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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Format: | Patent |
Sprache: | eng ; fre ; ger |
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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. |
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