发明名称 |
TURBINE BLADE-CASCADE END WALL |
摘要 |
<p>Provided is a turbine blade cascade endwall that is capable of suppressing a vortex generated on a suction surface of a turbine stator blade and that is capable of reducing secondary-flow loss due to this vortex. A turbine blade cascade endwall (10) that is positioned on a tip side of a plurality of turbine stator blades (B) arranged in a ring form is provided with a pressure gradient alleviating part (11) that alleviates a pressure gradient generated in the blade height direction at a suction surface of the turbine stator blades (B) due to a clearance leakage flow, leaking out of a gap between a tip of a turbine rotor blade located on the upstream side of the turbine stator blades (B) and a tip endwall disposed facing the tip of this turbine rotor blade.</p> |
申请公布号 |
EP2187000(A4) |
申请公布日期 |
2014.01.08 |
申请号 |
EP20080871537 |
申请日期 |
2008.09.25 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
SAKAMOTO, YASURO;ITO, EISAKU;OTOMO, HIROYUKI |
分类号 |
F01D9/04;F01D5/14;F01D11/08 |
主分类号 |
F01D9/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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