发明名称 BEARING SYSTEM FOR GAS TURBINE ENGINE
摘要 A bearing system is provided for a gas turbine engine. This bearing system includes a spring defined about an axis of rotation. The spring has a multiple of beams which extend between a flange and a damper attachment. A damper defined about the axis of rotation and mounted to the spring to at least partially axially overlap the multiple of beams.
申请公布号 US2016186607(A1) 申请公布日期 2016.06.30
申请号 US201414910829 申请日期 2014.08.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Witlicki Russell B.;Amador Armando
分类号 F01D25/16;F01D25/28 主分类号 F01D25/16
代理机构 代理人
主权项 1. A bearing system for a gas turbine engine, comprising: a spring defined about an axis, the spring including a multiple of beams that extend between a radial flange and a damper attachment; and a damper defined about the axis, the damper fastened to the damper attachment and nested within the spring.
地址 Hartford CT US