Fuel injector systems

Patent metadata

Field	Value
Publication number	US-2016377293-A1
Application number	US-201514750585-A
Country	US
Kind code	A1
Filing date	Jun 25, 2015
Priority date	Jun 25, 2015
Publication date	Dec 29, 2016
Grant date	—

Abstract

In accordance with at least one aspect of this disclosure, a fuel injector system can include an air mixer defining an outer air circuit, at least one intermediate air circuit, and an inner air circuit. The fuel injector system can also include a fuel manifold defining a fuel circuit, at least a portion of which is operatively disposed within the air mixer such that the fuel circuit and the intermediate air circuit are in fluid communication with each other for atomization of fuel. At least one of the air mixer or the fuel manifold can be additively manufactured.

First claim

What is claimed is:

1 . A fuel injector system comprising:
an air mixer defining an outer air circuit, at least one intermediate air circuit, and an inner air circuit; and a fuel manifold defining a fuel circuit, at least a portion of which is operatively disposed within the air mixer such that the fuel circuit and the intermediate air circuit are in fluid communication with each other for atomization of fuel.

2 . The system of claim 1 , wherein at least one of the air mixer or the fuel manifold is additively manufactured.

3 . The system of claim 1 , wherein the fuel manifold defines a plurality of multipoint injector branches extending from a base portion.

4 . The system of claim 3 , wherein the air mixer defines a plurality of receptacles configured to hold the multipoint injector branches therein.

5 . The system of claim 4 , wherein the receptacles are coaxial with the intermediate air circuit.

6 . The system of claim 3 , wherein each multipoint injector branch includes a metering device disposed on an outlet end thereof to meter fuel into the intermediate air circuit.

7 . The system of claim 3 , wherein the intermediate air circuit includes a diverging section downstream of an outlet end of each multipoint injector branch.

8 . The system of claim 4 , wherein the air mixer includes an outer wall, an intermediate wall, and an inner wall, wherein the outer air circuit is defined between the outer wall and the intermediate wall, wherein the intermediate air circuit is defined between the intermediate wall and the inner wall, and wherein the inner air circuit is defined within the inner wall.

9 . The system of claim 8 , wherein the outer wall and the intermediate wall are separated by outer support members, and wherein the intermediate wall and inner wall are separated from each receptacle with intermediate support members.

10 . The system of claim 9 , wherein the inner air circuit includes a swirler assembly having airfoils defined therein to swirl air therein in an inner swirl direction.

11 . The system of claim 10 , wherein the outer support members and the intermediate support members define an airfoil shape to swirl air in an outer swirl direction and an intermediate swirl direction, respectively.

12 . The system of claim 3 , wherein the base portion of the fuel manifold defines a smooth annular passage defined by non-linear inner walls, wherein the annular passage fluidly connects each multipoint injector branch to a fuel manifold inlet.

13 . The system of claim 1 , further comprising a heat shielding support holding the fuel manifold and the air mixer.

14 . The system of claim 13 , wherein the heat shielding support is brazed or welded to at least one of the air mixer and the fuel manifold.

15 . An air mixer for a fuel injector, defining an outer air circuit, at least one intermediate air circuit, and an inner air circuit.

16 . The air mixer of claim 15 , further defining a plurality of receptacles configured to hold fuel multipoint injector branches therein.

17 . The air mixer of claim 16 wherein the receptacles are coaxial with the intermediate air circuit.

18 . The air mixer of claim 17 , wherein the air mixer includes an outer wall, an intermediate wall, and an inner wall, wherein the outer air circuit is defined between the outer wall and the intermediate wall, wherein the intermediate air circuit is defined between the intermediate wall and the inner wall, and wherein the inner air circuit is defined within the inner wall.

19 . The air mixer of claim 18 , wherein the outer wall and the intermediate wall are separated by outer support members, and wherein the intermediate wall and inner wall are separated from each receptacle with intermediate support members.

20 . The air mixer of claim 19 , wherein the inner air circuit includes a swirler assembly having airfoils defined therein to swirl air therein in an inner swirl direction.

21 . The air mixer of claim 20 , wherein the outer support members and the intermediate support members define an airfoil shape to swirl air in an outer swirl direction and an intermediate swirl direction, respectively.

22 . The air mixer of claim 15 , wherein the intermediate air circuit can include a plurality of circumferentially spaced-apart outlets such that there is one outlet for each multipoint injector branch.

Assignees

• Delavan Inc

Inventors

• Short John E
• Pack Spencer D
• Zink Gregory
• Ryon Jason A
• Khairallah Fouad T

Classifications

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F23R3/286 Primary

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

• F23D11/22

  the gaseous medium being vaporised fuel, e.g. for a soldering lamp · CPC title

• F23R3/12

  inducing a vortex · CPC title

• F23R3/283

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title