| 发明名称 |
GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION |
| 摘要 |
A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.
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| 申请公布号 |
US2013192263(A1) |
申请公布日期 |
2013.08.01 |
| 申请号 |
US201213410776 |
申请日期 |
2012.03.02 |
| 申请人 |
SUCIU GABRIEL L.;SCHWARZ FREDERICK M.;ACKERMANN WILLIAM K.;KUPRATIS DANIEL BERNARD |
发明人 |
SUCIU GABRIEL L.;SCHWARZ FREDERICK M.;ACKERMANN WILLIAM K.;KUPRATIS DANIEL BERNARD |
| 分类号 |
F02C3/06 |
主分类号 |
F02C3/06 |
| 代理机构 |
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代理人 |
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| 主权项 |
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