发明名称 GAS TURBINE SHROUD WITH CERAMIC ABRADABLE LAYER
摘要 A gas turbine shroud includes a ceramic abradable coating superior in abradable property and durability. The gas turbine ceramic abradable coating of the present invention is configured by an abradable metal layer and a porous ceramic abradable layer (hardness RC15Y: 80±3), the porous ceramic abradable layer is provided with slit grooves by machining work, and a slit groove width is 0.5 to 5 mm. Thereby, the abradable property, and durability against a thermal cycle and high-temperature oxidation are improved.
申请公布号 US2012107103(A1) 申请公布日期 2012.05.03
申请号 US201113242951 申请日期 2011.09.23
申请人 KOJIMA YOSHITAKA;ARIKAWA HIDEYUKI;MEBATA AKIRA;KASUYA TADASHI;DOI HIROYUKI;ICHIKAWA KUNIHIRO;ENDO TAKAO;MIKAZUKI KAZUTO;KUROKI HIDETOSHI 发明人 KOJIMA YOSHITAKA;ARIKAWA HIDEYUKI;MEBATA AKIRA;KASUYA TADASHI;DOI HIROYUKI;ICHIKAWA KUNIHIRO;ENDO TAKAO;MIKAZUKI KAZUTO;KUROKI HIDETOSHI
分类号 F01D11/12;B23P15/00 主分类号 F01D11/12
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