| 发明名称 |
TURBINE ENGINE INCLUDING BALANCED LOW PRESSURE STAGE COUNT |
| 摘要 |
A turbine engine includes at least a compressor section and a turbine section, each having at least a first and second portion. A ratio of turbine section second portion stages to compressor section second portion stages is less than or equal to 1. |
| 申请公布号 |
EP3090160(A4) |
申请公布日期 |
2016.12.28 |
| 申请号 |
EP20140877384 |
申请日期 |
2014.12.19 |
| 申请人 |
United Technologies Corporation |
发明人 |
KUPRATIS, Daniel Bernard;HASEL, Karl L. |
| 分类号 |
F02C3/04;F02C7/00;F02K3/06 |
主分类号 |
F02C3/04 |
| 代理机构 |
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代理人 |
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