Arrangement for the cooling of thermally highly loaded components
An inexpensively manufacturable arrangement for the cooling of thermally highly loaded components, for example the combustion chamber of a gas turbine, comprises cavities ( 4 ) provided on the thermally loaded inner surface/air exit side ( 3 ) of the wall ( 1 ) of the component which are supplied with a cooling medium from the outer surface/air inlet side ( 5 ) via cooling air openings ( 6 ) and which are covered by a heat resistant wire mesh ( 7 ) of a certain permeability. The cavity, which acts as pressure accumulator, forms, in connection with the wire mesh, a uniform pressurized-air film ( 8 ) for the cooling and heat shielding of the wall surface.
1. An arrangement for the cooling of a thermally highly loaded component, in which cooling air openings are provided in the component to be cooled, which are supplied with cooling air at an air inlet side, to form a cooling air film at an air exit side of the component, wherein at least one cavity is provided at the air exit side which connects to at least one of the cooling air openings, the cooling air openings being dimensioned such that they are manufacturable by casting while being able to supply a required cooling air volume, the cavity, which is open at the air exit side, being covered with a gas-permeable Wire mesh made of heat-resistant material for the formation of the cooling air film.
2. An arrangement in accordance with claim 1 , wherein the wire mesh is connected to a rim area of the open side of the cavity.
3. An arrangement in accordance with claim 1 , wherein the component and the wire mesh are constructed of different materials, with the wire mesh material having a higher thermal loadability than the component material.
4. An arrangement in accordance with claim 1 , wherein the permeability of the wire mesh is between 5 and 95%.
5. An arrangement in accordance with claim 4 , wherein the permeability of the wire mesh is approximately 20%.
6. An arrangement in accordance with claim 1 , wherein the component is a wall of a combustion chamber and the cavity is provided by a groove-shaped channel which extends along an inner circumference of the combustion chamber and is formed into an inner surface of the wall, with cooling air openings being distributed over the channel length.
7. An arrangement in accordance with claim 6 , wherein multiple channel-style cavities are arranged in parallel and one above the other on the wall.
8. An arrangement in accordance with claim 7 , wherein the cavities are formed into steps resulting from a Z-shape of the component to be cooled.
9. An arrangement in accordance with claim 1 , wherein the cavity is provided by several sequential channels, with cooling air openings issuing into these channels.
10. An arrangement in accordance with claim 1 , wherein the component is a product of at least one of a non-cutting and a cutting forming process.
11. An arrangement in accordance with claim 1 , wherein the component, including the cooling air openings and the cavities, is a cast component.
12. An arrangement in accordance with claim 2 , wherein the component and the wire mesh are constructed of different materials, with the wire mesh material having a higher thermal loadability than the component material.
13. An arrangement in accordance with claim 12 , wherein the component is a wall of a combustion chamber and the cavity is provided by a groove-shaped channel which extends along an inner circumference of the combustion chamber and is formed into an inner surface of the wall, with cooling air openings being distributed over the channel length.
14. An arrangement in accordance with claim 13 , wherein the permeability of the wire mesh is between 5 and 95%.
15. An arrangement in accordance with claim 14 , wherein the permeability of the wire mesh is approximately 20%.
16. An arrangement for the coating of a thermally highly loaded component, comprising:
a component wall,
a plurality of cooling air openings provided in the component wail which are supplied with cooling air at an air inlet side of the component wall
at least one cavity at an air exit side of the component wall which connects to at least one of the cooling air openings, the cavity being open at the air exit side,
a gas-permeable wire mesh made of heat-resistant material covering the open side of the cavity for the formation of a cooling air film.
17. An arrangement in accordance with claim 16 , wherein the cooling air openings are dimensioned such that they are manufacturable by casting while being able to supply a required cooling air volume.
18. An arrangement in accordance with claim 16 , wherein the component and the wire mesh are constructed of different materials, with the wire mesh material having a higher thermal loadability than the component material.
19. An arrangement in accordance with claim 16 , wherein the component is a wall of a combustion chamber and the cavity is provided by a groove-shaped channel which extends along an inner circumference of the combustion chamber and is formed into an inner surface of the wall, with cooling air openings being distributed over the channel length.
20. An arrangement in accordance with claim 16 , wherein the permeability of the wire mesh is approximately 20%.