Guide vane for a turbomachine

A guide vane for a turbomachine, having a blade airfoil and at least one platform, to which the blade airfoil is connected. A cooling channel system is provided for cooling the platform and the blade airfoil. The platform has, on the side thereof facing the airfoil, at least one sealing lip for seal...

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Bibliographic Details
Main Authors Beeck, Alexander Ralph, Bolms, Hans-Thomas
Format Patent
LanguageEnglish
Published 16.11.2021
Subjects
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