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2. 发明公开

EP0625629A1 Turbine 失效
标题翻译：涡轮。
公开(公告)号：EP0625629A1
公开(公告)日：1994-11-23
申请号：EP93201449.1
申请日：1993-05-21
申请人： Chen, Shu Ping
发明人： Chen, Shu Ping
IPC分类号： F01D1/34 , F01D1/26
CPC分类号： F01D1/34 , F01D1/26
摘要： A turbine consisting of a central rotor (20) connected with a shaft (10) and a plurality of annular stators (30,50,70) and annular rotors (40,60). The central rotor (20) is formed as a hollow frustum of right circular cone so that it has an inner side and an outer side wherein a number of curved channels (204,205) are formed. The shaft (10) is axially inserted through the central rotor (20) and rotatably supported by means of at least one thrust bearing. Each annular stator or rotor has an outer side and an inner side wherein a plurality of curved channels (204,205) are formed. The central rotor (20) is sealably mounted in the annular stators or rotors. Driving gas flows through the curved channels (204,205) formed in the central rotor (20) and the curved channels (402,602) formed in the annular stators or rotors so that the central rotor rotates in an opposite direction relative to the annular stators or rotors.
摘要翻译：涡轮机由与轴（10）连接的中心转子（20）和多个环形定子（30,50,70）和环形转子（40,60）组成。中心转子（20）形成为圆锥形的中空截头圆锥，使得其具有形成多个弯曲通道（204,205）的内侧和外侧。轴（10）轴向地插入通过中心转子（20），并通过至少一个止推轴承可旋转地支撑。每个环形定子或转子具有形成多个弯曲通道（204,205）的外侧和内侧。中心转子（20）可密封地安装在环形定子或转子中。驱动气体流过形成在中心转子（20）中的弯曲通道（204,205）和形成在环形定子或转子中的弯曲通道（402,602），使得中心转子相对于环形定子或转子沿相反方向旋转。

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