Continuous ignition device exhaust manifold

Patent metadata

Field	Value
Publication number	US-11891956-B2
Application number	US-202217835525-A
Country	US
Kind code	B2
Filing date	Jun 8, 2022
Priority date	Dec 16, 2020
Publication date	Feb 6, 2024
Grant date	Feb 6, 2024

Abstract

A torch ignitor system provides a continuous flame to ignite fuel within a combustor of a gas turbine engine. The torch ignitor system includes a manifold and a plurality of torch nozzles to enable the flame or torch to simultaneously ignite multiple fuel nozzles within the combustor of the gas turbine engine.

First claim

The invention claimed is:

1. A torch ignitor system comprising:
a torch ignitor comprising:
a housing;
a plurality of hot surface ignitors coupled to the housing;
a fuel inlet coupled to the housing, wherein the fuel inlet provides a flow path for fuel to enter the housing; and
an air inlet positioned within the housing, wherein the air inlet provides a flow path for air to enter the housing and mix with the fuel entering the housing to create a fuel and air mixture;
wherein the plurality of hot surface ignitors are configured to ignite the fuel and air mixture to create an ignited fuel and air mixture; and

a combustion chamber positioned between and fluidly coupling the torch ignitor to an annular manifold, wherein the combustion chamber includes a hollow center portion to allow the ignited fuel and air mixture to flow to the annular manifold and wherein the annular manifold has a circular cross-section such that the annular manifold is a torus shaped manifold and the annular manifold includes tubular walls such that an interior of the annular manifold is hollow to allow the ignited fuel and air mixture to flow through the annular manifold;
wherein the annular manifold includes a plurality of torch nozzles extending from the annular manifold for expelling the ignited fuel and air mixture, wherein the plurality of torch nozzles are spaced around an outer wall of the annular manifold.

2. The torch ignitor system of claim 1 , wherein each of the plurality of hot surface ignitors are resistance heating elements configured to exceed an ignition temperature of the fuel and air mixture to ignite the fuel and air mixture.

3. The torch ignitor system of claim 1 , wherein a portion of the fuel inlet is positioned outside the housing and another portion of the fuel inlet is positioned within the housing.

4. The torch ignitor system of claim 1 , wherein the air inlet is a metering valve, and wherein the air inlet is configured to receive the air and meter or regulate an amount of the air entering the housing.

5. The torch ignitor system of claim 1 , wherein the combustion chamber is a tube, and wherein the combustion chamber includes an outer body defining the hollow center portion.

6. The torch ignitor system of claim 5 , wherein the outer body includes an inner skin, an outer skin, and a plurality of vanes positioned between the inner skin and the outer skin, and wherein a fluid flow path exists between the inner skin and the outer skin to allow a cooling fluid to flow within the outer body and past the plurality of vanes to reduce a temperature of the combustion chamber.

7. The torch ignitor system of claim 1 , wherein the combustion chamber includes a first end coupled to the torch ignitor and a second end coupled to the annular manifold, and wherein an inner diameter of the first end of the combustion chamber is greater than an inner diameter of the second end of the combustion chamber.

8. The torch ignitor system of claim 1 , wherein a cross-sectional area of the interior of the annular manifold gradually decreases extending from a location where the annular manifold is coupled to the combustion chamber to a location positioned farthest away from the location where the annular manifold is coupled to the combustion chamber.

9. The torch ignitor system of claim 1 , wherein:
the annular manifold comprises a split at a location opposite a location where the combustion chamber is coupled to the annular manifold;
at least one cap is positioned over an aperture created by the split; and
an interior of the annular manifold is blocked from continuous unobstructed flow around the interior of the annular manifold.

10. The torch ignitor system of claim 1 , wherein an outer wall of the annular manifold includes an inner skin, an outer skin, and a plurality of vanes positioned between the inner skin and the outer skin, and wherein a fluid flow path exists between the inner skin and the outer skin to allow a cooling fluid to flow within the outer wall and past the plurality of vanes to reduce a temperature of the annular manifold.

Assignees

• Delavan Inc

Inventors

• Ryon Jason

Classifications

• F02C7/264 Primary

  Ignition · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title

• F05D2260/85

  Starting · CPC title

• F02C7/266

  Electric (sparking plugs H01T) · CPC title