公开(公告)号：US10179948B2

公开(公告)日：2019-01-15

申请号：US14689461

申请日：2015-04-17

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Brooks E Snyder ,  Thomas J Martin ,  Thomas N Slavens

IPC: C23C16/48 ,  F01D5/28 ,  C23C16/455 ,  C23C16/40 ,  C23C16/04

Abstract: A method for coating a turbine engine component, said method includes the steps of: placing the component into a chamber; injecting a non-reactive carrier gas containing a coating material into the chamber; and forming a coating on a desired portion of the component by locally heating the desired portion of the component by redirecting a directed energy beam onto the desired portion of the component.