Combustion chamber

• US 6,959,550 B2
• Filed: 12/30/2003
• Issued: 11/01/2005
• Est. Priority Date: 05/15/2001
• Status: Expired due to Term

• Current Assignee: Industrial Turbine Company (UK) Limited (Siemens AG)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Scarinci, Thomas, Day, Ivor J, Freeman, Christopher
• Primary Examiner(s): KIM, TAE JUN
• Application Number:
  US10/747,401
• Publication Number:
  US 20040154301A1
• Time in Patent Office: 672 Days
• Field of Search: 607/25, 607/37, 607/46, 607/47, 607/48
• US Class Current: 60/725
• CPC Class Codes: F23R 3/04 Air inlet arrangements
• CPC Class Codes: F23R 3/286 having fuel-air premixing devices F23R3/30 takes precedence
• CPC Class Codes: F23R 3/346 for staged combustion

Abstract

A three-stage lean burn combustion chamber (28) comprises a primary combustion zone (36), a secondary combustion zone (40) and a tertiary combustion zone (44). Each of the combustion zones (36, 40, 44) is supplied with premixed fuel and air by respective fuel and air mixing ducts (54, 70, 92). The fuel and air mixing ducts (54, 70, 92) have a plurality of air injection slots (62, 64, 76, 98) spaced apart transversely to the direction of flow through the fuel and air mixing ducts (54, 70, 92). The air injection slots (62, 64, 76, 98) extend in the direction of flow through the fuel and air mixing ducts (54, 70, 92) to the reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone (36, 40, 44). This reduces the generation of harmful vibrations in the combustion chamber (28).

Claims

1. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the average travel time from the fuel injection means to the downstream end of the fuel and air mixing duct is greater than the time period of the fluctuation wherein the combustion chamber is a tubular combustion chamber, the tubular combustion chamber having a length and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than four times the length of the tubular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the tubular combustion chamber.

2. A combustion chamber as claimed in claim 1 wherein the at least one fuel and air mixing duct comprises at least one wall, the air injectors comprise a plurality of slots extending through the wall.

3. A combustion chamber as claimed in claim 1 wherein the combustion chamber comprises a primary combustion zone and a secondary combustion zone downstream of the primary combustion zone.

4. A combustion chamber as claimed in claim 3 wherein the combustion chamber comprises a primary combustion zone, a secondary combustion zone downstream of the primary combustion zone and a tertiary combustion zone downstream of the secondary combustion zone.

5. A combustion chamber as claimed in claim 4 wherein the at least one fuel and air mixing duct supplies fuel and air into the tertiary combustion zone.

6. A combustion chamber as claimed in claim 3 wherein the at least one fuel and air mixing duct supplies fuel and air into the primary combustion zone.

7. A combustion chamber as claimed in claim 3 wherein the at least one fuel and air mixing duct supplies fuel and air into the secondary combustion zone.

8. A combustion chamber as claimed in claim 1 wherein the at least one fuel and air mixing duct comprises a single annular fuel and air mixing duct, the air injection means being circumferentially spaced apart and the air injection means extending axially.

9. A combustion chamber as claimed in claim 8 wherein the annular fuel and air mixing duct comprises an inner annular wall and an outer annular wall, the air injector means being provided in at least one of the inner and outer annular walls.

10. A combustion chamber as claimed in claim 9 wherein the air injector means are arranged in the inner and outer annular walls.

11. A combustion chamber as claimed in claim 10 wherein the air injection means in the inner annular wall are staggered circumferentially with respect to the air injection means in the outer annular wall.

12. A combustion chamber as claimed in claim 1 wherein the fuel and air mixing duct comprises a radial fuel and air mixing duct, the air injection means being circumferentially spaced apart and the air injection means extending radially.

13. A combustion chamber as claimed in claim 12 wherein the radial fuel and air mixing duct comprises a first radial wall and a second radial wall, the air injector means being provided in at least one of the first and second radial walls.

14. A combustion chamber as claimed in claim 13 wherein the air injector means are provided in the first and second radial walls.

15. A combustion chamber as claimed in claim 13 wherein the air injection means in the first radial wall are staggered circumferentially with respect to the air injection means in the second radial wall.

16. A combustion chamber as claimed in claim 1 wherein the fuel and air mixing duct comprises a tubular fuel and air mixing duct, the air injector means being circumferentially spaced apart and the air injection means extending axially.

17. A combustion chamber as claimed in claim 1 wherein the fuel injector means is arranged at the upstream end of the fuel and air mixing duct and the air injector means are arranged downstream of the fuel injector means.

18. A combustion chamber as claimed in claim 1 wherein the fuel injector means is arranged between the upstream end and the downstream end of the at least one fuel and air mixing duct, at least a portion of the air injector means are arranged upstream of the fuel injector means and at least a portion of the air injector means are arranged downstream of the fuel injector means.

19. A combustion chamber as claimed in claim 18 wherein each air injector means at the downstream end of the fuel and air mixing duct is arranged to supply more air into the fuel and air mixing duct than each air injector means at the upstream end of the fuel and air mixing duct.

