Bluff body fuel mixer

Patent metadata

Field	Value
Publication number	US-9797601-B2
Application number	US-201514601389-A
Country	US
Kind code	B2
Filing date	Jan 21, 2015
Priority date	Jan 21, 2015
Publication date	Oct 24, 2017
Grant date	Oct 24, 2017

Abstract

A combustor is provided. The combustor may include an axial fuel injection system, and a radial fuel injection system aft of the axial fuel injection system. The axial fuel injection system includes a mixer having a bluff body at an exit port of the mixer, and a fuel injector disposed within the mixer. A fuel and air mixer is also provided and comprises an outer housing with an exit port and a bluff body. The bluff body extends across the exit port of the outer housing. A fuel injection system is also provided. The systems comprise a mixer having a bluff body at an exit port of the mixer and a fuel injector disposed within the mixer.

First claim

What is claimed is:

1. A combustor, comprising:
a combustion chamber;
an axial fuel injection system forward of the combustion chamber; and
a radial fuel injection system aft of the axial fuel injection system and configured to deliver fuel into the combustion chamber in a radial direction, the radial fuel injection system comprising:
a mixer having a bluff body at an exit port of the mixer, the bluff body having two surfaces extending between two points on an inner surface of the mixer, wherein the exit port of the mixer is proximal to the combustion chamber, wherein the mixer comprises a flared wall defined by the inner surface, and wherein a first angle formed by the flared wall and a horizontal plane is equal to a second angle formed by a third surface of the bluff body and the horizontal plane; and

a fuel injector disposed within the mixer.

2. The combustor of claim 1 , further comprising a counter swirler disposed around the fuel injector, the counter swirler comprising:
a first set of airfoils oriented in a first circumferential direction; and
a second set of airfoils oriented in a second circumferential direction different from the first circumferential direction.

3. The combustor of claim 1 , wherein the bluff body comprises a v-shaped gutter with an apex of the v-shaped gutter oriented away from the combustion chamber.

4. The combustor of claim 1 , wherein the mixer comprises a cylindrical outer housing.

5. The combustor of claim 1 , further comprising a liner, wherein the radial fuel injection system extends at least partially though the liner.

6. The combustor of claim 5 , further comprising:
a mounting structure coupled to the liner; and
an outer housing of the mixer disposed at least partially within the mounting structure.

7. The combustor of claim 6 , wherein the mixer comprises tabs retained in a slot defined by the mounting structure.

8. The combustor of claim 1 , wherein the bluff body comprises at least one of a circular, multi-radial, squared, or irregularly shaped gutter.

9. A combustor, comprising:
a combustion chamber;
an axial fuel injection system forward of the combustion chamber; and
a radial fuel injection system aft of the axial fuel injection system and configured to deliver fuel into the combustion chamber in a radial direction, the radial fuel injection system comprising:
a mixer having a bluff body at an exit port of the mixer, the bluff body having two sides extending between two points on an inner surface of the mixer, wherein the exit port of the mixer is proximal to the combustion chamber, wherein the mixer comprises a flared wall defined by the inner surface, wherein a third side and a fourth side of the bluff body define a v-shaped gutter with an apex of the v-shaped gutter oriented away from the combustion chamber, and wherein a first distance in a direction parallel to a horizontal plane extending from the inner surface of the mixer to the apex of the bluff body is equal to a second distance in the direction parallel to the horizontal plane extending from the inner surface of the mixer to the third side of the bluff body at the exit port of the mixer, and

a fuel injector disposed within the mixer.

10. The combustor of claim 9 , wherein the mixer comprises a cylindrical outer housing.

11. The combustor of claim 10 , further comprising a liner, wherein the radial fuel injection system extends at least partially through the liner.

12. The combustor of claim 11 further comprising:
a mounting structure coupled to the liner; and
an outer housing of the mixer disposed at least partially within the mounting structure.

13. The combustor of claim 12 , wherein the mixer comprises tabs retained in a slot defined by the mounting structure.

14. The combustor of claim 9 , wherein the mixer comprises an exit radius (R 1 ) at the exit port of the mixer and an inlet radius (R 2 ) at the apex of the bluff body, and wherein the exit radius (R 1 ) is greater than the inlet radius (R 2 ).

15. The combustor of claim 14 , wherein a ratio of the exit radius (R 1 ) to the inlet radius (R 2 ) is between 1.1 to 1 and 1.6 to 1.

16. The combustor of claim 9 , wherein a first angle formed by the flared wall and a horizontal plane is equal to a second angle formed by the third side of the bluff body and the horizontal plane.

Assignees

• United Technologies Corp

Inventors

• Cheung Albert K
• Hoke James B
• Mckinney Randal G

Classifications

• F23R3/34

  Feeding into different combustion zones · CPC title

• F23D11/383

  with swirl means · CPC title

• F23R3/286 Primary

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

• F02M61/162

  Means to impart a whirling motion to fuel upstream or near discharging orifices · CPC title

• F02C7/22

  Fuel supply systems · CPC title