发明名称 REACTEUR, NOTAMMENT REACTEUR POUR AERONEF
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.
申请公布号 FR2945316(B1) 申请公布日期 2013.01.04
申请号 FR20090003942 申请日期 2009.08.12
申请人 AGUILAR MICHEL 发明人 AGUILAR MICHEL
分类号 F02C5/12;F02K7/06;F23R3/44 主分类号 F02C5/12
代理机构 代理人
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