Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations
View Patent ↗A combustion device ( 1 ) for a gas turbine includes portions ( 12 ) having an inner and an outer wall ( 13, 14 ) with an interposed noise absorption plate ( 15 ) having a plurality of holes ( 16 ). The combustion device ( 1 ) further has first passages ( 17 ) connecting zones between the inner wall ( 13 ) and the plate ( 15 ) to the inside of the combustion device ( 1 ) and second passages ( 21 ) for cooling the inner wall ( 13 ). The portions ( 12 ) also have an inner layer ( 22 ) between the inner wall ( 13 ) and the plate ( 15 ) defining inner chambers ( 23 ), each connected to at least a first passage ( 17 ), and an outer layer ( 24 ) between the outer wall ( 14 ) and the plate ( 15 ) defining outer chambers ( 25 ) connected to the inner chambers ( 23 ) via the holes ( 16 ) of the plate ( 15 ).
1. A combustion device for a gas turbine comprising:
a portion having an inner wall and an outer wall and an interposed noise absorption plate having a plurality of holes between the inner wall and the plate, a plurality of zones being between the inner wall and the plate, the inner wall delimiting an inside of the combustion device;
first passages connecting the zones between the inner wall and the plate to the inside of the combustion device;
an inner layer between the inner wall and the plate defining inner chambers, each inner chamber connected to at least one of the first passages;
an outer layer between the outer wall and the plate defining outer chambers connected to the inner chambers via the holes; and
second passages extending through the outer wall to the inner wall, each of the second passages including a portion extending in and parallel to the inner wall, each of the inner chambers connected to at least one of the second passages through the portion, wherein the inner chambers, the outer chambers, and the passages define Helmholtz dampers.
2. The combustion device as claimed in claim 1 , wherein said inner wall, inner layer, plate, outer layer, and outer wall lay one over the other to define a layered structure.
3. The combustion device as claimed in claim 2 , wherein said inner wall, inner layer, plate, outer layer, and outer wall are brazed together.
4. The combustion device as claimed in claim 2 , wherein the inner layer is a separate piece from the inner wall.
5. The bustion device as claimed in claim 2 , wherein the outer layer is integral with or a separate piece from the outer wall.
6. The combustion device as claimed in claim 2 , wherein the outer wall delimits an outside of the combustion device and has a plurality of outer holes connecting said outside to the outer chambers.
7. The combustion device as claimed in claim 2 , wherein:
the outer wall delimits an outside of the combustion device; and
the second passages open to said outside and pass through the layered structure.
8. The combustion device as claimed in claim 7 , further comprising:
aligned apertures formed at least in said outer wall, outer layer, plate, and inner layer;
wherein the aligned apertures at least partly define the second passages.
9. The combustion device as claimed in claim 8 , wherein said portion of the second passages extending parallel to the inner wall is adjacent to and is configured and arranged to cool the inner wall.
10. The combustion device as claimed in claim 1 , wherein each of the second passages extend through the plate.
11. The combustion device as claimed in claim 10 , wherein each of the second passages extend through the inner layer and the outer layer.
12. The combustion device as claimed in claim 10 , wherein each of the second passages extend from the outer wall to within the inner wall without passing through the outer chambers.
13. The combustion device as claimed in claim 12 , wherein each of the second passages extend from the outer wall to within the inner wall without passing through the inner chambers.