Pre-swirl pressure atomizing tip

Patent metadata

Field	Value
Publication number	US-11149950-B2
Application number	US-201816005371-A
Country	US
Kind code	B2
Filing date	Jun 11, 2018
Priority date	Jun 11, 2018
Publication date	Oct 19, 2021
Grant date	Oct 19, 2021

Abstract

A tip for a nozzle of a fuel injector and an associated method are provided. The tip includes a tip body and a swirler. The swirler includes a plurality of pre-swirl passages which fluidly communicate an internal cavity of the swirler with a feed annulus. The swirler also includes a plurality of swirl chamber passages which fluidly communicate a swirl chamber with the feed annulus. Methods include manufacturing at least a portion of the swirler by additive manufacturing.

First claim

What is claimed is:

1. A tip for a nozzle of a fuel injector, the tip comprising:
a tip body, the tip body defining a longitudinal axis of the tip;
a swirler, situated within the tip body, wherein the swirler includes a plurality of pre-swirl passages, wherein each one of the plurality of pre-swirl passages has a longitudinal axis which extends in both a radial and axial direction relative to the longitudinal axis of the tip;
a feed annulus, wherein the feed annulus receives a flow of fuel from the plurality of pre-swirl passages, wherein the plurality of pre-swirl passages are configured and arranged such that the flow of fuel entering the feed annulus has a flow velocity having a tangential component;
wherein the swirler includes a plurality of swirl chamber passages, the plurality of swirl chamber passages receiving the flow of fuel from the feed annulus, wherein each one of the plurality of swirl chamber passages includes a longitudinal axis which extends from the feed annulus to a swirl chamber in only the radial direction relative to the longitudinal axis of the tip; and
wherein the swirler includes the swirl chamber, the swirl chamber receiving the flow of fuel from the feed annulus via the plurality of swirl chamber passages.

2. The tip of claim 1 , wherein the feed annulus is formed between an interior radially facing surface of the tip body and an exterior radially facing surface of the swirler.

3. The tip of claim 1 , wherein the feed annulus is radially outside of the swirl chamber relative to the longitudinal axis of the tip.

4. The tip of claim 1 , wherein the longitudinal axis of each of the plurality pre-swirl passages extends along a tapered helical path.

5. The tip of claim 1 , wherein the longitudinal axis of each of the plurality of pre-swirl passages extends along a straight path.

6. The tip of claim 1 , wherein the longitudinal axis of each of the plurality of swirl chamber passages is straight.

7. The tip of claim 1 , wherein the longitudinal axis of each of the plurality of swirl chamber passages is curved.

8. The tip of claim 1 , wherein at least a portion of the swirler is formed by additive manufacturing.

9. A tip for a nozzle of a fuel injector, the tip comprising:
a tip body;
a swirler contained within the tip body, wherein the swirler includes an inlet cavity for receiving a flow of fuel entering the tip body;
a feed annulus in fluid communication with the inlet cavity and downstream from the inlet cavity relative to a direction of fuel flow through the tip;
a swirl chamber in fluid communication with the feed annulus and downstream from the feed annulus relative to the direction of fuel flow through the tip;
wherein the feed annulus is formed between an interior radially facing surface of the tip body and an exterior radially facing surface of the swirler; and
wherein the feed annulus is at least one of axially upstream or radially outside of the swirl chamber relative to a longitudinal axis of the tip;
wherein the feed annulus and the swirl chamber are in fluid communication via a plurality of swirl chamber passages, wherein each one of the plurality of swirl chamber passages includes a longitudinal axis which extends from the feed annulus to the swirl chamber in only the radial direction relative to a longitudinal axis defined by the tip.

10. The tip of claim 9 , wherein the inlet cavity and feed annulus are in fluid communication via a plurality of pre-swirl passages, wherein each one of the plurality of pre-swirl passages has a longitudinal axis which extends in both a radial and axial direction relative to a longitudinal axis defined by the tip.

11. The tip of claim 10 , wherein the longitudinal axis of each of the plurality pre-swirl passages extends along one of a tapered helical path or a straight path.

12. The tip of claim 9 , wherein the longitudinal axis of each one of the swirl chamber passages extends along one of a straight or a curved path.

13. The tip of claim 9 , wherein the plurality of pre-swirl passages are configured and arranged such that the flow of fuel entering the feed annulus has a flow velocity having a tangential component.

14. A method of forming a tip for a nozzle of a fuel injector, the method comprising:
providing a swirler;
providing a tip body;
inserting the swirler into a passage of the tip body, the swirler having a plurality of pre-swirl passages and a plurality of swirl chamber passages;
fixing the swirler within the passage of the tip body such that a feed annulus is formed between a radially interior facing surface of the tip body and a radially exterior facing surface of the swirler to place the plurality of pre-swirl passages in fluid communication with the plurality of swirl chamber passages;
wherein each one of the plurality of swirl chamber passages include a longitudinal axis which extends from the feed annulus to a swirl chamber in only the radial direction relative to a longitudinal axis defined by the tip.

15. The method of claim 14 , wherein the step of providing the swirler includes manufacturing at least a portion of the swirler by additive manufacturing.

16. The method of claim 15 , wherein the step of manufacturing at least a portion of the swirler by additive manufacturing includes forming the pre-swirl passages by additive manufacturing.

17. The method of claim 16 , wherein the step of forming the pre-swirl passages by additive manufacturing includes forming the pre-swirl passages such that each one of the pre-swirl passages includes a longitudinal axis which moves along one of a tapered helical path or a straight path.

18. The method of claim 15 , wherein the step of manufacturing at least a portion of the swirler by additive manufacturing includes forming the swirl chamber passages by additive manufacturing.

19. The method of claim 18 , wherein the step of forming the swirl chamber passages by additive manufacturing includes forming the swirl chamber passages such that each one of the swirl chamber passages has a longitudinal axis which moves along one of a straight path or a curved path.

Assignees

• Niemeyer Sander G
• Pyle Deke R
• Woodward Inc

Inventors

• Niemeyer Sander G
• Pyle Deke R

Classifications

• F02M61/162

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

• F23D11/24

  by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space · CPC title

• F23R3/286

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

• F23R2900/00018

  Manufacturing combustion chamber liners or subparts · CPC title

• F23R3/14 Primary

  by using swirl vanes · CPC title