- 专利标题: Gas turbine stationary blade
-
申请号: US11246227申请日: 2005-10-11
-
公开(公告)号: US20060177301A1公开(公告)日: 2006-08-10
- 发明人: Shigehiro Shiozaki , Masamitsu Kuwabara , Yasuoki Tomita
- 申请人: Shigehiro Shiozaki , Masamitsu Kuwabara , Yasuoki Tomita
- 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
- 优先权: JP2001-211300 20010711
- 主分类号: F03B11/00
- IPC分类号: F03B11/00
摘要:
The gas turbine stationary blade comprises a stationary blade section provided therein with a passage for cooling air, an inner shroud for supporting the stationary blade section on the side of a discharge port of the cooling air, and a plurality of segments each of which includes at least one stationary blade section and at least one inner shroud. A flow passage is pulled out from the discharge port of the cooling air, and the flow passage is introduced to a front edge corner section of the inner shroud and is extended rearward along a side edge of the inner shroud.
公开/授权文献
- US07168914B2 Gas turbine stationary blade 公开/授权日:2007-01-30
信息查询