发明名称 Turbine disk preform, welded turbine rotor made therewith and methods of making the same
摘要 <p>A method (100) of making a turbine rotor is disclosed. The method includes forming a last stage disk preform (36) having a disk axis (44), the preform having a rotor face (46) and an opposed shaft face (48), the rotor face (46) having a circumferential, axially-extending rotor rib (50) protruding therefrom, the shaft face having a circumferential, axially-extending shaft rib (56) protruding therefrom, the disk preform comprising a disk preform material (76). The method also includes joining the rotor rib (50) to a rotor preform (13) to form a rotor joint (52), the rotor preform (13) comprising a rotor preform material (78). The method further includes joining the shaft rib (56) to a shaft (60) to form a shaft joint (58), the shaft comprising a shaft material (74), wherein the disk preform material (76) is different than the rotor preform material (78) and the shaft material (74).</p>
申请公布号 EP2540963(A2) 申请公布日期 2013.01.02
申请号 EP20120173855 申请日期 2012.06.27
申请人 GENERAL ELECTRIC COMPANY 发明人 GANESH, SWAMI;BREITENBACH, STEVEN LOUIS;SCHWANT, ROBIN CARL
分类号 F01D5/06;F01D5/02 主分类号 F01D5/06
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