Engine fuel control system

Patent metadata

Field	Value
Publication number	US-9617923-B2
Application number	US-201414528562-A
Country	US
Kind code	B2
Filing date	Oct 30, 2014
Priority date	Jan 3, 2014
Publication date	Apr 11, 2017
Grant date	Apr 11, 2017

Abstract

An engine fuel control system includes a fuel metering valve that controls the flow of fuel between supply and delivery lines which delivers fuel to engine burners. The fuel control system includes a fixed displacement main pump which receives fuel from a low pressure source and delivers the fuel at a first high pressure to the supply line, an augmenter pump which receives fuel from the low pressure source and delivers the fuel at a second high pressure to one or more fuel-pressure operated auxiliary engine devices, and a start valve which is actuated at low engine speeds to open a flow path which diverts fuel delivered by the augmenter pump away from the auxiliary engine devices to the supply line to augment the fuel delivered thereto by the main pump, the start valve being actuated at higher engine speeds to shut the flow path.

First claim

The invention claimed is:

1. An engine fuel control system including:
a fuel metering valve operable to control a flow of fuel between a supply line and a delivery line which delivers fuel to burners of an engine;
a fixed displacement main pump configured to receive fuel from a low pressure source and deliver the fuel at a first high pressure to the supply line;
a variable displacement augmenter pump which is configured to receive fuel from the low pressure source and deliver the fuel at a second high pressure to one or more fuel-pressure operated auxiliary engine devices, the variable displacement augmenter pump being configured to provide a fuel delivery flow rate which is variable to compensate for fuel flow demands imposed by the one or more fuel-pressure operated auxiliary engine devices; and
a start valve which is configured to be actuated at low engine speeds to open a flow path which diverts fuel delivered by the variable displacement augmenter pump away from the one or more fuel-pressure operated auxiliary engine devices to the supply line to augment the fuel delivered thereto by the fixed displacement main pump, the start valve being configured to be actuated at higher engine speeds to shut the flow path;
wherein the variable displacement augmenter pump has a servo-controller configured to vary its pump flow rate; and
wherein the engine fuel control system further includes a pressure drop control valve which is configured to sense a pressure differential across the variable displacement augmenter pump, the pressure drop control valve being arranged to control the servo-controller such that the pump flow rate of the variable displacement augmenter pump is varied to maintain a pressure differential across the variable displacement augmenter pump at a predetermined level, and being configured to spill, at the higher engine speeds, a portion of the fuel delivered by the variable displacement augmenter pump away from the one or more fuel-pressure operated auxiliary engine devices to the supply line to augment the fuel delivered thereto by the fixed displacement main pump.

2. The engine fuel control system according to claim 1 , wherein at the low engine speeds the flow path diverts all of the fuel delivered by the variable displacement augmenter pump to the supply line.

3. The engine fuel control system according to claim 1 , wherein the start valve is configured to be actuated by a change in pressure of the fuel received from the low pressure source, the pressure of the fuel received from the low pressure source being a function of engine speed.

4. The engine fuel control system according to claim 1 , wherein the low pressure source is a low pressure pump.

5. The engine fuel control system according to claim 1 , wherein at the low engine speeds, the pressure drop control valve is arranged to control the servo-controller such that the pump flow rate of the variable displacement augmenter pump is a constant maximum rate for a given speed.

6. The engine fuel control system according to claim 1 , wherein, at the higher engine speeds, the pressure drop control valve is configured to spill a portion of the fuel delivered by the variable displacement augmenter pump away from the one or more fuel-pressure operated auxiliary engine devices to the supply line to augment the fuel delivered thereto by the fixed displacement main pump.

7. The engine fuel control system according to claim 6 , wherein an amount of fuel spilled by the pressure drop control valve changes in inverse relation to variations in the pump flow rate of the variable displacement augmenter pump.

8. The engine fuel control system according to claim 1 , wherein when, at the higher engine speeds, the difference between the first high pressure and the second high pressure reduces to less than a predetermined amount, the pressure drop control valve is arranged to control the servo-controller such that the pump flow rate of the variable displacement augmenter pump is a constant maximum rate for a given speed.

9. The engine fuel control system according to claim 1 , wherein the fixed displacement main pump is a single gear pump.

10. The engine fuel control system according to claim 1 , wherein the fixed displacement main pump is a dual gear pump.

11. The engine fuel control system according to claim 1 , wherein the one or more fuel-pressure operated auxiliary engine devices include any one or more of: a variable stator vane actuator, variable inlet guide vane actuator and a bleed valve actuator.

12. A gas turbine engine having the engine fuel control system according to claim 1 .

13. An engine fuel control system including:
a fuel metering valve operable to control a flow of fuel between a supply line and a delivery line which is configured to deliver fuel to burners of an engine;
a fixed displacement main pump which is configured to receive fuel from a low pressure source and deliver the fuel at a first high pressure to the supply line;
a fixed displacement augmenter pump that is configured to receive fuel from the low pressure source and deliver the fuel at a second high pressure to one or more fuel-pressure operated auxiliary engine devices, and
a start valve which is configured to be actuated at low engine speeds to open a flow path which diverts fuel delivered by the fixed displacement augmenter pump away from the one or more fuel-pressure operated auxiliary engine devices to the supply line to augment the fuel delivered thereto by the fixed displacement main pump, the start valve being configured to be actuated at higher engine speeds to shut the flow path;
wherein the engine fuel control system further includes a pressure drop control valve which is configured to sense a pressure differential across the fixed displacement augmenter pump, the pressure drop control valve being configured to spill, at the higher engine speeds, a variable amount of the fuel delivered by the fixed displacement augmenter pump away from the one or more fuel-pressure operated auxiliary engine devices to the supply line to augment the fuel delivered thereto by the fixed displacement main pump and to maintain a pressure differential across the fixed displacement augmenter pump at a predetermined level.

Assignees

• Rolls Royce Plc
• Rolls-Royce Controls And Data Services Ltd

Inventors

• Griffiths Michael

Classifications

• F01D19/00 Primary

  Starting of machines or engines; Regulating, controlling, or safety means in connection therewith (warming-up before starting F01D25/10; turning or inching gear F01D25/34) · CPC title

• F05D2270/64

  Hydraulic actuators · CPC title

• F02C7/236

  Fuel delivery systems comprising two or more pumps · CPC title

• F05D2270/66

  Mechanical actuators (F05D2270/62 takes precedence) · CPC title

• F02C7/26

  Starting; Ignition · CPC title