Method for coating gas turbine engine components

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 5/14 (2006.01) B05D 3/00 (2006.01) B05D 7/00 (2006.01) B23K 1/00 (2006.01) F01D 11/12 (2006.01)

Patent

CA 2507192

A method for assembling a vane sector (50) for a gas turbine engine (10), the vane sector including an airfoil vane (52) and a platform (54) includes depositing (102) a wear coating material (110) onto a selected area (114) of the platform, positioning (104) the platform adjacent to the airfoil vane, and executing (106) a brazing operation such that the airfoil vane is permanently coupled to the platform portion and such that the wear coating material is bonded across a predefined area (118) of the platform.

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