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TURBINE VANE ASSEMBLY WITH CERAMIC MATRIX COMPOSITE AIRFOIL AND FRICTION FIT METALLIC ATTACHMENT FEATURES
A turbine vane for a gas turbine engine incorporating a ceramic matrix composite airfoil is disclosed in this paper. The turbine vane includes an attachment unit configured to mount the ceramic matrix composite airfoil to other metallic components of the turbine vane.
TURBINE VANE ASSEMBLY WITH CERAMIC MATRIX COMPOSITE AIRFOIL AND FRICTION FIT METALLIC ATTACHMENT FEATURES
A turbine vane for a gas turbine engine incorporating a ceramic matrix composite airfoil is disclosed in this paper. The turbine vane includes an attachment unit configured to mount the ceramic matrix composite airfoil to other metallic components of the turbine vane.
TURBINE VANE ASSEMBLY WITH CERAMIC MATRIX COMPOSITE AIRFOIL AND FRICTION FIT METALLIC ATTACHMENT FEATURES
VARNEY BRUCE E (Autor:in)
06.12.2018
Patent
Elektronische Ressource
Englisch
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