Direct injection multipoint nozzle

Patent metadata

Field	Value
Publication number	US-9810186-B2
Application number	US-201314758633-A
Country	US
Kind code	B2
Filing date	Dec 31, 2013
Priority date	Jan 2, 2013
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

Provided is an injector ( 30 ) having a plurality of injector modules ( 44 ) that include a spray cup having a chamber and a plurality of radial air passages for directing air radially into the chamber, and a pressure swirl atomizer attached to the spray cup and having a fluid passage for directing fluid axially into chamber and an air passage for directing air axially into the chamber. By providing radial and axial air flow and axial fuel flow into the chamber, the fuel may be mixed to prevent local hot spots that lead to high NOx emissions, and a stable flame may be maintained without autoignition and flashback. The axial air flow also prevents recirculation zones from forming at a base of the spray cup, provides improved atomization and enhanced combustion.

First claim

What is claimed is:

1. An injector including:
a housing having a fluid channel for fluid;
a plurality of injector modules fluidly connected to the fluid channel, each injector module including:
a spray cup having first and second open ends, a chamber defined between the ends, and a plurality of radial air passages extending through the spray cup for directing air radially inwardly into the chamber; and
a pressure swirl atomizer attached to the spray cup at the first end, the pressure swirl atomizer including a body having a tip extending into the chamber, a fluid passage extending through the body for directing fluid in an axial direction into the chamber, and at least one air passage radially outwardly spaced from the fluid passage for directing air in the axial direction into the chamber; and

a heatshield assembled to a downstream end of each injector module, the heatshield including a body for protecting the injector modules from combustion heat and a plurality of apertures located so as to allow the fluid from a corresponding injector module to be dispensed from the spray cup;
wherein the plurality of apertures are spaced along a length of the heatshield in a direction perpendicular to the axial direction, and
wherein the plurality of injector modules are spaced from one another in the direction perpendicular to the axial direction along the length of the heatshield such that the injector modules float radially relative to an adjacent one of the plurality of injector modules.

2. The injector according to claim 1 , wherein the injector modules are configured to float axially and/or transversely.

3. The injector according to claim 1 , wherein the heatshield includes a plurality of segments each including a plurality of apertures spaced along a length of the segment, wherein the segments are oriented in a side-by-side arrangement.

4. The injector according to claim 1 , wherein an axial gap is provided between the heatshield and the second end of each of the spray cups.

5. The injector according to claim 1 , wherein the heatshield includes a plurality of cooling holes extending through the body of the heatshield.

6. The injector according to claim 1 , wherein each pressure swirl atomizer has a first end attached to the housing and a second end attached to the first end of the respective spray cup.

7. The injector according to claim 1 , wherein the at least one air passage of each pressure swirl atomizer includes a plurality of circumferentially spaced air passages.

8. The injector according to claim 7 , wherein each pressure swirl atomizer includes a plurality of projections extending radially outwardly from the body, and wherein the air passages are formed between adjacent ones of the plurality of projections.

9. The injector according to claim 7 , wherein the plurality of projections are angled relative to the axis of the spray cup to swirl the air in the air passage.

10. The injector according to claim 1 , wherein the plurality of radial air passages of each spray cup are circumferentially spaced.

11. The injector according to claim 10 , wherein the plurality of circumferentially spaced radial air passages include a plurality of sets of circumferentially spaced passages axially spaced from one another.

12. The injector according to claim 1 , wherein the tip of each pressure swirl atomizer is conical.

13. The injector according to claim 1 , wherein the air from the radial air passages and the axial air passage of each injector module combines with the fluid from the respective fluid passage and is directed out of the spray cup through the second open end.

14. The injector according to claim 1 , wherein each pressure swirl atomizer includes an inner body defining the fluid passage and an outer body surrounding the inner body, the outer body being attached to the first end of the spray cup.

15. The injector according to claim 14 , wherein a heatshield gap is provided between the inner and outer bodies to shield the fluid in the fluid passage to isolate the fluid from air surrounding the outer body.

16. The injector according to claim 1 , wherein the heatshield has grooves, and the downstream ends of the injector modules are slidably disposed in the grooves.

17. An injector comprising:
a housing having a fluid channel for fluid;
a plurality of injector modules fluidly connected to the fluid channel, each injector module including:
a spray cup having first and second open ends, a chamber defined between the ends, and a plurality of radial air passages extending through the spray cup for directing air radially inwardly into the chamber; and
a pressure swirl atomizer attached to the spray cup at the first end, the pressure swirl atomizer including a body having a tip extending into the chamber, a fluid passage extending through the body for directing fluid in an axial direction into the chamber, and at least one air passage radially outwardly spaced from the fluid passage for directing air in the axial direction into the chamber; and

a heatshield assembled to a downstream end of each injector module, the heatshield including a body for protecting the injector modules from combustion heat and a plurality of apertures located so as to allow the fluid from a corresponding injector module to be dispensed from the spray cup;
wherein the plurality of apertures are spaced along a length of the heatshield in a direction perpendicular to the axial direction;
wherein the plurality of injector modules are spaced from one another in the direction perpendicular to the axial direction along the length of the heatshield such that the injector modules float radially relative to an adjacent one of the plurality of injector modules; and
wherein each spray cup includes a flange extending radially outwardly from the second end.

18. The injector according to claim 17 , wherein the flange includes a plurality of air cooling holes for stagnation flow.

19. An injector comprising:
a housing having a fluid channel for fluid;
a plurality of injector modules fluidly connected to the fluid channel, each injector module including:
a spray cup having first and second open ends, a chamber defined between the ends, and a plurality of radial air passages extending through the spray cup for directing air radially inwardly into the chamber; and
a pressure swirl atomizer attached to the spray cup at the first end, the pressure swirl atomizer including a body having a tip extending into the chamber, a fluid passage extending through the body for directing fluid in an axial direction into the chamber, and at least one air passage radially outwardly spaced from the fluid passage for directing air in the axial direction into the chamber; and

a heatshield assembled to a downstream end of each injector module, the heatshield including a body for protecting the injector modules from combustion heat and a plurality of apertures located so as to allow the fluid from a corresponding injector module to be dispensed from the spray cup;
wherein the plurality of apertures are spaced along a length of the heatshield in a direction perpendicular to the axial direction;
wherein the plurality of injector modules are spaced from one another in the direction perpendicular to the axial direction along the length of the heatshield such that the injector modules float radially relative to an adjacent one of the plurality of injector modules; and
wherein each spray cup diverges from the first end to the second end.

Assignees

• Parker Hannifin Corp

Inventors

• Mansour Adel B
• Teter Michael
• Steinthorsson Erlendur
• Hollon Brian P
• Lehtinen Jeffery R
• Ras Raman

Classifications

• F23D2900/11002

  Liquid fuel burners with more than one nozzle · CPC title

• F02M53/08

  with air cooling · CPC title

• F23R3/28 Primary

  characterised by the fuel supply (burners F23D) · CPC title

• F23D11/103 Primary

  with means creating a swirl inside the mixing chamber · CPC title

• F02M53/046 Primary

  with thermally-insulating means · CPC title