IP Library Granted Patent US 7,506,510
Granted Patent B2
US 7,506,510 · App. 11/333,388 · Granted Mar 24, 2009

System and method for cooling a staged airblast fuel injector

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,506,510
App. No.
11/333,388
Granted
Mar 24, 2009
Kind
B2
Abstract

A staged fuel injector is disclosed that includes a main fuel circuit for delivering fuel to a main fuel atomizer and a pilot fuel circuit for delivering fuel to a pilot fuel atomizer located radially inward of the main fuel atomizer. The pilot fuel circuit is in close proximity to the main fuel circuit enroute to the pilot fuel atomizer so that the pilot fuel flow cools stagnant fuel located within the main fuel circuit during low engine power operation to prevent coking.

Claims (28)

1. A staged fuel injector comprising:

a) a main fuel circuit for delivering fuel to a main fuel atomizer, the main fuel atomizer including a radially outer prefilmer having an outer diametrical surface, wherein portions of the main fuel circuit are formed in the outer diametrical surface of the prefilmer; and

b) a pilot fuel circuit for delivering fuel to a pilot fuel atomizer located radially inward of the main fuel atomizer, wherein portions of the pilot fuel circuit are formed in the outer diametrical surface of the prefilmer, and wherein the pilot fuel circuit is in thermal contact with the main fuel circuit enroute to the pilot fuel atomizer.

2. A staged fuel injector as recited in claim 1 , wherein the main fuel atomizer further includes a radially inner fuel swirler having an outer diametrical surface, and wherein portions of the main fuel circuit are formed in the outer diametrical surface of the fuel swirler.

3. A staged fuel injector as recited in claim 2 , wherein radial passage means extend through the prefilmer to provide communication between the portions of the main fuel circuit formed in the outer diametrical surface of the prefilmer and the portions of the main fuel circuit formed in the outer diametrical surface of the fuel swirler.

4. A staged fuel injector as recited in claim 2 , wherein portions of the pilot fuel circuit are formed in the outer diametrical surface of the fuel swirler.

5. A staged fuel injector as recited in claim 4 , wherein radial passage means extend through the prefilmer to provide communication between the portions of the pilot fuel circuit formed in the outer diametrical surface of the prefilmer and the portions of the pilot fuel circuit formed in the outer diametrical surface of the fuel swirler.

6. A staged fuel injector as recited in claim 5 , wherein a radial passage extends through the fuel swirler to provide communication between the pilot fuel circuit and the pilot atomizer.

7. A staged fuel injector as recited in claim 1 , wherein the main fuel atomizer includes a fuel swirler radially inward of the prefilmer, wherein the main fuel circuit includes a plurality of fuel exit slots formed in the fuel swirler, and wherein the pilot fuel circuit is located in close proximity to the fuel exit slots of the main fuel circuit.

8. A staged fuel injector as recited in claim 7 , wherein the fuel exit slots communicate with a spin chamber formed in the fuel swirler.

9. A staged fuel injector as recited in claim 8 , wherein the spin chamber is configured as a self-draining spin chamber.

10. A staged fuel injector comprising:

a) a main fuel atomizer including a radially outer prefilmer having an outer diametrical surface and a radially inner fuel swirler having an outer diametrical surface;

b) a main fuel circuit formed in the main fuel atomizer and including an outer main fuel circuit portion formed in the outer diametrical surface of the prefilmer and an inner main fuel circuit portion formed in the outer diametrical surface of the inner fuel swirler;

c) a pilot fuel circuit formed in the main fuel atomizer and including an outer pilot fuel circuit portion formed in the outer diametrical surface of the prefilmer and an inner pilot fuel circuit portion formed in the outer diametrical surface of the inner fuel swirler; and

d) a pilot fuel atomizer axially located within the main fuel atomizer, and communicating with the pilot fuel circuit.

11. A staged fuel injector as recited in claim 10 , wherein the pilot fuel circuit is in close proximity to the main fuel circuit such that pilot fuel flow serves to cool stagnant fuel located within the main fuel circuit during low engine power operation, and thereby prevent coking in the main fuel circuit.

12. A staged fuel injector as recited in claim 10 , wherein radial passage means extend through the prefilmer to provide communication between the outer main fuel circuit portion formed in the outer diametrical surface of the prefilmer and the inner main fuel circuit portion formed in the outer diametrical surface of the inner fuel swirler.

13. A staged fuel injector as recited in claim 10 , wherein radial passage means extend through the prefilmer to provide communication between the outer pilot fuel circuit portions formed in the outer diametrical surface of the prefilmer and the inner pilot fuel circuit portions formed in the outer diametrical surface of the inner fuel swirler.

14. A staged fuel injector as recited in claim 10 , wherein radial passage means extend through the inner fuel swirler to provide communication between the inner pilot fuel circuit portions formed in the outer diametrical surface of the inner fuel swirler and the pilot fuel atomizer.

15. A staged fuel injector as recited in claim 10 , wherein the main fuel circuit includes a plurality of fuel exit slots formed in the inner fuel swirler, and wherein the pilot fuel circuit is located in close proximity to the fuel exit slots of the main fuel circuit.

16. A staged fuel injector as recited in claim 15 , wherein the fuel exit slots communicate with a spin chamber formed in the inner fuel swirler.

17. A staged fuel injector as recited in claim 16 , wherein the spin chamber is configured as a self-draining spin chamber.

18. A method of cooling a staged fuel injector comprising:

a) providing a main fuel circuit for delivering fuel to a main fuel atomizer, the main fuel atomizer including a radially outer prefilmer having an outer diametrical surface, wherein portions of the main find circuit are formed in the outer diametrical surface of the prefilmer;

b) providing a pilot fuel circuit for delivering fuel to a pilot fuel atomizer located radially inward of the main fuel atomizer, wherein portions of the pilot fuel circuit are formed in the outer diametrical surface of the prefilmer; and

c) directing fuel through the pilot fuel circuit to cool stagnant fuel located within the main fuel circuit during low engine power operation to prevent coking.

19. A method according to claim 18 , further comprising the step of cooling the fuel flowing through the pilot fuel circuit with fuel flowing through the main fuel circuit during high engine power operation.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 10, 2014
From: DELAVAN INC
To: ROLLS-ROYCE PLC
Reel/Frame 034138/0668 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 17, 2006
From: THOMSON, NEAL A.
To: DELAVAN INC.
Reel/Frame 017488/0277 →