| 发明名称 |
INTERFACE DEVICE BETWEEN TWO TURBOMACHINE ELEMENTS |
| 摘要 |
The main purpose of the invention is an interface device (1) between first (2) and second (3) turbomachine elements, characterised in that it comprises an annular air inlet structure (4) comprising opposite first (5) and second (6) parts, designed to come into contact with first (2) and second (3) turbomachine elements respectively, the first part (5) being configured to be in swivel contact with the first element (2), and an elastic return device (7) that can be placed around the air inlet structure (4) and designed to come into contact with at least the first turbomachine element (2). |
| 申请公布号 |
US2014348637(A1) |
申请公布日期 |
2014.11.27 |
| 申请号 |
US201414280801 |
申请日期 |
2014.05.19 |
| 申请人 |
SNECMA |
发明人 |
COHIN Arthur;CHARRIE Audrey;GANT Florent;MASSOT Aurelien Rene-Pierre |
| 分类号 |
F01D11/24 |
主分类号 |
F01D11/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. Interface device between first and second turbomachine elements, wherein it comprises:
an annular air inlet structure comprising opposite first and second parts, designed to come into contact with first and second turbomachine elements respectively, the first part being configured to be in swivel contact with the first element, and an elastic return device, that can be placed around the air inlet structure and that will come into contact with at least the first element of the turbomachine. |
| 地址 |
Paris FR |
