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    • 1. 发明申请
    • ROTOR AND BEARING SYSTEM FOR A TURBOMACHINE
    • 涡轮机的转子和轴承系统
    • WO2005046021A3
    • 2005-12-29
    • PCT/US2004027495
    • 2004-08-24
    • CAPSTONE TURBINE CORPLUBELL DANIELWEISSERT DENNIS
    • LUBELL DANIELWEISSERT DENNIS
    • F01D25/16F01D25/22F01D3/00B63H1/00B63H13/00F01D3/04F01D25/00F03B17/00
    • F01D25/16F01D25/22
    • A rotor and bearing system for a turbomachine. The turbomachine (10) includes a drive shaft (20), an impeller (36) positioned on the drive shaft, and a turbine (34) positioned on the drive shaft proximate to the impeller. The bearing system (44) comprises one gas journal bearing (46) supporting the drive shaft between the impeller and the turbine. The area between the impeller and the turbine is an area of increased heat along the drive shaft in comparison to other locations along the drive shaft. The section of the drive shaft positioned between impeller and the turbine is also a section of the drive shaft that experiences increased stressed and load in the turbomachine. The inventive bearing machine system positions only one radial bearing in this area of increased stress and load.
    • 用于涡轮机的转子和轴承系统。 涡轮机(10)包括驱动轴(20),定位在驱动轴上的叶轮(36)以及定位在驱动轴上靠近叶轮的涡轮(34)。 轴承系统(44)包括在叶轮和涡轮机之间支撑驱动轴的一个气体轴颈轴承(46)。 与驱动轴上的其他位置相比,叶轮和涡轮之间的区域是沿驱动轴增加的热量区域。 位于叶轮和涡轮机之间的驱动轴的部分也是驱动轴的一部分,其在涡轮机中经受了增加的应力和负荷。 本发明的轴承机械系统仅在这个增加的应力和载荷区域内定位一个径向轴承。