发明名称 Two stage turbine rotor assembly.
摘要 <p>A first turbine rotor hub (32) and a second turbine rotor hub (42) each have respective internal splines (52, 62) which engage coaxial, non-concentric external splines (54, 64) on a shaft (20) and are inthrust bearing relationship. The assembly requires no bolts between the rotor stages (30) and (40) to hold the two stages together.</p>
申请公布号 EP0202188(A1) 申请公布日期 1986.11.20
申请号 EP19860630071 申请日期 1986.04.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ROBBINS, DONALD A.;KNOTEK, WILLIAM R.
分类号 F01D5/02;F01D5/06;(IPC1-7):F01D5/06 主分类号 F01D5/02
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