| 发明名称 |
GAS TURBINE AIRFOIL CLOCKING |
| 摘要 |
The first stage of vanes (16) and second stage of vanes (24) each contain the same number of vanes. The second stage vanes are located such that the wake flow (38) from the first stage vanes falls on or near the leading edge, after passing through the stage of rotating blades. |
| 申请公布号 |
WO9529331(A3) |
申请公布日期 |
1996.02.29 |
| 申请号 |
WO1995US04411 |
申请日期 |
1995.04.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHARMA, OM, PARKASH |
| 分类号 |
F01D1/04;F01D5/14;F01D9/04;F01D25/06;F02C7/00;F02K3/06 |
主分类号 |
F01D1/04 |
| 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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