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
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