FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS

Methods (1000) for fabricating a component of a gas turbine engine are provided. In one embodiment, the method (1000) includes molding (1002) a CMC material to form a first portion of the gas turbine engine component, processing (1006) the first portion to form a first assembly (A 1 ), preparing (10...

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Bibliographische Detailangaben
Hauptverfasser: HASSE, Christopher, VERRILLI, Michael J, NOE, Mark Eugene, MARUSKO, Mark Willard, TYLER, Robert, IZON, Paul
Format: Patent
Sprache:eng ; fre ; ger
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