发明名称 Engine Bearing Support
摘要 A turbofan engine comprises an engine case. A gaspath extends through the engine case. A fan has a circumferential array of fan blades. A fan case encircles the fan blades radially outboard of the engine case. A plurality of fan case vanes extend outward from the engine case to the fan case. A front frame assembly includes a plurality of vanes extending radially across the gaspath. A transmission couples a shaft to a fan shaft to drive the fan. A bearing assembly couples the shaft to the front frame assembly. A bearing support extends aftward and radially inward from the front frame assembly to the bearing assembly.
申请公布号 US2014301829(A1) 申请公布日期 2014.10.09
申请号 US201313970483 申请日期 2013.08.19
申请人 Reinhardt Gregory E.;DiBenedetto Enzo;Mazanec Jason W. 发明人 Reinhardt Gregory E.;DiBenedetto Enzo;Mazanec Jason W.
分类号 F02C7/06 主分类号 F02C7/06
代理机构 代理人
主权项 1. A turbofan engine comprising: an engine case; a gaspath through the engine case; a fan having a circumferential array of fan blades; a fan case encircling the fan blades radially outboard of the engine case; a plurality of fan case vanes extending outward from the engine case to the fan case; a front frame assembly comprising a plurality of vanes extending radially across the gas path; a shaft; a transmission coupling the shaft to a fan shaft to drive the fan; a bearing assembly coupling the shaft to the front frame assembly, the bearing assembly being a duplex bearing assembly; and a bearing support extending aftward and radially inward from the front frame assembly to the bearing assembly.
地址 South Glastonbury CT US