FABRICATION OF GAS TURBINE ENGINE COMPONENTS USING MULTIPLE PROCESSING STEPS

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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HASSE, Christopher, VERRILLI, Michael J, NOE, Mark Eugene, MARUSKO, Mark Willard, TYLER, Robert, IZON, Paul
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
ARTIFICIAL STONE
BLASTING
CEMENTS
CERAMICS
CHEMISTRY
COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS
CONCRETE
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
LIME, MAGNESIA
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METALLURGY
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
REFRACTORIES
SLAG
STEAM ENGINES
TREATMENT OF NATURAL STONE
WEAPONS
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung: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 ).