发明名称 Turbine engine components
摘要 A thermal barrier coating (208, 300) is formed over the substrate (201). A majority of the thermal barrier coating (208, 300) comprises a multi-phase material comprising a polycrystalline material including two or more phases. Each phase forms an individual grain (302, 304, 306), adjacent individual grains (302, 304, 306) are separated by grain boundaries, each phase comprises an oxide compound, the multi-phase material is formed from three or more constituents, the three or more constituents consist of different materials that are not completely soluble in each other, and the two or more phases are not completely soluble in each other and do not form only one compound.
申请公布号 EP2269966(A3) 申请公布日期 2012.04.25
申请号 EP20100167095 申请日期 2010.06.23
申请人 HONEYWELL INTERNATIONAL INC. 发明人 TOLPYGO, VLADIMIR K.
分类号 C04B35/488;C04B35/49;C04B35/495;C23C14/08;C23C14/30;C23C28/00;C23C30/00;F01D5/28 主分类号 C04B35/488
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