Smart fuel supply system

Patent metadata

Field	Value
Publication number	US-11859564-B2
Application number	US-202217719060-A
Country	US
Kind code	B2
Filing date	Apr 12, 2022
Priority date	Feb 18, 2022
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

A fuel supply system includes a pump to be connected to a fuel tank. A metering valve is downstream of the pump. A control is programmed to control at least one of the pump and metering valve. The control is operable to take in a flow demand signal and a fuel pressure signal from a controller associated with a gas turbine engine. The flow demand signal is indicative of a desired flow volume and the fuel pressure signal is indicative of a desired fuel pressure. Operation conditions are identified for the at least one of said pump and the metering valve. A gas turbine engine and fuel supply system is also disclosed.

First claim

What is claimed is:

1. A combined gas turbine engine and fuel supply system comprising:
a gas turbine engine including a combustor and an engine controller, said engine controller taking signals from a plurality of components on the gas turbine engine and identifying a desired flow demand and a desired fuel pressure dependent on conditions at the gas turbine engine;
the engine controller being operable to send a flow demand signal indicative of the desired flow demand and a fuel pressure signal indicative of the desired fuel pressure to a fuel supply system control in a fuel metering unit;
the fuel supply system including a pump connected to a fuel tank, a metering valve downstream of said pump; and
said fuel supply system control separate from the engine controller and programmed to control at least one of said pump and said metering valve, said fuel supply system control operable to take in the flow demand signal and the fuel pressure signal from the engine controller, and identify operation conditions for said at least one of said pump and said metering valve to achieve the desired flow volume and the desired fuel pressure; and
said pump including a motor, and the fuel supply system control further being programmed and operable to control the motor to achieve a desired speed of the pump.

2. The combined gas turbine engine and fuel supply system as set forth in claim 1 , wherein said fuel supply system is line replaceable and is received within a housing.

3. The combined gas turbine engine and fuel supply system as set forth in claim 2 , wherein said pump is a variable displacement pump.

4. The combined gas turbine engine and fuel supply system as set forth in claim 3 , wherein said variable displacement pump is a piston pump.

5. The combined gas turbine engine and fuel supply system as set forth in claim 3 , wherein said variable displacement pump is a vane pump.

6. The combined gas turbine engine and fuel supply system as set forth in claim 1 , wherein said fuel supply system includes a sharing valve and a plurality of pumps.

7. The combined gas turbine engine and fuel supply system as set forth in claim 1 , wherein the fuel supply system control controls the said pump based upon the flow demand signal and the fuel pressure signal from the engine controller, and the engine controller directly controlling the metering valve.

8. The combined gas turbine engine and fuel supply system as set forth in claim 1 , wherein the fuel supply system control is an electronic control.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Goy Edward W
• Shook Ryan
• Harder Benjamin T

Classifications

• F02C9/263 Primary

  by means of fuel metering valves · CPC title

• F02C9/30

  characterised by variable fuel pump output · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F02C9/28

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

• F05D2270/301

  Pressure · CPC title