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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Bibliographic Details
Main Authors DUECKERSHOFF, ROLAND, STEIGER, ULRICH, RATHMANN, ULRICH
Format Patent
LanguageEnglish
French
German
Published 30.03.2011
Subjects
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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.
Bibliography:Application Number: EP20090765688