发明名称 EPICYCLIC GEAR TRAIN
摘要 A turbine engine has a fan shaft. At least one tapered bearing is mounted on the fan shaft. The fan shaft includes at least one passage extending in a direction having at least a radial component, and adjacent the at least one tapered bearing. A fan is mounted for rotation on the tapered bearing. An epicyclic gear train is coupled to drive the fan. The epicyclic gear train includes a carrier supporting intermediate gears that mesh with a sun gear. A ring gear surrounds and meshes with the intermediate gears. Each of the intermediate gears are supported on a respective journal bearing. The epicyclic gear train defines a gear reduction ratio of greater than or equal to about 2.3. A turbine section is coupled to drive the fan through the epicyclic gear train. The turbine section has a fan drive turbine that includes a pressure ratio that is greater than about 5. The fan includes a pressure ratio that is less than about 1.45, and the fan has a bypass ratio of greater than about ten (10).
申请公布号 CA2936576(A1) 申请公布日期 2017.02.12
申请号 CA20162936576 申请日期 2016.07.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MCCUNE, MICHAEL E.;PORTLOCK, LAWRENCE E.;SCHWARZ, FREDERICK M.
分类号 F02C7/36;F02C7/06 主分类号 F02C7/36
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