发明名称 PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS
摘要 A gas turbine includes a mounting structure for mounting the engine to a pylon. A propulsor section includes a fan having a fan diameter. A geared architecture drives the fan. A generator section includes a fan drive turbine that drives the geared architecture. A turbine to fan diameter ratio is substantially less than 45%.
申请公布号 EP2904239(A4) 申请公布日期 2015.11.04
申请号 EP20130843578 申请日期 2013.02.12
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 GUKEISEN, ROBERT L.
分类号 F02C7/20;B64D27/12;F02C7/00;F02K3/06 主分类号 F02C7/20
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