基本信息:
- 专利标题： REACTEUR NOTAMMENT UN REACTEUR POUR AERONEF
- 专利标题（英）：Jet engine, in particular a jet engine for an aircraft
- 专利标题（中）：与等容烧伤飞机的喷气发动机
- 申请号：EP10700712.2 申请日：2010-01-15
- 公开(公告)号：EP2391802A1 公开(公告)日：2011-12-07
- 发明人： Aguilar, Michel
- 申请人： Aguilar, Michel
- 申请人地址： 33 rue Marcel Pagnol 31320 Castanet Tolosan FR
- 专利权人： Aguilar, Michel
- 当前专利权人： Aguilar, Michel
- 当前专利权人地址： 33 rue Marcel Pagnol 31320 Castanet Tolosan FR
- 代理机构： Junca, Eric
- 优先权： FR0900330 20090127; FR0903942 20090812
- 国际公布： WO2010086091 20100805
- 主分类号： F01D17/14
- IPC分类号： F01D17/14 ; F02C5/12 ; F02K9/40 ; F02K7/02
摘要：
The invention relates to a jet engine (1), in particular an aircraft jet engine, including at least one combustion chamber (3). The combustion chamber (3) is connected to at least one compressed gas intake (4) and to at least one burnt gas outlet (5). Said burnt gas outlet(s) (5) include an exhaust valve. The exhaust valve includes two rotary parts (7), referred to as rotary exhaust parts, the rotary exhaust parts (7) including curved walls (8) and intermediate walls (9) connecting the curved walls (8), and rotating in a coordinated, continuous fashion such that said valve is in a closed position in order to block the gas during at least one combustion step, and in an open position in order to define a space (10) through which the gas flows out from the combustion chamber (3) during at least one expansion step.
IPC结构图谱:
| F | 机械工程；照明；加热；武器；爆破 |
| --F01 | 一般机器或发动机；一般的发动机装置；蒸汽机 |
| ----F01D | 非变容式机器或发动机，如汽轮机 |
| ------F01D17/00 | 通过改变流量进行调节或控制 |
| --------F01D17/02 | .敏感元件布置 |
| ----------F01D17/12 | ..装在定子部件内的 |
| ------------F01D17/14 | ...变化喷嘴或导管的有效横截面积 |