Return flow powered turbine

Patent metadata

Field	Value
Publication number	US-10267237-B2
Application number	US-201615067921-A
Country	US
Kind code	B2
Filing date	Mar 11, 2016
Priority date	Mar 12, 2015
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

A fuel system for an aircraft is provided having an improved fluid circuit and method of operation. Un-burnt fuel is directed via a return loop towards a fuel tank reservoir. A turbine is located in the return loop and upstream from the fuel tank. The pressurized un-burnt fuel energizes the turbine and the fuel passes to the fuel tank. The turbine is harnessed to a generator for providing a power.

First claim

What is claimed as new and desired to be protected by Letters Patent of the United States is:

1. A fluid circuit for providing fuel to a gas turbine engine comprising:
a fuel supply tank;
a pressurized fuel supply circuit that receives fuel stored in the fuel supply tank and delivers pressurized fuel to a combustor;
a return fuel circuit that redirects un-burnt fuel away from the combustor and towards the fuel supply tank;

a pressure regulating valve (PRV) disposed within the return fuel circuit for controlling fuel flow within the return fuel circuit;
a turbine disposed within the return fuel circuit downstream of the PRV and upstream of the fuel supply tank; and
a metering valve disposed within the fuel supply circuit, wherein the return fuel circuit is connected to the fuel supply circuit upstream of the metering valve to redirect un-burnt fuel away from the combustor, and the return fuel circuit is connected to the fuel supply circuit downstream of the metering valve via a bypass path that delivers un-burnt fuel away from the combustor and towards the fuel supply tank.

2. The fluid circuit as claimed in claim 1 , further comprising at least one pump located within the fuel supply circuit for advancing pressurized fuel towards the combustor.

3. The fluid circuit as claimed in claim 1 , wherein the PRV has an inlet communicating with the fuel supply circuit upstream of the metering valve and another inlet communicating with the fuel supply circuit downstream of the metering valve via the bypass path, the PRV structured and arranged to redirect a flow of un-burnt fuel downstream towards the turbine.

4. The fluid circuit as claimed in claim 1 , further comprising a generator that is powered by the turbine, the generator has an output that provides electrical power to a power using device when the turbine is propelled by the un-burnt fuel received from the return fuel circuit.

5. The fluid circuit as claimed in claim 4 , further comprising a shaft connecting an output of the turbine to the generator, and wherein the turbine has an outlet for delivering un-burnt fuel to the fuel supply tank.

6. The fluid circuit as claimed in claim 5 , further comprising a low pressure pump disposed in the fuel supply circuit downstream of the fuel supply tank and a high pressure pump disposed in the fuel supply circuit downstream of the low pressure pump.

7. The fluid circuit as claimed in claim 6 , further comprising a booster pump disposed within the fuel supply tank for providing pressurized fuel to the fuel supply circuit.

8. A gas turbine engine comprising the fluid circuit as claimed in claim 1 , wherein the pressurized un-burnt fuel propels the turbine.

9. A fuel system for providing fuel to a power plant comprising:
a fuel tank;
a fuel supply line that delivers pressurized fuel stored in the fuel tank to a combustor;
a return fuel line that redirects un-burnt fuel away from the combustor and towards the fuel tank;
a metering valve disposed in the fuel supply line;

a turbine located within the return fuel line upstream of the fuel tank, the turbine having an inlet that receives a flow of un-burnt fuel conveyed through the return fuel line and an outlet that delivers un-burnt fuel to the fuel tank;
a generator operably connected to the turbine, the generator having an output that provides electrical power to a power consuming device;
wherein the turbine is propelled by the flow of un-burnt fuel and energizes the generator for providing electrical power to the power consuming device; and
wherein the return fuel line is connected to the fuel supply line upstream of the metering valve to redirect un-burnt fuel away from the combustor, and wherein the return fuel line has a bypass path connected to the fuel supply line downstream of the metering valve that delivers un-burnt fuel away from the combustor and towards the fuel tank.

10. The fuel system as claimed in claim 9 , further comprising a pressure regulating valve (PRV) disposed within the return fuel line and that controls fuel flow within the return fuel line, the PRV having a port that receives un-burnt fuel from the fuel supply line upstream of the metering valve and another port that receives un-burnt fuel via the bypass path from the fuel supply line downstream of the metering valve, and wherein the PRV is disposed upstream of the turbine.

11. The fuel system as claimed in claim 10 , wherein the PRV is structured and arranged to direct the un-burnt fuel downstream to the turbine based on demand requirements of the power plant.

12. The fuel system as claimed in claim 9 , wherein the turbine is connected to the generator via a shaft and has an output for delivering power to the shaft when the turbine is propelled by the flow of un-burnt fuel.

13. The fuel system as claimed in claim 9 , further comprising a first pump and a second pump disposed in the fuel supply line downstream of the fuel tank, the second pump disposed downstream of the first pump and upstream of the metering valve, wherein the metering valve receives pressurized fuel from the second pump.

14. A method of generating electrical power from a fuel circuit comprising the following steps:
supplying fuel to a fuel supply line;
pressurizing the fuel within the fuel supply line;
throttling pressurized fuel via a metering valve disposed in the fuel supply line so fuel flow and pressure is at a predetermined value;
introducing fuel via the fuel supply line into an engine;
redirecting un-burnt fuel from the fuel supply line to a return fuel line where a turbine is propelled;
creating power with the turbine; and
exiting the un-burnt fuel from turbine to a reservoir;
wherein redirecting un-burnt fuel from the fuel supply line to the return fuel line includes directing a flow of the un-burnt fuel to the return fuel line from the fuel supply line upstream of the metering valve and guiding a bypass flow of the un-burnt fuel to the return fuel line from the fuel supply line downstream of the metering valve.

15. The method of generating electrical power as claimed in claim 14 , wherein creating power with the turbine includes the turbine powering a generator which in turn outputs electrical power.

16. The method of generating electrical power as claimed in claim 14 , further comprising the step of regulating the fuel pressure in the return fuel line.

17. The method of generating electrical power as claimed in claim 14 , wherein the step of redirecting un-burnt fuel from the fuel supply line to the return fuel line further includes introducing the un-burnt fuel into a pressure regulation valve (PRV) and directing via the PRV a downstream flow of the un-burnt fuel towards the reservoir based on demand requirements of the engine, the PRV having an inlet for receiving the flow of the un-burnt fuel from the fuel supply line upstream of the metering valve and another inlet for receiving the bypass flow of the un-burnt fuel from the fuel supply line downstream of the metering valve.

18. The method of generating electrical power as claimed in claim 17 , wherein directing via the PRV the downstream flow of the un-burnt fuel towards the reservoir includes redirecting the downstream flow of the un-burnt fuel to the turbine, and wherein creating power with the turbine includes propelling the turbine via the downstream flow of the un-burnt fuel and transferring power from the turbine to a generator that outputs electrical power.

Assignees

• Rolls Royce Corp

Inventors

• Pool Andrew J
• Rubel Joel M
• Patzer Perry J
• Hollander Stephen E

Classifications

• F05D2270/07

  to improve fuel economy · CPC title

• F05D2220/76

  an electrical generator · CPC title

• F05D2220/62

  with energy recovery turbines · CPC title

• F02C9/38

  characterised by throttling and returning of fuel to sump · CPC title

• F02C9/263 Primary

  by means of fuel metering valves · CPC title