MANUFACTURE OF COOLING HOLES FOR CERAMIC MATRIX COMPOSITE COMPONENTS

To provide systems and methods for machining openings of a component.SOLUTION: A laser system 100 includes features for machining an opening 210 into a component 200, such as a cooling hole for a CMC component of a gas turbine engine. The component can be oriented in a first position P1 and lasered...

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Bibliographische Detailangaben
Hauptverfasser:	ALAN JOSEPH PARVIS, TIMOTHY FRANCIS ANDREWS, MARK SAMUEL BAILEY
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLADDING OR PLATING BY SOLDERING OR WELDING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING WEAPONS WELDING WORKING BY LASER BEAM
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