Method for making a gas turbine engine component

Metal working – Method of mechanical manufacture – Impeller making

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Details

298891, 298897, B23K 2700

Patent

active

052109445

ABSTRACT:
A method for making a gas turbine engine component includes the steps of: providing an unfinished gas turbine engine component; directing a laser beam on a selected surface portion of the engine component to prepare the selected surface portion before at least one of a subsequent coating and bonding step; and depositing at least one layer of an abradable material, a subassembly of the component or a thermal barrier coating on the selected surface portion.

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