Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
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 (1008) the first assembly and a second portion of the gas turbine engine component for processing, and processing (1010) the first assembly and second portion to form a second assembly (A 2 ). In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly (A 1 ); positioning the first assembly (A 1 ) and a second plurality of CMC plies on a tool for processing, the first assembly (A 1 ) defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly (A 2 ).
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 (1008) the first assembly and a second portion of the gas turbine engine component for processing, and processing (1010) the first assembly and second portion to form a second assembly (A 2 ). In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly (A 1 ); positioning the first assembly (A 1 ) and a second plurality of CMC plies on a tool for processing, the first assembly (A 1 ) defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly (A 2 ).
FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS
HERSTELLUNG VON GASTURBINENMOTORKOMPONENTEN MIT MEHREREN VERARBEITUNGSSTUFEN
FABRICATION DE COMPOSANTS DE MOTEUR À TURBINE À GAZ À L'AIDE DE MULTIPLES ÉTAPES DE TRAITEMENT
VERRILLI MICHAEL J (Autor:in) / NOE MARK EUGENE (Autor:in) / MARUSKO MARK WILLARD (Autor:in) / IZON PAUL (Autor:in) / TYLER ROBERT (Autor:in) / HASSE CHRISTOPHER (Autor:in)
09.10.2024
Patent
Elektronische Ressource
Englisch
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