A method of applying a profiled abradable
coating onto a substrate in which an abradable
ceramic coating composition is applied to a
metal substrate using one or more
coating application techniques to produce a defined
ceramic pattern without requiring a separate web or grid to be brazed onto the substrate. The invention is particularly designed to withstand the higher operating temperatures encountered with the stage 1 section of 7FA+e
gas turbines to allow for increased coating life without significant deterioration in structural or
functional integrity. Typically, the
grid pattern coating begins approximately 0.431″ after the
leading edge of the shroud, and ends approximately 1.60″ before the
trailing edge of the shroud. In the case of
diamond-shaped patterns, the
grid pattern will be about 0.28″ long and 0.28″ wide, with an overall thickness of about 0.46.″ The coatings thus provide the required levels of abradability and leakage performance and may be applied as a chevron or
diamond pattern with the shape oriented such that the diagonals run perpendicular and parallel to the sides of the shroud.