Fuel metering system electrically servoed metering pump

Patent metadata

Field	Value
Publication number	US-9234464-B2
Application number	US-201314079281-A
Country	US
Kind code	B2
Filing date	Nov 13, 2013
Priority date	Jan 5, 2010
Publication date	Jan 12, 2016
Grant date	Jan 12, 2016

Abstract

A fuel metering system for supplying fuel to load includes a variable displacement piston pump having an adjustable hanger that is movable to a plurality of positions. The variable displacement piston pump is configured to receive a drive torque and, upon receipt of the drive torque, to supply fuel to the plurality of loads at a flow rate dependent on the position of the adjustable hanger. A hanger actuator is coupled to receive hanger position commands and is operable, in response thereto, to move the adjustable hanger to the commanded position.

First claim

What is claimed is:

1. A fuel metering system for supplying fuel to a load, comprising:
a gas turbine engine controller adapted to receive throttle input commands and configured, in response thereto, to supply hanger position commands;
a variable displacement piston pump including an adjustable hanger that is movable to a plurality of positions, the variable displacement piston pump configured to receive a drive torque and, upon receipt of the drive torque, to supply fuel to the load at a flow rate and a discharge pressure that is dependent on drive speed and adjustable hanger position;
a hanger actuator coupled to receive the hanger position commands and configured, in response thereto, to move the adjustable hanger to the commanded position, the hanger actuator comprising:
a first piston engaging the adjustable hangar and coupled to receive a first force, the first piston responsive to the first force to supply a hangar position force to the adjustable hanger;
a servo valve coupled to receive a spring force and configured, upon receipt thereof, to control the first force that is supplied to the first piston;
a second piston engaging the adjustable hangar and coupled to receive fuel at the discharge pressure, the second piston configured to supply a pressure control force to the adjustable hangar that opposes the hangar position force; and
an electromechanical actuator coupled to receive the hanger position commands and configured, in response thereto, to control the first force that is supplied to the first piston, the electromechanical actuator comprising:
an electric motor configured to be selectively energized and, upon being selectively energized, supply an actuation drive torque,
a linear actuator coupled to receive the actuation drive torque from the electric motor and control the first force that is supplied to the first piston, and
a bias spring coupled between the linear actuator and the servo valve and configured to supply the spring force to the servo valve.

2. The system of claim 1 , further comprising:
a position sensor coupled to the variable displacement piston pump and configured to supply a position signal representative of hangar position to the gas turbine engine controller.

3. The system of claim 2 , wherein the gas turbine engine controller is configured to supply the hanger position commands in response to the position signal.

4. The system of claim 3 , further comprising:
a pump speed sensor operable to sense variable displacement piston pump speed and to supply a speed signal representative thereof to the gas turbine engine controller.

5. The system of claim 4 , wherein the gas turbine engine controller is configured to supply the hanger position commands additionally in response to the speed signal.

6. The system of claim 1 , further comprising:
a pressure sensor configured to sense the discharge pressure and supply a pressure signal representative thereof to the gas turbine engine controller.

7. A fuel metering system for supplying fuel to a load, comprising:
a variable displacement piston pump including an adjustable hanger that is movable to a plurality of positions, the variable displacement piston pump configured to receive a drive torque and, upon receipt of the drive torque, to supply fuel to the load at a flow rate and a discharge pressure that are dependent on drive speed and adjustable hanger position;
a position sensor coupled to the variable displacement piston pump and configured supply a position signal representative of hangar position;
a pressure sensor configured to sense the discharge pressure and supply a pressure signal representative thereof;
a gas turbine engine controller coupled to receive throttle input commands and the position signal and configured, in response thereto, to supply hanger position commands;
a hanger actuator coupled to receive the hanger position commands and configured, in response thereto, to move the adjustable hanger to the commanded position, the hanger actuator comprising:
a first piston engaging the adjustable hangar and coupled to receive a first force, the first piston responsive to the first force to supply a hangar position force to the adjustable hanger;
a servo valve coupled to receive a spring force and configured, upon receipt thereof, to control the first force that is supplied to the first piston;
a second piston engaging the adjustable hangar and coupled to receive fuel at the discharge pressure, the second piston configured to supply a pressure control force to the adjustable hangar that opposes the hangar position force; and
an electromechanical actuator coupled to receive the hanger position commands and configured, in response thereto, to control the first force that is supplied to the first piston, the electromechanical actuator comprising:
an electric motor configured to be selectively energized and de-energized, the electric motor configured to (i) supply an actuation drive torque upon being selectively energized and (ii) hold position upon being de-energized,
a linear actuator coupled to receive the actuation drive torque from the electric motor and control the first force that is supplied to the first piston, and
a bias spring coupled between the linear actuator and the servo valve and configured to supply the spring force to the servo valve.

Assignees

• Honeywell Int Inc

Inventors

• Benson Dwayne Michael

Classifications

• F02C9/263

  by means of fuel metering valves · CPC title

• F02C7/232 Primary

  Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

• F04B1/324

  by changing the inclination of the swash plate · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F01B3/106

  by changing the inclination of the swash plate · CPC title