发明名称 THREE SPOOL GEARED TURBOFAN WITH LOW PRESSURE COMPRESSOR DRIVE GEAR SYSTEM
摘要 A turbofan engine includes a fan rotatable about an axis and a compressor section including a high pressure compressor and a low pressure compressor. A turbine section includes a high pressure turbine, an intermediate turbine and a fan drive turbine. The high pressure turbine is coupled to drive the high pressure compressor. A fan drive gear system is driven by the fan drive turbine for driving the fan and a compressor drive gear system is driven by the intermediate turbine for driving the low pressure compressor.
申请公布号 WO2015006162(A1) 申请公布日期 2015.01.15
申请号 WO2014US45411 申请日期 2014.07.03
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 OTTO, JOHN R.;COFFIN, JAMES B.;HUSBAND, JASON
分类号 F02C7/36;F01D25/00;F16H1/34;F16H3/66;F16H57/08 主分类号 F02C7/36
代理机构 代理人
主权项
地址