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1. 发明申请

US20050284127A1 Detonation engine and flying object provided therewith 有权
标题翻译：引爆引擎和飞行物体
公开(公告)号：US20050284127A1
公开(公告)日：2005-12-29
申请号：US11143495
申请日：2005-06-03
申请人： Akihiro Tobita , Toshitaka Fujiwara , Piotr Wolanski
发明人： Akihiro Tobita , Toshitaka Fujiwara , Piotr Wolanski
IPC分类号： C23C4/12 , C23C24/04 , F01D5/02 , F02C3/14 , F02K3/04 , F02K5/02 , F02K7/00 , F02K7/02
CPC分类号： F02K7/02 , C23C4/126 , C23C24/04 , F01D5/022 , F02K3/04 , F02K7/00
摘要： A detonation engine which creates thrust by generating a detonation wave, wherein the overall engine structure is simplified, and continuous output can be obtained, comprises: a rotational flow generation device which generates rotational flow about an axis in a mixed gas of air and fuel or of oxygen and fuel; a detonation chamber arranged downstream from the rotational flow generation device, formed in a ring-shape radially extended and continuous in the circumferential direction, which continuously combusts in the circumferential direction the mixed gas in which the rotational flow is generated to generate detonation waves, and draws it in from the radial inside and exhausts it to the radial outside; and a nozzle which is connected to the detonation chamber, and jets the high temperature and pressure combustion gas generated by the detonation waves flowing from the detonation chamber, to the rear while expanding it, and converts it into thrust.
摘要翻译：一种通过产生爆震波产生推力的引爆引擎，其中简化了整个发动机结构，并且可以获得连续的输出，包括：旋转流产生装置，其产生围绕空气和燃料的混合气体中的轴线的旋转流动，的氧气和燃料; 在所述旋转流产生装置的下游设置有形成为沿周向径向延伸且连续的环状的引爆室，所述环状体沿圆周方向连续燃烧产生旋转流的混合气体以产生爆震波，以及从径向内部吸入，并将其排放到径向外侧; 以及与爆震室连接的喷嘴，将从爆震室流动的爆震波产生的高温高压燃烧气体喷射到后方，同时使其膨胀成推力。

2. 发明授权

US07784267B2 Detonation engine and flying object provided therewith 有权
标题翻译：引爆引擎和飞行物体
公开(公告)号：US07784267B2
公开(公告)日：2010-08-31
申请号：US11143495
申请日：2005-06-03
申请人： Akihiro Tobita , Toshitaka Fujiwara , Piotr Wolanski
发明人： Akihiro Tobita , Toshitaka Fujiwara , Piotr Wolanski
IPC分类号： F02K5/02 , F02C5/02
CPC分类号： F02K7/02 , C23C4/126 , C23C24/04 , F01D5/022 , F02K3/04 , F02K7/00
摘要： A detonation engine which creates thrust by generating a detonation wave, wherein the overall engine structure is simplified, and continuous output can be obtained, comprises: a rotational flow generation device which generates rotational flow about an axis in a mixed gas of air and fuel or of oxygen and fuel; a detonation chamber arranged downstream from the rotational flow generation device, formed in a ring-shape radially extended and continuous in the circumferential direction, which continuously combusts in the circumferential direction the mixed gas in which the rotational flow is generated to generate detonation waves, and draws it in from the radial inside and exhausts it to the radial outside; and a nozzle which is connected to the detonation chamber, and jets the high temperature and pressure combustion gas generated by the detonation waves flowing from the detonation chamber, to the rear while expanding it, and converts it into thrust.
摘要翻译：一种通过产生爆震波产生推力的引爆发动机，其中简化了整个发动机结构，并且可以获得连续的输出，包括：旋转流产生装置，其围绕空气和燃料的混合气体中的轴产生旋转流，或的氧气和燃料; 在所述旋转流产生装置的下游设置有形成为沿周向径向延伸且连续的环状的引爆室，所述环状体沿圆周方向连续燃烧产生旋转流的混合气体以产生爆震波，以及从径向内部吸入，并将其排放到径向外侧; 以及与爆震室连接的喷嘴，将从爆震室流动的爆震波产生的高温高压燃烧气体喷射到后方，同时使其膨胀成推力。

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