发明名称 HYBRID GAMMA TIAL ALLOY COMPONENT
摘要 A hybrid component (52; 54) for a turbine engine (10) having a casing (48) includes a first part (100) of a gamma TiAl intermetallic alloy and a second part (102) of a material of at least one of nickel, a nickel base, a cobalt base, an iron base superalloy or mixtures thereof. The second part is coupled to and configured to attach the first part to the casing of the engine. The first and second parts are attached to each other by transient liquid phase (TLP) bonding.
申请公布号 EP3000980(A2) 申请公布日期 2016.03.30
申请号 EP20150187449 申请日期 2015.09.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SUCIU, GABRIEL L.;HILL, JAMES D.
分类号 F01D9/04;B23K20/16;B23K35/02;B23K35/32;B23K101/00;C23C24/00;F01D25/24 主分类号 F01D9/04
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