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1. 发明授权

US08220249B2 Rocket nozzle and control method for combustion gas flow in rocket engine 有权
标题翻译：火箭发动机燃烧气体流量的火箭喷嘴和控制方法
公开(公告)号：US08220249B2
公开(公告)日：2012-07-17
申请号：US12200265
申请日：2008-08-28
申请人： Tatsuya Kimura , Yoshihiro Kawamata , Kenichi Niu
发明人： Tatsuya Kimura , Yoshihiro Kawamata , Kenichi Niu
IPC分类号： B64G1/40
CPC分类号： F02K1/38 , F02K9/48 , F02K9/58 , F02K9/82 , F02K9/972 , F05D2250/713
摘要： A rocket nozzle includes a dual-bell nozzle and a gas introducing section configured to introduce gas into space surrounded by the dual-bell nozzle. Combustion gas flows in the space. The dual-bell nozzle includes a first stage nozzle bell-shaped and surrounding an upstream portion of the space, and a second stage nozzle bell-shaped and surrounding a downstream portion of the space. The dual-bell nozzle has an inflection point between the first stage nozzle and the second stage nozzle. The gas introducing section includes a gas inlet provided to an inner wall surface of the first stage nozzle. The gas is introduced into the space from the gas inlet.
摘要翻译：火箭喷嘴包括双钟形喷嘴和构造成将气体引入由双钟形喷嘴包围的空间中的气体导入部。燃烧气体在空间中流动。双钟形喷嘴包括钟形状的第一级喷嘴并且围绕该空间的上游部分，以及第二级喷嘴钟形并围绕该空间的下游部分。双钟形喷嘴在第一级喷嘴和第二级喷嘴之间具有拐点。气体导入部包括设置在第一级喷嘴的内壁面的气体入口。气体从气体入口引入空间。

2. 发明申请

US20110024548A1 LAUNCHING SYSTEM AND LAUNCHING APPARATUS 有权
标题翻译：启动系统和启动装置
公开(公告)号：US20110024548A1
公开(公告)日：2011-02-03
申请号：US12649808
申请日：2009-12-30
申请人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
发明人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
IPC分类号： B64D3/00 , B64C3/00 , B64F1/04 , B64C37/02 , B64D1/12 , B64G1/10
CPC分类号： B64D1/04 , B64D3/00 , B64G1/005
摘要： A flying object capable of being launched in air is detachably mounted on a wing body of a launching apparatus. The launching apparatus is towed by an aircraft through a cable so as to be run and taken off. After raising the launching apparatus to a launching height of the flying object by the aircraft, the flying object is released from the wing body in air and then the flying object is ignited and launched in air in a launching system. The system for launching in air can be developed without newly developing a platform as a mother ship so that a research cost can be remarkably reduced. In the case that a small artificial satellite is installed in a flying object, it is possible to develop an artificial satellite smoothly and quickly applicable to security matters and disaster observation.
摘要翻译：能够在空气中发射的飞行物体可拆卸地安装在发射装置的翼体上。发射装置由飞机通过电缆拖曳以便被运行和取下。在将发射装置升高到飞行器的飞行物体的发射高度之后，飞行物体在空中从翼体释放，然后飞行物体在发射系统中被点燃并在空气中发射。可以开发空气发射系统，而不需要开发作为母船的平台，从而大大减少研究费用。在飞行物体上安装有小型人造卫星的情况下，可以平稳，快速地开发人造卫星，从而可以安全地进行灾害观察。

3. 发明授权

US08262015B2 Launching system and launching apparatus 有权
标题翻译：发射系统和发射装置
公开(公告)号：US08262015B2
公开(公告)日：2012-09-11
申请号：US12649808
申请日：2009-12-30
申请人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
发明人： Yoshikatsu Kuroda , Yoshihiro Kawamata , Mika Shingo
IPC分类号： B64D3/00
CPC分类号： B64D1/04 , B64D3/00 , B64G1/005
摘要： A flying object capable of being launched in air is detachably mounted on a wing body of a launching apparatus. The launching apparatus is towed by an aircraft through a cable so as to be run and taken off. After raising the launching apparatus to a launching height of the flying object by the aircraft, the flying object is released from the wing body in air and then the flying object is ignited and launched in air in a launching system. The system for launching in air can be developed without newly developing a platform as a mother ship so that a research cost can be remarkably reduced. In the case that a small artificial satellite is installed in a flying object, it is possible to develop an artificial satellite smoothly and quickly applicable to security matters and disaster observation.
摘要翻译：能够在空气中发射的飞行物体可拆卸地安装在发射装置的翼体上。发射装置由飞机通过电缆拖曳以便被运行和取下。在将发射装置升高到飞行器的飞行物体的发射高度之后，飞行物体在空中从翼体释放，然后飞行物体在发射系统中被点燃并在空气中发射。可以开发空气发射系统，而不需要开发一个作为母船的平台，从而可以显着降低研究成本。在飞行物体上安装小型人造卫星的情况下，可以平稳，快速地开发人造卫星用于安全事项和灾害观察。

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