Methods and systems for a fuel injector

Patent metadata

Field	Value
Publication number	US-11045776-B2
Application number	US-201816109383-A
Country	US
Kind code	B2
Filing date	Aug 22, 2018
Priority date	Aug 22, 2018
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

Methods and systems are provided for a fuel injector. In one example, a system may include an injection nozzle having a venturi shape with an upstream twisted fin arranged in a venturi inlet. The system may further include a downstream twisted fin arranged in a venturi outlet.

First claim

The invention claimed is:

1. A system, comprising:
an injector having a venturi-shaped nozzle, wherein the nozzle comprises a plurality of upstream twisted fins arranged in a venturi inlet of the nozzle, and where a leading edge of an upstream twisted fin of the plurality of upstream twisted fins is perpendicular to a trailing edge of the upstream twisted fin, and further comprising a plurality of downstream twisted fins, wherein the pluralities of upstream and downstream twisted fins do not extend into a venturi throat.

2. The system of claim 1 , wherein the nozzle further comprises the plurality of downstream twisted fins arranged in a venturi outlet of the nozzle, and where the plurality of downstream twisted fins is identical to the plurality of upstream twisted fins in shape.

3. The system of claim 2 , wherein a leading edge of a downstream twisted fin of the plurality of downstream twisted fins is oriented at an angle relative to the leading edge of the upstream twisted fin of the plurality of upstream twisted fins.

4. The system of claim 3 , wherein the angle is equal to 45°.

5. The system of claim 2 , wherein a width of each of the plurality of downstream twisted fins is equal to 40% of a greatest diameter of the venturi outlet, and where a diameter of the venturi outlet increases in a downstream direction.

6. The system of claim 1 , wherein a venturi throat of the nozzle is arranged between the venturi inlet and a venturi outlet, and where the plurality of upstream twisted fins do not extend into the venturi throat.

7. The system of claim 1 , wherein a diameter of the venturi inlet decreases in a downstream direction, and where a width of each of the plurality of upstream twisted fins decreases in the downstream direction, and where the width is equal to 40% of a greatest diameter of a venturi outlet.

8. The system of claim 1 , wherein the plurality of upstream twisted fins is oriented to impart a counterclockwise or clockwise swirl onto a fuel mixture flow.

9. The system of claim 1 , wherein the venturi-shaped nozzle is a single nozzle of a plurality of venturi-shaped nozzles evenly distributed along a surface of a tip of the injector, and where the surface is curved.

10. An injector, comprising:
a tip including at least one injection nozzle comprising a venturi throat arranged between a venturi inlet and a venturi outlet, and where the venturi inlet comprises at least one upstream twisted fin and the venturi outlet comprises at least one downstream twisted fin spaced away from the at least one upstream twisted fin; and
an air entrainment system fluidly coupled to an extreme end of the venturi outlet and the venturi throat, and where the air entrainment system is arranged completely outside of the at least one injection nozzle, wherein the air entrainment system comprises two or more air entrainment passages directly fluidly coupled to a chamber, where the chamber extends around an entire circumference of the venturi throat.

11. The injector of claim 10 , wherein the air entrainment system comprises two or more air entrainment passages directly fluidly coupled to the venturi throat.

12. The injector of claim 10 , wherein the chamber comprises two openings arranged in 180° across from one another, the two openings fluidly coupling the chamber to the venturi throat.

13. The injector of claim 10 , wherein the chamber comprises a trapezoidal cross-section, and where an upper diameter of the venturi outlet is larger than a lower diameter of the venturi inlet.

14. The injector of claim 10 , wherein the at least one upstream twisted fin is one of four total upstream twisted fins, and where the at least one downstream twisted fin is one of four total downstream twisted fins, and where the downstream twisted fins and upstream twisted fins are angled and radially offset with one another.

15. A fuel injector, comprising:
a curved tip comprising a central nozzle arranged along a central axis, a plurality of inner ring nozzles arranged around the central axis via a first diameter, a plurality of middle ring nozzles arranged around the central axis via a second diameter, and a plurality of outer ring nozzles arranged around the central axis via a third diameter, and where each of the pluralities of inner, middle, and outer ring nozzles are angled relative to the central axis, wherein one or more of the central nozzle and the pluralities of inner, middle, and outer rings nozzles comprises a venturi throat arranged between a venturi inlet and a venturi outlet, and where the venturi inlet comprises at least one upstream twisted fin, and where the venturi outlet comprises at least one downstream twisted fin, and where the at least one downstream twisted fin is misaligned with the at least one upstream twisted fin relative to a general direction of fuel mixture flow.

16. The fuel injector of claim 15 , wherein the first diameter is less than the second diameter, and where the second diameter is less than the third diameter, and where the inner ring nozzles are sized uniformly and evenly distributed, and where the middle ring nozzles are sized uniformly and evenly distributed, and where the outer ring nozzles are sized uniformly and evenly distributed.

17. The fuel injector of claim 15 , wherein the plurality of inner ring nozzles is smaller than the central nozzle, and where the central nozzle is smaller than each of the plurality of outer ring nozzles, and where the plurality of outer ring nozzles is smaller than each of the plurality of middle ring nozzles.

18. The fuel injector of claim 15 , wherein a number of the plurality of inner ring nozzles is equal to 10, and where a number of the plurality of middle ring nozzles is equal to 10, and where a number of the plurality of outer ring nozzles is equal to 10, and where the plurality of inner ring nozzles, the plurality of middle ring nozzles, and a first half of the plurality of outer ring nozzles are radially aligned, and where a second half of the plurality of outer ring nozzles are radially misaligned with the plurality of inner ring nozzles and the plurality of middle ring nozzles.

Assignees

• Ford Global Tech Llc

Inventors

• Zhang Xiaogang
• Basmaji Joseph
• Yi Jianwen James
• Meinhart Mark

Classifications

• B01F25/31252

  Nozzles · CPC title

• B01F25/31241 Primary

  the main flow being injected in the circumferential area of the venturi, creating an aspiration in the central part of the conduit · CPC title

• B01F25/312532

  Profiled, grooved, ribbed discharge conduit, or being provided with baffles · CPC title

• B01F25/312512

  Profiled, grooved, ribbed throat, or being provided with baffles · CPC title

• B01F25/31242

  the main flow being injected in the central area of the venturi, creating an aspiration in the circumferential part of the conduit (B01F25/31243 takes precedence) · CPC title