发明名称 DETONATION ENGINE AND FLIGHT VEHICLE EQUIPPED WITH THE SAME
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a detonation engine simplifying structure of whole engine and providing continuous output. <P>SOLUTION: This detonation engine 10 producing propulsion force by generating detonation wave is provided with a swirl generation means 13 generating swirl of mixture of atmospheric air and fuel or mixture of oxygen and fuel around axial line, a detonation chamber 14 arranged in a downstream of the swirl generation device 13 and formed in a ring shape extending in a radial direction and connecting in a circumference direction and burning mixture of which swirl is generated by the swirl generation means 13 continuously in a circumference direction to generate detonation wave and sucking air from a radial direction inside and discharging air to a radial direction outside, and a nozzle 15 connected to the detonation chamber 14 and jetting high temperature and high pressure combustion gas generated by detonation wave made flow out of the detonation chamber 14 backward while the same is being expanded to convert the same to propulsion force. <P>COPYRIGHT: (C)2006,JPO&NCIPI</p>
申请公布号 JP2006009764(A) 申请公布日期 2006.01.12
申请号 JP20040191793 申请日期 2004.06.29
申请人 MITSUBISHI HEAVY IND LTD;FUJIWARA TOSHITAKA;PIOTR WALANSKI 发明人 HIDA AKIHIRO;FUJIWARA TOSHITAKA;PIOTR WALANSKI
分类号 F02C5/02;B64D27/02;C23C4/12;C23C24/04;F01D5/02;F02C3/14;F02C5/11;F02K3/04;F02K3/062;F02K5/02;F02K7/00;F02K7/02 主分类号 F02C5/02
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