| 摘要 |
<p>The invention relates to an erosion protection coating (11), in particular for gas turbine components, having a horizontally segmented and multi-layered design, which is to say with at least one relatively hard layer (12) and at least one relatively soft layer (13), wherein the relatively hard layer, or every one thereof, and the relatively soft layer, or every one thereof, are disposed one on top of the other in an alternating fashion such that an outer layer forming an outer surface of the erosion protection coating is configured as a relatively hard layer (12). According to the invention, the relatively hard layer (12), or every one thereof, and the relatively soft layer (13), or every one thereof, are each designed as ceramic layers.</p> |
