基本信息:
- 专利标题： STRUCTURE INTERNE POUR UNE NACELLE D'UN AÉRONEF
- 专利标题（英）：Inner structure for an aircraft nacelle
- 专利标题（中）：一种平面GONDEL内部结构
- 申请号：EP11799798.1 申请日：2011-11-30
- 公开(公告)号：EP2655191A1 公开(公告)日：2013-10-30
- 发明人： HURLIN, Hervé , KERBLER, Olivier , GILO, Olivier
- 申请人： Aircelle
- 申请人地址： Route du Pont 8 76700 Gonfreville L'Orcher FR
- 专利权人： Aircelle
- 当前专利权人： Aircelle
- 当前专利权人地址： Route du Pont 8 76700 Gonfreville L'Orcher FR
- 代理机构： Gaillarde, Frédéric F. Ch.
- 优先权： FR1060816 20101220
- 国际公布： WO2012085379 20120628
- 主分类号： B64D33/04
- IPC分类号： B64D33/04 ; F02K1/08
摘要：
The invention relates to an inner structure (8) for a nacelle (1) for a aircraft turbofan including a plurality of active (103) and passive (101) movable elements. Each active movable element (103) consists of one or more movable portions (103a, 103b), and each active movable element (103) is configured so as to drive the adjacent passive movable elements (101) such that the inner structure (103) has a nominal first position, a second position in which the active movable elements (103) project beyond by the passive movable elements (101) toward the outside of the inner structure (8), and a third position in which the active movable elements (103) project beyond the passive movable elements (101) toward the inside of the inner structure (8). The invention also relates to a nacelle comprising an outer structure and such an inner structure.
IPC结构图谱:
| B | 作业；运输 |
| --B64 | 飞行器；航空；宇宙航行 |
| ----B64D | 用于与飞机配合或装到飞机上的设备；飞行衣；降落伞；动力装置或推进传动装置的配置或安装 |
| ------B64D33/00 | 其他类目不包含的动力装置部件或辅助设备在飞机内的布置 |
| --------B64D33/04 | .排气口或尾喷管的 |