发明申请
US20110033281A1 STEAM TURBINE, METHOD OF COOLING STEAM TURBINE, AND HEAT INSULATING METHOD FOR STEAM TURBINE
有权
蒸汽涡轮机,蒸汽涡轮机冷却方法和蒸汽涡轮机热绝缘方法
- 专利标题: STEAM TURBINE, METHOD OF COOLING STEAM TURBINE, AND HEAT INSULATING METHOD FOR STEAM TURBINE
- 专利标题(中): 蒸汽涡轮机,蒸汽涡轮机冷却方法和蒸汽涡轮机热绝缘方法
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申请号: US12839826申请日: 2010-07-20
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公开(公告)号: US20110033281A1公开(公告)日: 2011-02-10
- 发明人: Asako INOMATA , Katsuya YAMASHITA , Kazuhiro SAITO , Takao INUKAI , Kunihiko WADA , Kazutaka IKEDA , Takeo SUGA
- 申请人: Asako INOMATA , Katsuya YAMASHITA , Kazuhiro SAITO , Takao INUKAI , Kunihiko WADA , Kazutaka IKEDA , Takeo SUGA
- 专利权人: KABUSHIKI KAISHA TOSHIBA
- 当前专利权人: KABUSHIKI KAISHA TOSHIBA
- 优先权: JP2009-184406 20090807
- 主分类号: F01D25/14
- IPC分类号: F01D25/14 ; F01D1/04 ; F01D1/10 ; F01D25/26
摘要:
A steam turbine 10 is provided with a double-structure comprising an inner casing 20 and an outer casing 21. A turbine rotor 22, in which plural stages of moving blades 24 are circumferentially implanted, is operatively disposed in inner casing 20. A diaphragm outer ring 25 and a diaphragm inner ring are disposed along the circumferential direction in inner casing 20. Stationary blades 27 are circumferentially provided between diaphragm outer ring 25 and the diaphragm inner ring, so that diaphragm outer ring 25, the diaphragm inner ring and stationary blades 27 form a stage of stationary blades. The stages of the stationary blades are arranged alternately with the stages of moving blades 24 in the axial direction of turbine rotor 22. A cooling medium passage 40 for passing a cooling medium CM which is supplied through a supply pipe 45 is formed between inner casing 20 and diaphragm outer ring 25.
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