发明名称 Turbofan engine bearing support
摘要 <p>A turbofan engine (20) comprises an engine case (22). A gaspath extends through the engine case (22). A fan (42) has a circumferential array of fan blades (100). A fan case (40) encircles the fan blades (100) radially outboard of the engine case (22). A plurality of fan case vanes (44) extend outward from the engine case (22) to the fan case (40). A front frame assembly (172) includes a plurality of vanes (173) extending radially across the gaspath. A transmission (46) couples a shaft (25) to a fan shaft (132) to drive the fan (42). A bearing assembly (176) couples the shaft (25) to the front frame assembly (172). A bearing support (454) extends aftward and radially inward from the front frame assembly (172) to the bearing assembly (176). </p>
申请公布号 EP2535528(A3) 申请公布日期 2014.02.19
申请号 EP20120172460 申请日期 2012.06.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 REINHARDT, GREGORY E.;DIBENEDETTO, ENZO;MAZANEC, JASON W.
分类号 F01D25/16;F02C7/36 主分类号 F01D25/16
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