发明名称 GEARED TURBOFAN HIGH GEARBOX POWER DENSITY
摘要 <p>A geared architecture for a gas turbine engine includes a central gear supported for rotation about the axis, a plurality of intermediate gears engaged with the central gear and a ring gear circumscribing the intermediate gears. A first flexible coupling is provided between an input shaft driven by a turbine section and the sun gear. The geared architecture provides a power density comprising a power measured in horsepower (HP) related to a weight of the geared architecture within a defined range that benefits overall engine weight and efficiency.</p>
申请公布号 EP2904250(A1) 申请公布日期 2015.08.12
申请号 EP20130843540 申请日期 2013.03.15
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SCHWARZ, FREDERICK M.;SHERIDAN, WILLIAM G.;LEVASSEUR, GLENN
分类号 F02K3/00;F02C3/00;F02C3/107;F02C7/00;F02C7/36;F02K99/00 主分类号 F02K3/00
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