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METHOD FOR GLOBALLY RECHARGING A METAL PIECE FOR AIRCRAFT TURBOREACTORS, AND GLOBAL PROTECTION TOOLS FOR THE IMPLEMENTATION OF THE METHOD
METHOD FOR GLOBALLY RECHARGING A METAL PIECE FOR AIRCRAFT TURBOREACTORS, AND GLOBAL PROTECTION TOOLS FOR THE IMPLEMENTATION OF THE METHOD
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机译:用于飞机涡轮增压器的金属零件全局充电的方法,以及用于实施该方法的整体保护工具
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摘要
A process for cladding a metal part of an aircraft turbojet, including a plurality of metal portions, using a nozzle for emitting a laser beam, the process including positioning the metal part to be cladded on a turntable; positioning a cover on the turntable; positioning the nozzle in an aperture present in the cover; introducing an inert gas under the cover; and cladding a first portion of the metal part by carrying out operations of: spraying metal powders; emitting the laser beam; and moving the nozzle relative to the first metal portion.
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