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 |
WO2015102952(A1) |
申请公布日期 |
2015.07.09 |
申请号 |
WO2014US71537 |
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 |
主分类号 |
F02C3/04 |
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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