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 |
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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 |