发明名称 TURBOFAN ENGINE FRONT SECTION
摘要 A turbofan engine includes a geared architecture for driving a fan about an axis. The geared architecture includes a sun gear rotatable about an axis, a plurality of planet gears driven by the sun gear and a ring gear circumscribing the plurality of planet gears. A carrier supports the plurality of planet gears. The geared architecture includes a power transfer parameter (PTP) defined as power transferred through the geared architecture divided by gear volume multiplied by a gear reduction ratio and is between about 430 and 645.
申请公布号 WO2015012923(A3) 申请公布日期 2015.04.02
申请号 WO2014US35821 申请日期 2014.04.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SCHWARZ, FREDERICK M.;SHERIDAN, WILLIAM G.
分类号 F02C7/32;F02C3/04;F02K3/06;F16H1/28 主分类号 F02C7/32
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