| 摘要 |
The invention relates to a protection system for a turbo engine, in particular an aircraft engine, said turbo engine comprising at least one fluid duct element, characterized by a casing device (1) comprising at least one casing section (2), encasing at least partially the at least one fluid duct element (3), said casing device (1) comprising at least one fluid escaping means (4), wherein the casing device (1) is intended to at least partially contain and/or deflect a fluid (F) stemming from a burst event at the fluid duct element (3) event in order to at least partially protect the turbo engine. |
