Gas turbine engines having fuel injector shrouds with interior ribs

Patent metadata

Field	Value
Publication number	US-9625156-B2
Application number	US-201314067377-A
Country	US
Kind code	B2
Filing date	Oct 30, 2013
Priority date	Oct 30, 2013
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

A fuel injector assembly includes a fuel injector and a fuel injector shroud housing the fuel injector. The fuel injector includes a body and a nozzle coupled to the body. The fuel injector shroud includes a swirler device defining a center opening proximate to the nozzle of the fuel injector and a plurality of swirler holes surrounding the center opening, a body section with an air inlet configured to admit a flow of air into the fuel injector shroud and a dome section defining a mount for securing the swirler device to the body section, and at least one interior rib positioned on an interior surface of the dome section configured to direct the flow of air to the swirler holes of the swirler device such that the flow of air exiting through the swirler is mixed with the flow of fuel exiting the nozzle.

First claim

What is claimed is:

1. A fuel injector assembly, comprising:
a fuel injector comprising a body and a nozzle coupled to the body, the body configured to deliver a flow of fuel to the nozzle; and
a fuel injector shroud housing the fuel injector, the fuel injector shroud comprising
a swirler device defining a center opening proximate to the nozzle of the fuel injector and a plurality of swirler holes surrounding the center opening,
a body section comprising an air inlet configured to admit a flow of air into the fuel injector shroud and a dome section, wherein the dome section defines a mount for securing the swirler device to the body section, and
at least one interior rib positioned on an interior surface of the dome section configured to direct the flow of air to the swirler holes of the swirler device such that the flow of air exiting through the swirler device through the swirler holes is mixed with the flow of fuel exiting the nozzle,

wherein the at least one interior rib is a first interior rib of a plurality of interior ribs, and wherein each of the plurality of interior ribs has an end positioned in between adjacent swirler holes, and
wherein each of the plurality of interior ribs extends from, and is integral with, the dome section.

2. The fuel injector assembly of claim 1 , wherein each of the plurality of interior ribs follows an interior contour of the dome section.

3. The fuel injector assembly of claim 1 , wherein the fuel injector shroud further includes at least one cooling hole extending through the at least one interior rib and the dome section.

4. The fuel injector assembly of claim 1 , wherein the fuel injector shroud includes a bell mouth at the air inlet.

5. The fuel injector assembly of claim 1 , wherein the fuel injector shroud includes a flange extending in a generally axial direction on a radial side of the air inlet.

6. The fuel injector assembly of claim 5 , wherein the flange extends in the generally axial direction into the fuel injector shroud.

7. The fuel injector assembly of claim 5 , wherein the flange extends in the generally axial direction away from the fuel injector shroud.

8. The fuel injection assembly of claim 1 , wherein the plurality of interior ribs is configured to evenly distribute the flow of air into the plurality of swirler holes.

9. The fuel injection assembly of claim 1 , wherein the fuel injector shroud further comprises a body portion with a mounting flange for mounting the fuel injector shroud and a cylindrical section extending from the mounting flange, the dome section extending from the cylindrical section,
wherein the end of the first interior rib positioned in between adjacent swirler holes is a first end, and wherein the first interior rib has a second end positioned on the cylindrical section such that the first rib extends from the second end on the cylindrical section, along the concave length of the dome section generally in the direction of air flow to the first end, proximate to the swirler device.

10. A fuel injector shroud for a fuel injector assembly, comprising:
a swirler device defining a center opening and a plurality of swirler holes surrounding the center opening, each of the plurality of swirler holes extending through the swirler device between an inlet and an outlet;
a body section comprising an air net configured to admit a flow of air into the fuel injector shroud and a dome section, wherein the dome section defines a mount for securing the swirler device to the body section;
at least one interior rib extending from an interior surface of the dome section configured to direct the flow of air to the inlets of the swirler holes of the swirler device; and
wherein the at least one interior rib is a first interior rib of a plurality of interior ribs, and wherein each of the plurality of interior ribs has an end positioned in between adjacent swirler holes.

11. The fuel injector shroud of claim 10 , wherein at least one interior rib of the plurality of interior ribs is integral with the dome section.

12. The fuel injector shroud of claim 10 , wherein at least one interior rib of the plurality of interior ribs follows an interior contour of the dome section.

13. The fuel injector shroud of claim 10 , wherein the fuel injector shroud further includes at least one cooling hole extending through at least one interior rib of the plurality of interior ribs and the dome section.

14. The fuel injector shroud of claim 10 , wherein the fuel injector shroud includes a bell mouth at the air inlet.

15. The fuel injector shroud of claim 10 , further comprising a bellows mounting ring configured to couple the body section to a combustor liner.

16. A method for manufacturing a fuel injector shroud, comprising the steps of: defining a design model of the fuel injector shroud; and using additive manufacturing to form the fuel injector shroud as a unitary piece, including forming:
a swirler device defining a center opening and a plurality of swirler holes surrounding the center opening, each of the plurality of swirler holes extending through the swirler device between an inlet and an outlet;
a body section comprising an air inlet configured to admit a flow of air into the fuel injector shroud and a dome section, wherein the dome section defines a mount for securing the swirler device to the body section;
at least one interior rib extending from an interior surface of the dome section configured to direct the flow of air to the inlets of the swirler holes of the swirler device; and
wherein the at least one interior rib is a first interior rib of a plurality of interior ribs, and wherein each of the plurality of interior ribs has an end positioned in between adjacent swirler holes.

17. The method of claim 16 , wherein the using step includes using direct metal laser fusing as the additive manufacturing.

Assignees

• Honeywell Int Inc

Inventors

• Rudrapatna Nagaraja S
• Bronson Thomas J
• Godfrey Donald G

Classifications

• F23R3/286 Primary

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• B22F10/66

  by mechanical means · CPC title

• B22F10/64

  by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• F23R3/14 Primary

  by using swirl vanes · CPC title