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    • 6. 发明授权
    • High temperature abradable coating for turbine shrouds without bucket tipping
    • 高温耐磨涂层用于无铲斗倾翻的涡轮机罩
    • US06660405B2
    • 2003-12-09
    • US09863760
    • 2001-05-24
    • Yuk-Chiu LauFarshad GhasripoorDennis M. GrayChek Beng Ng
    • Yuk-Chiu LauFarshad GhasripoorDennis M. GrayChek Beng Ng
    • B32B518
    • C23C4/02C23C4/04Y10T428/12479Y10T428/12736Y10T428/1275Y10T428/12771Y10T428/12931Y10T428/12944Y10T428/12951Y10T428/249953
    • An abradable coating composition for use on shrouds in gas turbine engines (or other hot gas path metal components exposed to high temperatures) containing an initial porous coating phase created by adding a “fugitive polymer” (such as polyester or polyimide) to the base metal alloy, together with a brittle intermetallic phase such as &bgr;-NiAl that serves to increase the brittle nature of the metal matrix, thereby increasing the abradability of the coating at elevated temperatures, and to improve the oxidation resistance of the coating at elevated temperatures. Coatings having about 12 wt % polyester has been found to exhibit excellent abradability for applications involving turbine shroud coatings. An abradable coating thickness in the range of between 40 and 60 ml provides the best performance for turbine shrouds exposed to gas temperatures between 1380° F. and 1850° F. Abradable coatings in accordance with the invention can be used for new metal components or to repair existing equipment.
    • 一种用于燃气涡轮发动机(或暴露于高温的其它热气体通道金属组分)的护罩上的耐磨涂层组合物,其包含通过向基体金属添加“短暂性聚合物”(例如聚酯或聚酰亚胺)而产生的初始多孔涂层相 合金,以及诸如β-NiAl的脆性金属间相,其用于增加金属基体的脆性,从而提高涂层在高温下的耐磨性,并提高涂层在高温下的抗氧化性。 已经发现具有约12重量%聚酯的涂层对于涉及涡轮机护罩涂层的应用表现出优异的耐磨性。 40至60毫升范围内的可磨损涂层厚度为暴露于1380°F至1850°F之间的气体温度的涡轮机罩提供了最佳性能。根据本发明的可磨损涂层可用于新的金属组分或 修理现有设备。