BLADE TIP COATING THAT CAN BE RUBBED OFF

摘要

The present invention relates to a method for producing a component, in particular a blade for a gas turbine, wherein a main body (2) is provided, to which a run-in layer (6) is applied, which can be worn away at least partially during operation to form an accurately fitting surface (11), wherein the run-in layer is applied by kinetic cold-gas compacting, and a component, in particular a blade for a gas turbine, comprising a main body, to which a run-in layer is applied, which can be worn away at least partially during operation to form an accurately fitting surface, wherein the run-in layer is a porous layer made of a Ti alloy.