发明名称 TURBINE BLADES AND MANUFACTURE METHODS
摘要 A blade (60; 60-2) comprises an airfoil (61) and an attachment root (63). The blade has a tipward zone (80; 80-2; 80-2, 81) and a rootward zone (82; 82-2, 81; 82). The rootward zone has a single crystal structure. The tipward zone has a single crystal structure. The crystalline orientations of the rootward zone and tipward zone are at least 15° out of registry with each other.
申请公布号 EP3047103(A1) 申请公布日期 2016.07.27
申请号 EP20140845908 申请日期 2014.08.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MARCIN, JOHN J. JR.;BULLIED, STEVEN J.;SHAH, DILIP M.;CETEL, ALAN D.
分类号 F01D5/14;F01D5/30 主分类号 F01D5/14
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