Ceramic composite with integrated compliance/wear layer

An integral layer (38) provides a ductile interface for attachment locations of a turbine engine component (16) where a metallic surface (12) is adjacent the attachment location. The ductile layer provides a favorable load distribution through the composite at the attachment location, and eliminates...

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Bibliographische Detailangaben
Hauptverfasser: CARPER, DOUGLAS MELTON, SUBRAMANIAN, SURESH
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:An integral layer (38) provides a ductile interface for attachment locations of a turbine engine component (16) where a metallic surface (12) is adjacent the attachment location. The ductile layer provides a favorable load distribution through the composite at the attachment location, and eliminates the need for a metallic shim.