried respectively by said diaphragms and interengaged when the air pressure signal has a value less than a predetermined value, whereby the spring force is applied through said abutments to the fuel pressure device, said abutments separating when the air pressure signal has a value above said predetermined value.
Claim 9
Dependent Claim 34 words
A system as claimed in claim 1 in which said governor comprises a kinetic nozzle controlled by a movable blade movable by means responsive to the relationship between the desired and actual engine speeds.
Claim 10
Dependent Claim 40 words
A system as claimed in claim 8 in which the said responsive means comprises a lever coacting both with a speed responsive mechanism driven at a speed proportional to the engine and with a linkage to the engine throttle control.

References Cited (Backward Citations)

US3123128A Cited
GB677138A Cited
US2851855A Cited
US3002348A Cited
US3018621A Cited
US2982096A Cited
US3168102A Cited
US3438199A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-08-23 1975-02-22 1975-08-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-08-23 1979-02-22 1979-08-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-08-23 1983-02-22 1983-08-24 $7700.00 Window Closed / Lapsed

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