基本信息:
- 专利标题： AVION À EMPENNAGE QUEUE-DE-MORUE ET MOTEUR ARRIÈRE
- 专利标题（英）：Airplane with a tailcoat tail assembly and rear engine
- 专利标题（中）：与白色领带和尾排列HECKMOTOR PLANE
- 申请号：EP10716387.5 申请日：2010-03-12
- 公开(公告)号：EP2406133A1 公开(公告)日：2012-01-18
- 发明人： CAZALS, Olivier , GENTY DE LA SAGNE, Jaime
- 申请人： Airbus Operations (S.A.S.)
- 申请人地址： 316, route de Bayonne 31060 Toulouse FR
- 专利权人： Airbus Operations (S.A.S.)
- 当前专利权人： Airbus Operations (S.A.S.)
- 当前专利权人地址： 316, route de Bayonne 31060 Toulouse FR
- 代理机构： Maupilier, Didier
- 优先权： FR0951561 20090312
- 国际公布： WO2010103252 20100916
- 主分类号： B64D27/20
- IPC分类号： B64D27/20
摘要：
The invention relates to an airplane (1), comprising a fuselage (2) having an elongate shape along a longitudinal axis X of the airplane, and at least one wing (3) attached to the fuselage between a front end and a back end (25) of the fuselage. The fuselage (2) comprises a substantially cylindrical central portion (21) and a rear scaleable portion (23) on which a vertical tail assembly (4, 4a) and a rear propulsion assembly are attached. Between a section (231) for connecting the rear portion (23) to the central portion (21) of the fuselage and the back end (25): the maximum width of each fuselage section is constant or increases towards the rear up to a maximum fuselage width L; the height of each fuselage section decreases towards the rear, such that the back end of the fuselage forms a thin trailing edge that is substantially horizontal in the indicating line of the airplane and substantially rectilinear; a reactor (51) for the propulsion assembly is provided in a so-called semi-buried configuration in the fuselage.
公开/授权文献:
- EP2406133B1 AVION À EMPENNAGE QUEUE-DE-MORUE ET MOTEUR ARRIÈRE 公开/授权日：2013-01-16
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 |
| ------B64D27/00 | 飞机上动力装置的布置或安装；以此为特点的飞机 |
| --------B64D27/02 | .以动力装置类型或位置为特点的飞机 |
| ----------B64D27/04 | ..活塞式的 |
| ------------B64D27/20 | ...在机身内部或与机身连接的 |