| 发明名称 |
Turbine nozzle segment having arcuate concave leading edge |
| 摘要 |
Turbine nozzle segments with trimmed leading edges are disclosed. In one embodiment of the invention, a turbine static nozzle airfoil includes: an arcuate concave leading edge; and a substantially flat trailing edge. |
| 申请公布号 |
US8602727(B2) |
申请公布日期 |
2013.12.10 |
| 申请号 |
US20100841365 |
申请日期 |
2010.07.22 |
| 申请人 |
BAHADUR BALA MURALIDHAR SINGH;GENERAL ELECTRIC COMPANY |
发明人 |
BAHADUR BALA MURALIDHAR SINGH |
| 分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
| 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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