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2. 发明申请

US20070180815A1 COMPACT, LOW PRESSURE-DROP SHOCK-DRIVEN COMBUSTOR AND ROCKET BOOSTER, PULSE DETONATION BASED SUPERSONIC PROPULSION SYSTEM EMPLOYING THE SAME 有权
标题翻译：紧凑型，低压降驱动式燃烧器和摇臂增压器，采用脉冲爆震的超声波推进系统
公开(公告)号：US20070180815A1
公开(公告)日：2007-08-09
申请号：US11554897
申请日：2006-10-31
申请人： Venkat Tangirala , Jonathan Janssen , Anthony Dean
发明人： Venkat Tangirala , Jonathan Janssen , Anthony Dean
IPC分类号： F02K7/02
CPC分类号： F02K7/02
摘要： A supersonic propulsion system is provided. The supersonic propulsion system includes a plurality of systems for efficiently creating cyclic detonations and at least one rocket booster device. Each of the systems include at least a first initiator chamber configured to generate an initial wave, at least one main chamber coupled to the first initiator chamber. The main chamber is configured to generate a main wave and to output products of supersonic combustion. The products are generated within the main chamber. The main chamber is configured to enable the main wave to travel upstream and downstream within the main chamber when the first initiator chamber is located outside the main chamber. The system further includes an initial connection section located between the first initiator chamber and the main chamber that enhances a combustion process via shock focusing and shock reflection.
摘要翻译：提供超音速推进系统。超音速推进系统包括用于有效地产生循环爆炸的多个系统和至少一个火箭增压装置。每个系统包括至少一个配置成产生初始波的第一启动器室，耦合到第一起动器室的至少一个主室。主室被配置为产生主波并输出超音速燃烧的产物。产品在主室内产生。主室被构造成使得当第一起动器室位于主室外部时，能够使主波浪在主室内的上游和下游行进。该系统还包括位于第一起动器室和主室之间的初始连接部分，其通过冲击聚焦和冲击反射增强燃烧过程。

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