| 发明名称 |
GAS TURBINE ENGINE SYSTEMS AND RELATED METHODS INVOLVING VANE-BLADE COUNT RATIOS GREATER THAN UNITY |
| 摘要 |
An exemplary gas turbine engine includes a turbine section operative to impart rotational energy to a compressor section. The turbine section includes at least a low-pressure turbine and a high-pressure turbine, and a ratio of a number of stages in the low-pressure turbine to a number of stages in the high-pressure turbine is 2.
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| 申请公布号 |
US2012117975(A1) |
申请公布日期 |
2012.05.17 |
| 申请号 |
US201113339972 |
申请日期 |
2011.12.29 |
| 申请人 |
SHARMA OM P.;BLAIR MICHAEL F. |
发明人 |
SHARMA OM P.;BLAIR MICHAEL F. |
| 分类号 |
F02C3/06;F01D1/04 |
主分类号 |
F02C3/06 |
| 代理机构 |
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