GAS TURBINE COMPRISING A GUIDE VANE
A gas turbine with a stator blade is disclosed. The stator blade is fastened on a blade carrier and includes a blade airfoil which extends inwards in the radial direction from an outer platform into a hot gas passage. A cooling medium can flow through an interior of the blade airfoil, such as coolin...
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
30.03.2011
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine with a stator blade is disclosed. The stator blade is fastened on a blade carrier and includes a blade airfoil which extends inwards in the radial direction from an outer platform into a hot gas passage. A cooling medium can flow through an interior of the blade airfoil, such as cooling air, which flows through an access in the blade carrier into a first plenum which is arranged above the outer platform, and from there, via an inlet which is provided in the outer platform, flows into the interior of the blade airfoil. |
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Bibliography: | Application Number: EP20090765688 |