发明名称 MULTI-CIRCUIT LUBRICATION SYSTEM FOR A TURBINE ENGINE
摘要 A turbine engine system includes a first lubricant circuit, a second lubricant circuit, a plurality of engine stages and a shaft. The first lubricant circuit includes a first turbine engine component that is fluidly coupled with a first lubricant heat exchanger. The second lubricant circuit includes a second turbine engine component that is fluidly coupled with a second lubricant heat exchanger, wherein the second lubricant circuit is fluidly separate from the first lubricant circuit. The first turbine engine component includes a gear train, which connects a first of the engine stages to a second of the engine stages. The second turbine engine component includes a bearing. The shaft is supported by the bearing and connected to one of the engine stages.
申请公布号 US2015369082(A1) 申请公布日期 2015.12.24
申请号 US201414765211 申请日期 2014.02.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Schwarz Frederick M.;Pickford Simon
分类号 F01D25/20;F01D25/08;F01D15/10;F01D15/12;F01D1/02;F01D25/16 主分类号 F01D25/20
代理机构 代理人
主权项 1. A turbine engine system, comprising: a first lubricant circuit comprising a first turbine engine component fluidly coupled with a first lubricant heat exchanger, wherein the first turbine engine component comprises a gear train; a second lubricant circuit comprising a second turbine engine component fluidly coupled with a second lubricant heat exchanger, wherein the second lubricant circuit is fluidly separate from the first lubricant circuit, and the second turbine engine component comprises a bearing; a plurality of engine stages, wherein the gear train connects a first of the plurality of engine stages to a second of the plurality of engine stages; and a shaft supported by the bearing, and connected to one of the plurality of engine stages.
地址 Hartford CT US