System and method for purging a fuel manifold of a gas turbine engine using a flow divider assembly

Patent metadata

Field	Value
Publication number	US-11846236-B2
Application number	US-202217836510-A
Country	US
Kind code	B2
Filing date	Jun 9, 2022
Priority date	May 15, 2019
Publication date	Dec 19, 2023
Grant date	Dec 19, 2023

Abstract

Methods and systems of operating a gas turbine engine in a low-power condition are provided. In one embodiment, the method includes supplying fuel to the combustor by supplying fuel to the first fuel manifold via a first flow divider valve and supplying fuel to the second fuel manifold via a second flow divider valve. While supplying fuel to the combustor by supplying fuel to the first fuel manifold, the method includes stopping supplying fuel to the second fuel manifold and supplying pressurized gas to the second fuel manifold via the second flow divider valve to flush fuel in the second fuel manifold into the combustor and hinder coking in the second fuel manifold and associated nozzles.

First claim

What is claimed is:

1. A fuel system of a gas turbine engine, the fuel system comprising:
a first fuel manifold fluidly connected to a combustor of the gas turbine engine;
a second fuel manifold fluidly connected to the combustor; and
a flow divider assembly actuatable between a first configuration and a second configuration, the flow divider assembly including:
a first flow divider valve, in the first and second configurations of the flow divider assembly, configured to supply fuel to the first fuel manifold;
a second flow divider valve, in the first configuration of the flow divider assembly, configured to supply fuel to the second fuel manifold, and in the second configuration of the flow divider assembly, configured to stop supplying fuel to the second fuel manifold; and
a purge valve, in the second configuration of the flow divider assembly, discharging pressurized gas to the second fuel manifold via the second flow divider valve to flush fuel in the second fuel manifold into the combustor,

wherein the first and second flow divider valves are operatively disposed in series between a fuel inlet and a fuel outlet to the second fuel manifold.

2. The fuel system of claim 1 , wherein the purge valve, the first flow divider valve and the second flow divider valve are disposed inside a common housing including:
one or more fuel inlets configured to supply fuel to the first and second flow divider valves;
a first fuel outlet for establishing fluid communication between the first flow divider valve and the first fuel manifold; and
a second fuel outlet for establishing fluid communication between the second flow divider valve and the second fuel manifold.

3. The fuel system of claim 2 , comprising a regulator configured to regulate the pressurized gas supplied to the second flow divider valve, the regulator being disposed inside the common housing.

4. The fuel system of claim 2 , comprising a calibrated orifice to restrict a flow of the pressurized gas to the second flow divider valve, the calibrated orifice being disposed inside the common housing.

5. The fuel system of claim 2 , wherein the first and second flow divider valves are spool-type valves.

Assignees

• Pratt & Whitney Canada

Inventors

• Saintignan Cédric
• Cirtwill Joseph Daniel Maxim
• Mccaldon Kian
• Waddleton David
• Tremblay Marc-André
• Broccolini Ignazio
• Tarling Stephen

Classifications

• F02C7/30 Primary

  Preventing corrosion {or unwanted deposits} in gas-swept spaces · CPC title

• F02C6/00

  Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use · CPC title

• F02C6/16

  for storing compressed air · CPC title

• F02C7/222

  Fuel flow conduits, e.g. manifolds · 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