发明名称 |
TURBINE BLADES IN A GAS TURBINE ENGINE |
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 number of stages in the low pressure turbine is from three to five. |
申请公布号 |
WO2013137960(A1) |
申请公布日期 |
2013.09.19 |
申请号 |
WO2012US70861 |
申请日期 |
2012.12.20 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHARMA, OM P.;BLAIR, MICHAEL F. |
分类号 |
F02C3/14 |
主分类号 |
F02C3/14 |
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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