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CERAMIC MATRIX COMPOSITE COMPONENT,GAS TURBINE SEAL ASSEMBLY, AND METHOD OF FORMING CERAMIC MATRIX COMPOSITE COMPONENT
A gas turbine seal assembly includes a gas turbine component (20) and a gas turbine seal component (56) contacting the gas turbine component (20) to form a seal (52) between the two components. The gas turbine seal component (56) includes ceramic matrix composite plies (12) bonded together to form the ceramic matrix composite component (20). A bond-inhibiting coating (14) on a non-bonding portion (24) of a first surface of one of the ceramic matrix composite plies (12) prevents bonding between the non-bonding portion (24) of the first surface and a second surface of a neighboring ceramic matrix composite ply (12). At least one bonding portion (16) of the first surface lacking the bond-inhibiting coating (14) is bonded to the second surface. A method of forming a ceramic matrix composite component (20) includes selectively applying a bond-inhibiting coating (14) to a non-bonding portion (24) of a first surface of a ceramic matrix composite ply (12) and bonding the ceramic matrix composite plies (12) together.
CERAMIC MATRIX COMPOSITE COMPONENT,GAS TURBINE SEAL ASSEMBLY, AND METHOD OF FORMING CERAMIC MATRIX COMPOSITE COMPONENT
A gas turbine seal assembly includes a gas turbine component (20) and a gas turbine seal component (56) contacting the gas turbine component (20) to form a seal (52) between the two components. The gas turbine seal component (56) includes ceramic matrix composite plies (12) bonded together to form the ceramic matrix composite component (20). A bond-inhibiting coating (14) on a non-bonding portion (24) of a first surface of one of the ceramic matrix composite plies (12) prevents bonding between the non-bonding portion (24) of the first surface and a second surface of a neighboring ceramic matrix composite ply (12). At least one bonding portion (16) of the first surface lacking the bond-inhibiting coating (14) is bonded to the second surface. A method of forming a ceramic matrix composite component (20) includes selectively applying a bond-inhibiting coating (14) to a non-bonding portion (24) of a first surface of a ceramic matrix composite ply (12) and bonding the ceramic matrix composite plies (12) together.
CERAMIC MATRIX COMPOSITE COMPONENT,GAS TURBINE SEAL ASSEMBLY, AND METHOD OF FORMING CERAMIC MATRIX COMPOSITE COMPONENT
KERAMIKMATRIXVERBUNDSTOFFKOMPONENTE, GASTURBINENDICHTUNGSANORDNUNG UND VERFAHREN ZUR HERSTELLUNG EINER KERAMIKMATRIXVERBUNDSTOFFKOMPONENTE
COMPOSANT COMPOSITE À MATRICE CÉRAMIQUE, ENSEMBLE D'ÉTANCHÉITÉ DE TURBINE À GAZ ET PROCÉDÉ DE FORMATION D'UN COMPOSANT COMPOSITE À MATRICE CÉRAMIQUE
HAFNER MATTHEW TROY (Autor:in) / ITZEL GARY MICHAEL (Autor:in) / DELVAUX JOHN MCCONNELL (Autor:in)
13.09.2017
Patent
Elektronische Ressource
Englisch
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