| 发明名称 |
PROTECTION SYSTEM AND TURBO ENGINE WITH A PROTECTION SYSTEM |
| 摘要 |
A protection system for a turbo engine, in particular an aircraft engine is provided. The turbo engine comprises at least one fluid duct element with a casing device comprising at least one casing section, encasing at least partially the at least one fluid duct element, said casing device comprising at least one fluid escaping means, wherein the casing device is intended to at least partially contain and/or deflect a fluid stemming from a burst event at the fluid duct element event in order to at least partially protect the turbo engine. |
| 申请公布号 |
US2016298487(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201615094234 |
申请日期 |
2016.04.08 |
| 申请人 |
Rolls-Royce Deutschland Ltd & Co KG |
发明人 |
TEIA DOS SANTOS MENDES GOMES Luis Daniel |
| 分类号 |
F01D21/14;F01D25/12;F01D25/26;F01D25/14 |
主分类号 |
F01D21/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A protection system for a turbo engine, in particular an aircraft engine, said turbo engine comprising at least one fluid duct element, with a casing device comprising at least one casing section, encasing at least partially the at least one fluid duct element, said casing device comprising at least one fluid escaping means, wherein the casing device is intended to at least partially contain and/or deflect a fluid stemming from a burst event at the fluid duct element in order to at least partially protect the turbo engine. |
| 地址 |
Blankenfelde-Mahlow DE |
