Method of removing excess overlay coating from within cooling holes of aluminide coated gas turbine engine components

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Hauptverfasser: GOODSTEIN, MARK, B, DAWSON, DAVID, R, FREDETTE, MARK, A, LIEBKE, WILLIAM, R
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DAWSON, DAVID, R
FREDETTE, MARK, A
LIEBKE, WILLIAM, R
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language eng
recordid cdi_epo_espacenet_SG47171A1
source esp@cenet
subjects BLASTING
COMBINED OPERATIONS
DRESSING OR CONDITIONING OF ABRADING SURFACES
ENGINE PLANTS IN GENERAL
FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
GRINDING
HEATING
LIGHTING
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
OTHER WORKING OF METAL
PERFORMING OPERATIONS
POLISHING
STEAM ENGINES
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
title Method of removing excess overlay coating from within cooling holes of aluminide coated gas turbine engine components
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