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 |