发明名称 VARIABLE FAN INLET GUIDE VANE FOR TURBINE ENGINE
摘要 A turbine engine includes a compressor section, a combustor arranged in fluid-receiving communication with the compressor section, a turbine section arranged in fluid-receiving communication with the combustor and a gearbox assembly coupled to be driven by the turbine section. The gearbox assembly is located at an axial position that is aft of the compressor section.
申请公布号 WO2013101795(A1) 申请公布日期 2013.07.04
申请号 WO2012US71600 申请日期 2012.12.26
申请人 UNITED TECHNOLOGIES CORPORATION;MERRY, BRIAN;SUCIU, GABRIEL L.;NORRIS, JAMES W.;SIRICA, STEVEN J.;SCHWARZ, FREDERICK M. 发明人 MERRY, BRIAN;SUCIU, GABRIEL L.;NORRIS, JAMES W.;SIRICA, STEVEN J.;SCHWARZ, FREDERICK M.
分类号 F02K3/02 主分类号 F02K3/02
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