Compressor blade or vane having an erosion-resistant hard material coating
A compressor blade for a gas turbine is provided. The compressor blade has a blade substrate that consists of a metal alloy and has an aluminum diffusion zone on a surface of the blade substrate. In addition, the compressor blade has a hard material coating provided on the surface of the blade substrate. A compressor that has a compressor blade and a method of producing such a compressor blade is also provided.
1. A method for producing a compressor blade or vane, comprising the following steps:
providing a blade or vane substrate comprising a metal alloy;
coating the blade or vane substrate with a hard material coating;
reducing a corrosion of the metal alloy as a result of spalling of the hard material coating by diffusing aluminum into a surface zone of the blade or vane substrate to produce an aluminum diffusion zone such that an aluminum proportion of 0.05 to 0.2% by weight is present in the surface zone, wherein, upon spalling of the hard material coating, the aluminum diffusion zone reacts to form aluminum oxide that protects the metal alloy against the corrosion; and
wherein the hard material coating comprises at least one of TiN, TiAlN, AlTiN, and CrN as a single-layer ceramic or multi-layer ceramics;
wherein the aluminum diffusion zone has a thickness of 10 to 24 micrometers.
2. The method of claim 1 , wherein the step of diffusing is carried out in such a manner that an aluminum proportion of 0.075 to 0.15% by weight is present in the surface zone.
3. The method of claim 1 , wherein, in the step of coating, a step of physical vapor deposition or of thermal plasma spraying is carried out.
4. The method of claim 1 , wherein the aluminum diffusion zone has a thickness of 15 to 24 micrometers.
5. The method of claim 1 , wherein the aluminum diffusion zone has a thickness of 20 micrometers.