| 发明名称 |
AIRCRAFT ENGINE WITH AN APPARATUS FOR SEPARATING OIL AND A DEVICE FOR INCREASING PRESSURE |
| 摘要 |
An aircraft engine having a device for separating oil from an air-oil volume flow, where a fluid volume flow with a lower oil load than the air-oil volume flow supplied to the device can be discharged from the device via a line area. The fluid volume flow can be supplied via the line area to a unit by means of which a pressure in the line area downstream of the unit can be increased. |
| 申请公布号 |
US2016158679(A1) |
申请公布日期 |
2016.06.09 |
| 申请号 |
US201514959179 |
申请日期 |
2015.12.04 |
| 申请人 |
Rolls-Royce Deutschland Ltd & Co KG |
发明人 |
BEIER Juergen;VENTER Gideon |
| 分类号 |
B01D45/12;F01D25/18;F01D15/12;B64D27/10 |
主分类号 |
B01D45/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft engine having a device for separating oil from an air-oil volume flow, where a fluid volume flow with a lower oil load than the air-oil volume flow supplied to the device can be discharged from the device via a line area wherein the fluid volume flow can be supplied via the line area to a unit by means of which a pressure in the line area downstream of the unit can be increased. |
| 地址 |
Blankenfelde-Mahlow DE |
