PROCESS FOR COMPLETE CLADDING OF METAL PARTS OF AIRCRAFT TURBOJETS, AND COMPLETE PROTECTION TOOL FOR IMPLEMENTING THE PROCESS

摘要

The invention relates to a method for recharging a metal part (202) of an aircraft turbojet engine, comprising a plurality of metal parts (203; 204), involving a nozzle (211) emitting a laser beam, characterized in that said method comprises the following different steps: - positioning of the metal part (202) to be recharged on a turntable (201); - Positioning of a cover (205) on the turntable (201); - Positioning of the nozzle (211) at an opening (206) present in the cover (205); - introduction of an inert gas under the cover (205); - reloading a first part (203) of the metal part (202) by carrying out operations: - spraying metal powders; - emission of the laser beam; - relative displacement of the nozzle (211) relative to said first metal part (203).