Method and apparatus for manufacturing components

A method for manufacturing a turbine nozzle assembly (50) using a fixture (104) includes providing a first position (110) of the fixture, positioning at least one datum (70) of the turbine nozzle assembly adjacent at least one datum location point (108) on the fixture when the fixture is in the firs...

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Bibliographische Detailangaben
Hauptverfasser:	RIGGS, TIMOTHY, HILL, JR.,, KENNETH RAY, WHEAT, GARY EUGENE, MOONEY, JR.,, FRANK DELANO, EDWARDS, RONALD DALE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING LIGHTING MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A method for manufacturing a turbine nozzle assembly (50) using a fixture (104) includes providing a first position (110) of the fixture, positioning at least one datum (70) of the turbine nozzle assembly adjacent at least one datum location point (108) on the fixture when the fixture is in the first position, coupling the turbine nozzle assembly to the fixture when the fixture is in the first position, rotating the fixture from the first position into a second position (112) that facilitates manufacturing the turbine nozzle assembly, and performing a manufacturing process on the turbine nozzle assembly when the fixture is in the second position.