发明名称 THERMAL BARRIER PLACED DIRECTLY ON MONOCRYSTALLINE SUPERALLOY
摘要 PROBLEM TO BE SOLVED: To provide a method in which the production flow process of an assembled body is simplified, while reducing the production cost thereof, the service life of a superalloy coated with a thermal barrier is elongated. SOLUTION: On a monocrystalline superalloy (10) having the following composition containing, by weight: 3.5% to 7.5% Cr, 0 to 1.5% Mo, 1.5% to 5.5% Re, 2.5% to 5.5% Ru, 3.5% to 8.5% W, 5% to 6.5% Al, 0 to 2.5% Ti, 4.5% to 9% Ta, 0.08% to 0.12% Hf, 0.08% to 0.12% Si, the balance to 100% being constituted by Ni and any impurities, a stabilized zirconia (20) is deposited directly, the zirconia being stabilized with at least one oxide of an element selected from the group constituted by rare earths, or with a combination of a tantalum oxide and at least one rare earth oxide, or with a combination of a niobium oxide and at least one rare earth oxide. COPYRIGHT: (C)2009,JPO&INPIT
申请公布号 JP2008255485(A) 申请公布日期 2008.10.23
申请号 JP20080079784 申请日期 2008.03.26
申请人 SNECMA 发明人 BOURLIER FLORENT;LE BIAVANT KRISTELL
分类号 C23C30/00;F01D5/18;F01D5/28;F01D25/00;F02C7/00;F02C7/24 主分类号 C23C30/00
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