发明授权
- 专利标题: Disc axis adjusting mechanism in gas turbine
- 专利标题(中): 燃气轮机中的圆盘轴调整机构
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申请号: US14376035申请日: 2013-02-08
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公开(公告)号: US09567873B2公开(公告)日: 2017-02-14
- 发明人: Motoharu Ueda , Eigo Katou , Eisaku Ito
- 申请人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 申请人地址: JP Tokyo
- 专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人: MITSUBISHI HEAVY INDUSTRIES, LTD.
- 当前专利权人地址: JP Tokyo
- 代理机构: Westerman, Hattori, Daniels & Adrian, LLP
- 优先权: JP2012-027334 20120210; JP2012-037719 20120223
- 国际申请: PCT/JP2013/053113 WO 20130208
- 国际公布: WO2013/118880 WO 20130815
- 主分类号: F01D9/02
- IPC分类号: F01D9/02 ; F01D25/14 ; F01D25/30 ; F02C7/18 ; F01D25/16 ; F02C7/20 ; F01D9/06 ; F01D11/24 ; F01D17/02 ; F01D21/04
摘要:
In a disc axis adjusting mechanism in a gas turbine, the gas turbine has an exhaust gas diffuser provided between a casing wall and a bearing case which are connected to a downstream side of a turbine, a plurality of struts provided at intervals in a circumferential direction, and strut covers coupling an outer diffuser and an inner diffuser of the exhaust gas diffuser so as to cover the struts, and the mechanism comprises: a plurality of air introduction holes formed in the casing wall so as to allow the interior and exterior of the wall to communicate with each other; a sensor unit configured to detect a parameter corresponding to the thermal elongation of each of the struts; and a flow rate adjustor configured to adjust the flow rate of air flowing through each of the air introduction holes based on a detection value detected by the sensor unit.
公开/授权文献
- US20150078887A1 DISC SHAFT CENTER ADJUSTING MECHANISM IN GAS TURBINE 公开/授权日:2015-03-19
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