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1. 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。

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

US5276447A Radar echo reduction device 失效
标题翻译：雷达回波减速装置
公开(公告)号：US5276447A
公开(公告)日：1994-01-04
申请号：US868738
申请日：1992-04-15
申请人： Mika Shingo
发明人： Mika Shingo
IPC分类号： B64D7/00 , F41H3/00 , F41H11/00 , G01S7/38 , H01Q17/00
CPC分类号： F41H3/00 , F42B7/00 , H01Q17/00
摘要： Radar echo reduction in an aircraft and the like provides a radar reflective rear edge that is independent of the configuration of a main wing or the like. In a particular object required to suppress radar echoes such as, for example, an aircraft, a ship such as a warship, a special vehicle, a bridge or the like, the radar echo reduction constituent is a conductive thin layer equipped on an outer surface of the object and having its terminal rear edge oriented obliquely to the expected direction of an incoming radar wave.
摘要翻译：飞机等中的雷达回波减少提供了独立于主翼等的构造的雷达反射后缘。在抑制诸如飞机，诸如军舰，特种车辆，桥梁等的船舶的雷达回波所需的特定对象中，雷达回波减少构件是设置在外表面上的导电薄层并且其终端后缘倾斜于入射雷达波的预期方向定向。

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