Combustor dynamic attenuation and cooling arrangement
Disclosed is a combustor casing with an inner casing which defines a combustion chamber, an outer casing spaced apart from the inner casing for defining a passage between the inner and the outer casing, first and second effusion holes arranged in the inner casing, and dividing ribs connecting the inner and outer casings and forming at least first and second volumes for receiving part of a flow injected into the passage.
1. A combustor casing, comprising:
an inner casing defining a combustion chamber;
an outer casing spaced apart from the inner casing for defining a passage between the inner and the outer casing, the passage being adapted to guide cooling air from a cooling air entrance arranged at a downstream end of the combustion chamber to a burner hood arranged at an upstream end of the combustion chamber;
first and second effusion holes arranged in the inner casing, through which a portion of the cooling air penetrates into the combustion chamber; and
dividing ribs connecting the inner casing and outer casing and forming first and second volumes for receiving part of a flow injected into the passage, wherein the dividing ribs are separate from one another and are not equally spaced to form the first and second volumes,
wherein the first effusion holes are arranged in the first volume and the second effusion holes are arranged in the second volume, and
wherein the first effusion holes have a first pattern and the second effusion holes have a second pattern, such that the first and second patterns differ in terms of hole diameters and/or spacing between the holes, and
wherein the first and second volumes, as well as the hole diameters and/or spacing between the holes are adapted to specific frequencies to optimise damping performance and differ between different volumes.
2. The combustor casing as claimed in claim 1 , wherein the first and second effusion holes and the first and second volumes are arranged in areas of previously determined antinodes of dynamic acoustic waves to be damped during operation of the combustion chamber.
3. The combustor casing as claimed in claim 1 , wherein turbulators are arranged in the passage.
4. The combustor casing as claimed in claim 3 , wherein the turbulators are arranged on the inner casing.
5. The combustor casing as claimed in claim 3 , wherein the turbulators extend in a direction traverse to a flow direction.
6. The combustor casing as claimed in claim 1 , wherein the dividing ribs extend along the passage parallel to a centre line of the combustor casing.
7. The combustor casing as claimed in claim 1 , wherein there are more second effusion holes in the second pattern than first effusion holes in the first pattern.
8. The combustor casing as claimed in claim 1 , wherein there are more rows of second effusion holes in the second pattern than rows of first effusion holes in the first pattern.
9. The combustor casing as claimed in claim 1 , wherein the second effusion holes in the second pattern have a greater diameter than the diameter of the first effusion holes in the first pattern.
10. The combustor casing as claimed in claim 1 , wherein the second effusion holes in the second pattern have a greater spacing than the spacing of the first effusion holes in the first pattern.
11. The combustor casing as claimed in claim 1 , wherein the dividing ribs are not equally spaced in a direction transverse to the cooling air flow direction from the cooling air entrance to the burner hood.
12. The combustor casing as claimed in claim 1 , wherein the second volume has a greater volume than the first volume.
13. A combustor, comprising:
a combustor casing, the combustor casing having
an inner casing defining a combustion chamber;
an outer casing spaced apart from the inner casing for defining a passage between the inner and the outer casing, the passage being adapted to guide cooling air from a cooling air entrance arranged at a downstream end of the combustion chamber to a burner hood arranged at an upstream end of the combustion chamber;
first and second effusion holes arranged in the inner casing, through which a portion of the cooling air penetrates into the combustion chamber; and
dividing ribs connecting the inner casing and outer casing and forming first and second volumes for receiving part of a flow injected into the passage, wherein the dividing ribs are separate from one another and are unequally spaced to form the first and second volumes,
wherein the first effusion holes are arranged in the first volume and the second effusion holes are arranged in the second volume,
wherein the first effusion holes have a first pattern and the second effusion holes have a second pattern, such that the first and second patterns differ in terms of hole diameters and/or spacing between the holes, and
wherein the first and second volumes, as well as the hole diameters and/or spacing between the holes are adapted to specific frequencies to optimise damping performance and differ between different volumes.
14. The combustor as claimed in claim 13 , wherein the combustor is a can-type combustor.
15. The combustor as claimed in claim 13 , wherein the combustor is an annular combustor.
16. The combustor as claimed in claim 13 , wherein the combustor is a sequential combustor.
17. The combustor as claimed in claim 13 , wherein the combustor is a reheat combustor.
18. The combustor as claimed in claim 13 , wherein the first and second effusion holes and the first and second volumes are arranged in areas of previously determined antinodes of dynamic acoustic waves to be damped during operation of the combustion chamber.