| 发明名称 |
AIRCRAFT ENGINE HAVING A DEVICE FOR SEPARATING OIL |
| 摘要 |
An aircraft engine having at least two shafts, each mounted rotatably about a center axis of the aircraft engine. A first shaft is driven, during operation of the aircraft engine, at a lower speed than a second shaft of the aircraft engine. A chamber limited at least in some areas by one of the shafts is provided, inside which is arranged a device for separating oil from an air-oil volume flow, said device being in operative connection with one of the shafts of the aircraft engine. The device for separating oil is in operative connection with the second shaft of the aircraft engine. |
| 申请公布号 |
US2016177825(A1) |
申请公布日期 |
2016.06.23 |
| 申请号 |
US201514955235 |
申请日期 |
2015.12.01 |
| 申请人 |
Rolls-Royce Deutschland Ltd & Co KG |
发明人 |
BURGHARDT Sascha |
| 分类号 |
F02C7/06;F02C7/36;F01M11/03;F02C3/107 |
主分类号 |
F02C7/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft engine having at least two shafts, each mounted rotatably about a center axis of the aircraft engine, where a first shaft has, during operation of the aircraft engine, a lower speed than a second shaft of the aircraft engine, and where a chamber limited at least in some areas by one of the shafts is provided, inside which is arranged a device for separating oil from an air-oil volume flow, said device being in operative connection with one of the shafts of the aircraft engine, wherein the device for separating oil is in operative connection with the second shaft of the aircraft engine. |
| 地址 |
Blankenfelde-Mahlow DE |
