- 专利标题: Cooling structure of stationary blade, and gas turbine
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申请号: US10202654申请日: 2002-07-25
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公开(公告)号: US06761529B2公开(公告)日: 2004-07-13
- 发明人: Friedrich Soechting , Satoshi Hada , Masamitsu Kuwabara , Junichiro Masada , Yasuoki Tomita
- 申请人: Friedrich Soechting , Satoshi Hada , Masamitsu Kuwabara , Junichiro Masada , Yasuoki Tomita
- 主分类号: F01D906
- IPC分类号: F01D906
摘要:
A collision plate having plural small holes is provided at an interval from a bottom surface of an inner shroud to form a chamber and guides cooling air from the small holes into the chamber. A leading edge flow path is provided at a leading edge side along a width direction and introduces the cooling air. A side flow path is provided along both sides of the inner shroud and guides the cooling air to a trailing edge side. A header is formed along the width direction near the trailing edge and guides the cooling air from the side flow path. Plural trailing edge flow paths are formed at the trailing edge side at intervals along a width direction, in which one end of each flow path is connected to the header and the other end is open at the trailing edge, and the cooling air in the header is ejected from the trailing edge.
公开/授权文献
- US20040018082A1 Cooling structure of stationary blade, and gas turbine 公开/授权日:2004-01-29
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