发明名称 Front bearing support for a fan drive gear system
摘要 A fan shaft support assembly for a gas turbine engine includes first and second bearing assembles supported by a bearing support structure. The bearing support structure includes a first support including a first support end supporting the first bearing assembly and a second support including a second support end supporting the second bearing assembly. The first support end and the second support end are spaced apart to provide a preload on the first and second bearing assemblies.
申请公布号 US9115598(B2) 申请公布日期 2015.08.25
申请号 US201213488605 申请日期 2012.06.05
申请人 United Technologies Corporation 发明人 Van Duyn Keven G.;Coffin James B.
分类号 F01D25/16 主分类号 F01D25/16
代理机构 Carlson, Gaskey & Olds, P.C. 代理人 Carlson, Gaskey & Olds, P.C.
主权项 1. A fan shaft support assembly comprising: a first bearing assembly; a second bearing assembly spaced axially apart from the first bearing assembly; a first support including a first support end disposed on a first support leg supporting the first bearing assembly, wherein the first support end is connected only to the first support leg; and a second support including a second support end disposed on a second support leg supporting the second bearing assembly, wherein the second support end is connected only to the second support leg and the first support end exerts an axial preload on the first bearing assembly and the second support end exerts an axial preload on the second bearing assembly.
地址 Hartford CT US
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