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Ceramic matrix composite airfoil with heat transfer augmentation
A turbine vane assembly adapted for use in a gas turbine engine includes a support and a turbine vane arranged around the support. The support is made of metallic materials. The turbine vane is made of ceramic matrix composite materials to insulate the metallic materials of the support.
Ceramic matrix composite airfoil with heat transfer augmentation
A turbine vane assembly adapted for use in a gas turbine engine includes a support and a turbine vane arranged around the support. The support is made of metallic materials. The turbine vane is made of ceramic matrix composite materials to insulate the metallic materials of the support.
Ceramic matrix composite airfoil with heat transfer augmentation
WHITTLE MICHAEL J (Autor:in) / HILLIER STEVEN (Autor:in) / HARRIS STEPHEN (Autor:in) / SHIM SUNGBO (Autor:in)
03.10.2023
Patent
Elektronische Ressource
Englisch
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