发明名称 FUNDAMENTAL GEAR SYSTEM ARCHITECTURE
摘要 A fan drive gear system for a gas turbine engine includes a gear system that provides a speed reduction between a fan drive turbine and a fan and a mount flexibly supporting portions of the gear system. A lubrication system supporting the fan drive gear system provides lubricant to the gear system and removes thermal energy produced by the gear system. The lubrication system includes a capacity for removing energy equal to less than about 2% of energy input into the gear system.
申请公布号 CA2854728(C) 申请公布日期 2016.08.16
申请号 CA20142854728 申请日期 2014.06.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SHERIDAN, WILLIAM G.;MCCUNE, MICHAEL E.;SCHWARZ, FREDERICK M.;KUPRATIS, DANIEL BERNARD;SUCIU, GABRIEL L.;ACKERMANN, WILLIAM K.;HUSBAND, JASON
分类号 F02C7/36;F02C7/06 主分类号 F02C7/36
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