发明名称 ABRADABLE LAYER INCLUDING A LOW THERMAL CONDUCTIVITY COMPOSITION
摘要 A system may include a blade track or blade shroud and a gas turbine blade that includes a blade tip. The blade track or blade shroud may include a substrate and an abradable layer formed over the substrate. The abradable layer may include at least one of zirconia or hafnia; ytterbia; samaria; and at least one of lutetia, scandia, ceria, gadolinia, neodymia, or europia. The abradable layer may include a porosity between about 25 vol. % and about 50 vol. %. The blade track or blade shroud and the gas turbine blade may be configured so the blade tip contacts a portion of the abradable layer during rotation of the gas turbine blade, and the abradable layer may be configured to be abraded by the contact by the blade tip.
申请公布号 US2014199163(A1) 申请公布日期 2014.07.17
申请号 US201214004075 申请日期 2012.03.08
申请人 Lee Kang N. 发明人 Lee Kang N.
分类号 F01D11/12;C23C28/04 主分类号 F01D11/12
代理机构 代理人
主权项 1. A system comprising: a blade track or blade shroud comprising: a substrate, andan abradable layer formed over the substrate, wherein the abradable layer comprises: at least one of zirconia or hafnia,ytterbia,samaria, andat least one of lutetia, scandia, ceria, gadolinia, neodymia, or europia, wherein the abradable layer comprises a porosity between about 25 vol. % and about 50 vol. %; and a gas turbine blade comprising a blade tip, wherein the blade track or blade shroud and the gas turbine blade are configured so the blade tip contacts a portion of the abradable layer during rotation of the gas turbine blade, and wherein the abradable layer is configured to be abraded by the contact by the blade tip.
地址 Zionsville IN US