Damping device for a gas turbine combustor

Patent metadata

Field	Value
Publication number	US-9557062-B2
Application number	US-201314088527-A
Country	US
Kind code	B2
Filing date	Nov 25, 2013
Priority date	Nov 30, 2012
Publication date	Jan 31, 2017
Grant date	Jan 31, 2017

Abstract

The invention relates to a damping device for a gas turbine combustor with significantly reduced cooling air mass flow requirements. The damping device includes a wall with a first inner wall and a second outer wall, arranged in a distance to each other. The inner wall is subjected to high temperatures on a side with a hot gas flow. A plurality of cooling channels extend essentially parallel between the first inner wall and the second outer wall, and at least one damping volume bordered by cooling channels. Furthermore, the damping device includes a first passage for supplying a cooling medium from a cooling channel into the damping volume and a second passage for connecting the damping volume to the combustion chamber. An end plate, fixed to the inner wall, separates the damping volume from the combustion chamber.

First claim

The invention claimed is:

1. A damping device for a gas turbine combustor, comprising:
a first inner wall on a side with a hot gas flow and arranged to be subjected to high temperatures;
a second outer wall, arranged at a distance from the first inner wall;
a plurality of cooling channels extending parallel between the first inner wall and the second outer wall;
at least one damping volume between the inner wall and the outer wall;
a first passage for supplying a cooling medium from a cooling channel of the plurality of cooling channels into the damping volume;
a neck passage configured to connect the at least one damping volume to a combustion chamber; and
an end plate fixed to the first inner wall, separating the damping volume from the combustion chamber, wherein said end plate is provided with the neck passage and includes at least one feed plenum for the cooling medium, at least one exit plenum for the cooling medium and cooling passages enabling a flow of cooling medium from the at least one feed plenum to a second plenum and to the at least one exit plenum in a cooling medium flow path direction, wherein the feed plenum, exit plenum, second plenum, and the cooling passages are formed within the end plate and are in serial flow communication to circulate cooling medium through the end plate, and the exit plenum exhaust cooling medium to the damping volume or combustion chamber.

2. The damping device according to claim 1 , wherein the cooling passages acts as a near wall cooling channel.

3. The damping device according to claim 2 , wherein the end plate comprises a plurality of near wall cooling channels.

4. The damping device according to claim 3 , wherein the near wall cooling channels have the same cross-section.

5. The damping device according to claim 1 , wherein the at least one feed plenum communicates via a feeding passage in the first inner wall with a cooling channel.

6. The damping device according to claim 1 , wherein the feed plenum and the second plenum are arranged at different lateral edges of the end plate, and the second plenum and a third plenum are arranged at different lateral edges of the end plate.

7. The damping device according to claim 1 , wherein the feed plenum and the second plenum are arranged at opposite edges of the end plate, and the second plenum and a third plenum are arranged at opposite edges of the end plate.

8. The damping device according to claim 7 , wherein the cooling passages run parallel.

9. The damping device according to claim 1 , wherein the at least one exit plenum communicates with either the damping volume or the combustion chamber.

10. The damping device according to claim 1 , wherein lateral edges of the end plate are provided with recesses, and in conjunction with a connected inner wall form the feed plenum and the second plenum.

11. The damping device according to claim 1 , wherein the end plate is fixed to the inner wall by welding.

12. The damping device according to claim 1 , wherein the inner wall is a liner of a gas turbine combustor.

13. The damping device according to claim 1 , wherein the wall comprises more than one individual damping volumes.

14. The damping device according to claim 13 , wherein the more than one individual damping volumes are arranged in an axial direction.

15. The damping device according to claim 13 , wherein the individual damping volumes have different parameters.

Assignees

• Alstom Technology Ltd
• General Electric Technology Gmbh

Inventors

• Maurer Thomas Michael
• Benz Urs
• Bothien Mirko Ruben

Classifications

• F23R3/42 Primary

  characterised by the arrangement or form of the flame tubes or combustion chambers · CPC title

• F05D2260/963

  by Helmholtz resonators · CPC title

• F23M20/005 Primary

  Noise absorbing means · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F23R3/00

  Continuous combustion chambers using liquid or gaseous fuel · CPC title