发明名称 |
Casing cover in a jet engine |
摘要 |
A casing cover for enclosing a casing in a jet engine is disclosed. The casing cover includes two coaxial shells arranged one inside the other and radial envelopes which connect the two coaxial shells. Radial arms of the casing extend inside the radial envelopes. The cover is fastened at its downstream end to a first element of the casing and axially abuts at its upstream end on a second element of the casing. In a free state, an axial dimension of the cover of less than the axial distance of the casing between the point where the first element of the casing is fastened to the downstream end of the cover and the point where the second element of the casing axially abuts the upstream end of the cover such that the cover is tensioned axially when it is mounted on and fastened to the casing.
|
申请公布号 |
US7909573(B2) |
申请公布日期 |
2011.03.22 |
申请号 |
US20070687406 |
申请日期 |
2007.03.16 |
申请人 |
SNECMA |
发明人 |
CAMERIANO LAURENT BERNARD;DUVAL SYLVAIN;MASSON ERIC;PLISSON HERVE BERNARD |
分类号 |
F01D25/26;F01D25/24;F03D11/04 |
主分类号 |
F01D25/26 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|