20. A combustion chamber as claimed in claim 18 wherein each air injector means at a first position in the direction of flow through the fuel and air mixing duct is arranged to supply more air into the fuel and air mixing duct than said air injector means upstream of the first position in the fuel and air mixing duct.

21. A combustion chamber as claimed in claim 1 wherein each air injector means at the first position in the fuel and air mixing duct is arranged to supply less air into the fuel and air mixing duct than said air injector means downstream of the first position in the fuel and air mixing duct.

31. A combustion chamber as claimed in any of claims 1, 22, 23, 24, 25 and 26-28 wherein the at least one fuel and air mixing duct comprises a swirler.

32. A combustion chamber as claimed in claim 31 wherein the swirler is a radial flow swirler.

22. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the length of the fuel and air mixing duct multiplied by the frequency of fluctuations divided by the velocity of the fuel and air leaving the downstream end of the fuel and air mixing duct is at least one wherein the combustion chamber is a tubular combustion chamber, the tubular combustion chamber having a length and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than four times the length of the tubular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the tubular combustion chamber.

23. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the length of the fuel and air mixing duct multiplied by the frequency of fluctuations divided by the velocity of the fuel and air leaving the downstream end of the fuel and air mixing duct is at least two wherein the combustion chamber is a tubular combustion chamber, the tubular combustion chamber having a length and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than four times the length of the tubular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the tubular combustion chamber.

24. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the length of an air injector in the direction of flow through the at least one fuel and air mixing duct multiplied by the frequency of the fluctuations divided by the velocity of the fuel and air inside the at least one mixing duct is at least one wherein the combustion chamber is a tubular combustion chamber, the tubular combustion chamber having a length and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than four times the length of the tubular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the tubular combustion chamber.

25. A combustion chamber as claimed in claim 24 wherein the length of an air injector in the direction of flow through the at least one fuel and air mixing duct multiplied by the frequency of the fluctuations divided by the average velocity of the fuel and air inside the at least one mixing duct is at least two wherein the length of the slots in the direction of flow through the at least one fuel and air mixing duct is greater than eight times the length of the tubular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the tubular combustion chamber.

26. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the average travel time from the fuel injection means to the downstream end of the fuel and air mixing duct is greater than the time period of the fluctuation wherein the combustion chamber is an annular combustion chamber, the annular combustion chamber having a diameter and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than π

times the diameter of the annular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the annular combustion chamber.

27. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the length of the fuel and air mixing duct multiplied by the frequency of fluctuations divided by the velocity of the fuel and air leaving the downstream end of the fuel and air mixing duct is at least one wherein the combustion chamber is an annular combustion chamber, the annular combustion chamber having a diameter and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than 7t times the diameter of the annular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the annular combustion chamber.

28. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the volume of the fuel and air mixing duct being arranged such that the length of the fuel and air mixing duct multiplied by the frequency of fluctuations divided by the velocity of the fuel and air leaving the downstream end of the fuel and air mixing duct is at least two wherein the combustion chamber is an annular combustion chamber, the annular combustion chamber having a diameter and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct being greater than π

times the diameter of the annular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the annular combustion chamber.

29. A combustion chamber comprising at least one combustion zone defined by at least one peripheral wall, at least one fuel and air mixing duct for supplying a fuel and air mixture to the at least one combustion zone, the at least one fuel and air mixing duct having an upstream end and a downstream end, fuel injection means for supplying fuel into the at least one fuel and air mixing duct, air injection means for supplying air into the at least one fuel and air mixing duct, the pressure of the air supplied to the at least one fuel and air mixing duct fluctuating, the air injection means comprising a plurality of air injectors spaced apart transversely to the direction of flow through the at least one fuel and air mixing duct, each air injector comprising a slot extending in the direction of flow through the at least one fuel and air mixing duct to reduce the magnitude of the fluctuations in the fuel to air ratio of the fuel and air mixture supplied into the at least one combustion zone;

the length of an air injector in the direction of flow through the at least one fuel and air mixing duct multiplied by the frequency of the fluctuations divided by the velocity of the fuel and air inside the at least one mixing duct is at least one wherein the combustion chamber is an annular combustion chamber, the annular combustion chamber having a diameter and the slots in the fuel and air mixing duct having a length in the direction of flow through the at least one fuel and air mixing duct, the length of the slots in the direction of flow through the at least one fuel and air mixing duct is greater than it times the diameter of the annular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the annular combustion chamber.

30. A combustion chamber as claimed in claim 29 wherein the length of an air injector in the direction of flow through the at least one fuel and air mixing duct multiplied by the frequency of the fluctuations divided by the average velocity of the fuel and air inside the at least one mixing duct is at least two wherein the length of the slots in the direction of flow through the at least one fuel and air mixing duct is greater than 2 π

times the diameter of the annular combustion chamber multiplied by the velocity of the fuel and air in the at least one fuel and air mixing duct divided by the average speed of sound inside the annular combustion chamber.