Claims
- 1. A method of forming an injector assembly, comprising the steps of:etching a fuel swirl chamber in a first thin plate of etchable material, said fuel swirl chamber having a shape such that fluid to be sprayed can move therein in a vortex motion toward the center of the fuel swirl chamber; and etching a spray orifice which extends through the thin section of material at the center of the fuel swirl chamber such that fluid to be sprayed can move from said fuel swirl chamber to said spray orifice and then exit the spray orifice in a conically-shaped spray; and providing at least one fuel feed slot in fluid communication with the fuel swirl chamber and which extends non-radially to said fuel swirl chamber for supplying fuel to be sprayed through the injector assembly; and etching a cylindrical air swirler passage in a second thin plate of etchable material, and locating the second plate in adjacent relation to the second side of the first plate such that the cylindrical air swirler passage is located in co-axial relation to the spray orifice of the fuel swirler passage such that fuel directed through the spray orifice passes through the air swirl passage and swirling air can be imparted to the fuel to cause the fuel to have a swirling component of motion; and providing at least one air feed slot in fluid communication with the air swirler passage and extending in non-radial relation thereto for supplying air to the air swirler passage.
- 2. The method as in claim 1, further including the step of etching the at least one air feed slot in the second plate.
- 3. The method as in claim 1, further including the steps of etching cylindrical air swirler passages in multiple thin plates of etchable material, and locating the multiple air swirler plates in stacked relation with each other and with the first plate, each of the air swirler plates having a portion of the air swirler passages, with the plates arranged such that the air swirler passage portions are arranged in co-axial relation with one another and with the spray orifice of the fuel swirler passage, and each of the air swirler plates including at least one air feed slot in fluid communication with a respective air swirler passage portion and extending in non-radial relation thereto for supplying multiple air streams to be swirled in the respective air swirler passage.
- 4. The method as in claim 3, further including providing an air supply passage to feed all the at least one feed slots of the multiple air swirler plates.
- 5. The method as in claim 4, further including forming the air supply passage axially through the multiple air swirler plates.
- 6. The method as in claim 1, further including providing an air supply passage in fluid communication with the at least one air feed slot, the air supply passage extending in axial relation thereto for supplying air to the at least one air feed slot.
- 7. The method as in claim 1, including etching the first and second plates from a metal.
- 8. A method of forming an injector assembly, comprising the steps of:etching a swirl chamber in a first thin plate of etchable material, said swirl chamber having a shape such that a first to be sprayed can move therein in a vortex motion toward the center of the swirl chamber; and forming a spray orifice which extends through the thin section of material at the center of the swirl chamber such that the first fluid to be sprayed can move from said swirl chamber to said spray orifice and then exit the spray orifice in a conically-shaped spray; and providing at least one feed slot in fluid communication with the swirl chamber and which extends non-radially to said swirl chamber for supplying the first fluid to be sprayed through the injector assembly; and etching a cylindrical swirler passage in a second thin plate of etchable material, and locating the second plate in stacked relation relative to the first plate such that the cylindrical swirler passage is located in co-axial relation to the spray orifice of the swirler passage such that the first fluid directed through the spray orifice passes through the swirl passage and swirling second fluid can be imparted to the first fluid to cause the first fluid to have a swirling component of motion; and providing at least one second fluid feed slot in fluid communication with the swirler passage and extending in non-radial relation thereto for supplying the second fluid to the swirler passage.
- 9. A method of forming an injector assembly, comprising the steps of:providing a metering set including a first thin plate of etchable material, a first feed slot for supplying a first fluid to the first plate, and an orifice for dispensing the first fluid in a spray; and etching a cylindrical swirler passage in a second thin plate of etchable material, and locating the second plate in stacked relation relative to the first plate such that the cylindrical swirler passage is located in co-axial relation to the spray orifice such that the first fluid directed through the spray orifice passes through the swirl passage and swirling second fluid can be imparted to the first fluid to cause the first fluid to have a swirling component of motion; and providing at least one second fluid feed slot in fluid communication with the swirler passage and extending in non-radial relation thereto for supplying the second fluid to the swirler passage.
- 10. The method as in claim 1, wherein the at least one air feed slot extends in the plane of the second thin plate of etchable material.
- 11. Tue method as in claim 8, wherein the at least one second feed slot extends in the plane of the second thin plate of etchable material.
- 12. The method as in claim 9, wherein the at least one second fluid feed slot extends in the plane of the second thin plate of etchable material.
CROSS REFERENCE TO RELATED CASES
The present application claims priority to U.S. Provisional Application Ser. No. 60/185,254; filed Feb. 28, 2000.
US Referenced Citations (25)
Foreign Referenced Citations (3)
Number |
Date |
Country |
2 124 554 |
Feb 1994 |
GB |
60-190593 |
Mar 1984 |
JP |
409189490 |
Jul 1997 |
JP |
Provisional Applications (1)
|
Number |
Date |
Country |
|
60/185254 |
Feb 2000 |
US |