Combustion staging system

Patent metadata

Field	Value
Publication number	US-10982858-B2
Application number	US-201816011741-A
Country	US
Kind code	B2
Filing date	Jun 19, 2018
Priority date	Jun 23, 2017
Publication date	Apr 20, 2021
Grant date	Apr 20, 2021

Abstract

A combustion staging system is provided for fuel injectors of a multi-stage combustor of a gas turbine engine. The system has a splitting unit which receives a metered total fuel flow and controllably splits the metered total fuel flow into out-going pilot and mains fuel flows to perform pilot-only and pilot-and-mains staging control of the combustor. The splitting unit includes a metering valve and a spill valve, a first portion of the total metered fuel flow received by the splitting unit being an inflow to the metering valve and a second portion of the total metered fuel flow received by the splitting unit being an inflow to the spill valve. The metering valve is configured to controllably determine a fuel flow rate of a metered outflow formed from the first portion of the total metered fuel flow.

First claim

What is claimed is:

1. A combustion staging system for fuel injectors of a multi-stage combustor of a gas turbine engine, the system comprising:
a splitting unit which receives a metered total fuel flow and controllably splits the metered total fuel flow into a pilot fuel flow, which is out-going, and a mains fuel flow, which is out-going, to perform pilot-only staging control or pilot-and-mains staging control of the combustor, wherein for the pilot-only staging control only the pilot fuel flow is formed from the metered total fuel flow by the splitting unit, and for the pilot-and-mains staging control both the pilot fuel flow and the mains fuel flow are formed from the metered total fuel flow by the splitting unit;
a allot fuel manifold to receive the pilot fuel flow and a mains fuel manifold to receive the mains fuel flow;
wherein the splitting unit includes a metering valve and a spill valve, a first portion of the metered total fuel flow received by the splitting unit being an inflow to the metering valve and a second portion of the metered total fuel flow received by the splitting unit being an inflow to the spill valve, the metering valve being configured to controllably determine a fuel flow rate of a metered outflow as the first portion of the metered total fuel flow, the spill valve being configured to produce a spilled outflow as the second portion of the metered total fuel flow, and the spill valve being further configured to sense a pressure differential between the inflow to the metering valve and the metered outflow from the metering valve and to vary the amount of the spilled outflow in response to the sensed pressure differential, whereby the metered outflow forms the mains fuel flow, and the spilled outflow forms the pilot fuel flow; and
wherein the splitting unit sends a cooling flow to the mains fuel manifold during the pilot-only operation.

2. A combustion staging system according to claim 1 , wherein the metering valve has a spool whose position is controllable to determine the fuel flow rate of the metered outflow.

3. A combustion staging system according to claim 2 , wherein the metering valve further has a device to measure the position of the spool.

4. A combustion staging system according to claim 1 , wherein the system further has a mains cooling valve which, during the pilot-only operation, opens a bypass connection between the mains fuel manifold and the pilot fuel manifold such that the cooling flow passes from the mains fuel manifold to the pilot fuel manifold.

5. A combustion staging system according to claim 4 , wherein the spill valve sends some or all of the cooling flow to the mains fuel manifold during the pilot-only operation.

6. A combustion staging system according to claim 5 , wherein the spill valve receives a third portion of the metered total fuel flow and forms some or all of the cooling flow therefrom.

7. A combustion staging system according to claim 4 , wherein the system further has a non-return valve in the bypass connection which prevents flow in a direction from the pilot fuel manifold to the mains fuel manifold.

8. A combustion staging system according to claim 1 , the staging system further having a plurality of mains flow scheduling valves which distribute the mains fuel flow from the mains manifold to mains discharge orifices of a res ective iniector of the fuel injectors of the combustor.

9. A combustion staging system according to claim 8 , wherein each of the plurality of mains flow scheduling valves has a chamber contain ng a movable piston, the chamber to a mains side of the piston being in fluid communication with the mains fuel manifold, the piston being biased towards a closed pilot-only position which prevents flow out of the mains side of the chamber to the mains discharge orifice of the respective injector, and the piston being movable under an increase in pressure in the mains fuel manifold to an open pilot-and-mains position which allows the flow out of the mains side of the chamber to the mains discharge orifice of the respective injector.

10. A combustion staging system according to claim 8 , wherein the mains flow scheduling valves also pass the pilot fuel flow from the pilot manifold to pilot discharge orifices of the respective injector.

11. A combustion staging system according to claim 10 , wherein the chamber to a pilot side of the piston is in fluid communication with the pilot fuel manifold.

12. A fuel supply system having:
a fuel metering valve which is configured to receive a flow of pressurised fuel and to form therefrom the metered total fuel flow; and
the combustion staging system according to claim 1 , the splitting unit of the combustion staging system receiving the metered total fuel flow from the fuel metering valve.

13. A gas turbine engine having the fuel supply system according to claim 12 .

Assignees

• Rolls Royce Plc

Inventors

• Bickley Daniel J

Classifications

• F02C7/228 Primary

  Dividing fuel between various burners · CPC title

• F02C9/263

  by means of fuel metering valves · CPC title

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title

• F02C9/266

  specially adapted for gas turbines with intermittent fuel injection · CPC title

• F23R3/346 Primary

  for staged combustion · CPC title