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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Main Authors | , |
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Format | Patent |
Language | English |
Published |
16.11.2021
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Subjects | |
Online Access | Get full text |
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