发明名称 VARIABLE VANE FOR USE IN TURBO MACHINES
摘要 A vane having a trunnion portion and an airfoil portion is provided with a stress reducing undercut on the trunnion portion proximate to the transition zone defined between the trunnion portion and the airfoil portion of the vane.
申请公布号 US2002076321(A1) 申请公布日期 2002.06.20
申请号 US20000742934 申请日期 2000.12.20
申请人 NICOLSON MATTHEW;DUESLER PAUL W. 发明人 NICOLSON MATTHEW;DUESLER PAUL W.
分类号 F01D9/02;F01D5/14;F01D17/16;(IPC1-7):F01D17/12 主分类号 F01D9/02
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