发明名称 |
REDUCED TRIM FLOW GAS TURBINE ENGINE OIL SYSTEM |
摘要 |
A disclosed lubrication system for a gas turbine engine includes a primary passage defining a flow path for lubricant to a gas turbine engine and a bypass passage defining a flow path for lubricant around the gas turbine engine. The lubrication system further includes a primary lubrication pump including a reduced total flow capacity of lubricant with a reduced bypass lubricant flow relative to the total overall flow capacity. |
申请公布号 |
EP2900958(A4) |
申请公布日期 |
2015.11.18 |
申请号 |
EP20130840271 |
申请日期 |
2013.09.24 |
申请人 |
UNITED TECHNOLOGIES CORPORATION;JAMES, DENMAN H.;GLAHN, JORN A. |
发明人 |
JAMES, DENMAN H.;GLAHN, JORN A. |
分类号 |
F02C7/06;F01D25/18;F01D25/20 |
主分类号 |
F02C7/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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