Cooled constructional element for a gas turbine
First Claim
1. A cooled constructional element for a gas turbine comprising:
- a wall including a front side and a rear side, the front side being configured to be thermally loaded during operation of the turbine and the rear side having a plurality of pins projecting therefrom in a two-dimensional distribution, the two-dimensional distribution including a higher density distribution of pins in a critical zone of the cooled constructional element than in the remaining regions of the cooled constructional element; and
an impingement cooling plate having a plurality of impingement cooling holes in a distributed arrangement and configured to create jets of a cooling medium that are directed onto the rear side of the wall in a region of the plurality of pins so as to cool the rear side of the wall by impingement, the impingement cooling plate being disposed essentially parallel at a distance to the rear side of the wall and the distributed arrangement of the plurality of cooling holes corresponding to the two-dimensional distribution of the plurality of pins such that, in a direction perpendicular to the impingement cooling plate, the plurality of cooling holes are respectively disposed between the plurality of pins.
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Accused Products
Abstract
A cooled constructional element for a gas turbine includes a wall having a front and a rear side. The front side is configured to be thermally loaded during operation of the turbine, and the rear side has a plurality of pins projecting therefrom in a two-dimensional distribution, the two-dimensional distribution including a higher density distribution of pins in a critical zone of the cooled constructional element than in the remaining regions of the cooled constructional element. A device is configured to create jets of a cooling medium that are directed onto the rear side of the wall in a region of the plurality of pins so as to cool the rear side of the wall by impingement.
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Citations
5 Claims
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1. A cooled constructional element for a gas turbine comprising:
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a wall including a front side and a rear side, the front side being configured to be thermally loaded during operation of the turbine and the rear side having a plurality of pins projecting therefrom in a two-dimensional distribution, the two-dimensional distribution including a higher density distribution of pins in a critical zone of the cooled constructional element than in the remaining regions of the cooled constructional element; and an impingement cooling plate having a plurality of impingement cooling holes in a distributed arrangement and configured to create jets of a cooling medium that are directed onto the rear side of the wall in a region of the plurality of pins so as to cool the rear side of the wall by impingement, the impingement cooling plate being disposed essentially parallel at a distance to the rear side of the wall and the distributed arrangement of the plurality of cooling holes corresponding to the two-dimensional distribution of the plurality of pins such that, in a direction perpendicular to the impingement cooling plate, the plurality of cooling holes are respectively disposed between the plurality of pins. - View Dependent Claims (2, 3)
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4. A stator blade for a gas turbine comprising:
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a blade airfoil extending in a longitudinal direction; a platform adjoining the blade airfoil and extending transversely to the longitudinal direction, the platform including a base having a front side and a rear side, the front side being configured to be thermally loaded during operation of the turbine and the rear side having a plurality of pins projecting therefrom in a two-dimensional distribution, the two-dimensional distribution including a higher density distribution of pins in a critical zone of the stator blade than in the remaining regions of the stator blade; and an impingement cooling plate configured to create jets of a cooling medium that are directed onto the rear side of the base in a region of the plurality of pins so as to cool the rear side of the base by impingement, the impingement cooling plate being disposed essentially parallel at a distance to the rear side of the base and the distributed arrangement of the plurality of cooling holes corresponding to the two-dimensional distribution of the plurality of pins such that, in a direction perpendicular to the impingement cooling plate, the plurality of cooling holes are respectively disposed between the plurality of pins. - View Dependent Claims (5)
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Specification