| 摘要 |
<p>An abradable coating for gas turbines is provided. The abradable coating is used for sealing a radial gap between a casing ( 11 ) of the gas turbine and rotating blades ( 10 ) of the same. The abradable coating ( 13 ) is applied to the casing. The abradable coating ( 13 ) is at least single-layered, at least one outer layer of the abradable coating ( 13 ) being produced from a material having a magnetoplumbite structure, preferably lanthanum hexaaluminate.</p> |
