发明名称 REAR BEARING SLEEVE FOR GAS TURBINE AUXILIARY POWER UNIT
摘要 The presently disclosed embodiments utilize a rear bearing sleeve interposed between an inner surface of an exhaust housing of a gas turbine auxiliary power unit and the rear roller bearing supporting a turbine within the exhaust housing. In some embodiments, the rear bearing sleeve includes a lubricant supply channel formed in an outer surface thereof for receipt of a supply of lubricant, and at least one lubricant supply opening between the outer surface and an inner surface thereof, the inner surface of the bearing sleeve forming an outer race of the rear roller bearing. The at least one lubricant supply opening supplies the lubricant to a gap between the rear roller bearing and the rear bearing sleeve for formation of a squeeze film viscous damper therebetween.
申请公布号 US2016040554(A1) 申请公布日期 2016.02.11
申请号 US201414780171 申请日期 2014.03.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Hovhannisian Ara J.;Schade Christine Ingrid;Herfort Walter
分类号 F01D25/16;F16C19/26;F01D25/18;F16C33/66 主分类号 F01D25/16
代理机构 代理人
主权项 1. A gas turbine auxiliary power unit, comprising: a turbine; an exhaust housing; a bearing disposed between the turbine and the exhaust housing; and a bearing sleeve disposed between the bearing and the exhaust housing; wherein the turbine is at least partially supported by the bearing and the bearing bears upon the bearing sleeve.
地址 Hartford CT US