专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08028953B2 Accelerating device 有权
标题翻译：加速装置
公开(公告)号：US08028953B2
公开(公告)日：2011-10-04
申请号：US12089996
申请日：2006-10-06
申请人： Shiro Hosaka , Masatada Yamamoto , Satoshi Matsuda , Akio Yamanaka , Toshihiko Takeo
发明人： Shiro Hosaka , Masatada Yamamoto , Satoshi Matsuda , Akio Yamanaka , Toshihiko Takeo
IPC分类号： B64F1/04
CPC分类号： B64F1/10 , Y02T50/82
摘要： Providing an accelerating device capable of safely and efficiently accelerating an aircraft even if the aircraft is a high-speed and heavyweight one.The accelerating device has a support base for supporting an aircraft so that it does not go backward or levitate and does not pitch; a guide way placed along a predetermined route; guide means for guiding the support base along the guide way; and drive means for driving the support base along the guide way.
摘要翻译：提供能够安全有效地加速飞机的加速装置，即使飞机是高速和重量级的。加速装置具有用于支撑飞行器的支撑基座，使得其不会向后或悬浮并且不俯仰; 沿着预定路线放置的引导方式; 引导装置，用于沿着引导方向引导支撑基座; 以及用于沿着引导方向驱动支撑基座的驱动装置。

2. 发明申请

US20090134274A1 ACCELERATING DEVICE 有权
标题翻译：加速装置
公开(公告)号：US20090134274A1
公开(公告)日：2009-05-28
申请号：US12089996
申请日：2006-10-06
申请人： Shiro Hosaka , Masatada Yamamoto , Satoshi Matsuda , Akio Yamanaka , Toshihiko Takeo
发明人： Shiro Hosaka , Masatada Yamamoto , Satoshi Matsuda , Akio Yamanaka , Toshihiko Takeo
IPC分类号： B64F1/04
CPC分类号： B64F1/10 , Y02T50/82
摘要： [PROBLEMS] Providing an accelerating device capable of safely and efficiently accelerating an aircraft even if the aircraft is a high-speed and heavyweight one.[MEANS FOR SOLVING PROBLEMS] The accelerating device has a support base for supporting an aircraft so that it does not go backward or levitate and does not pitch; a guide way placed along a predetermined route; guide means for guiding the support base along the guide way; and drive means for driving the support base along the guide way.
摘要翻译： [问题]提供能够安全有效地加速飞机的加速装置，即使飞机是高速和重量级的。解决问题的手段加速装置具有用于支撑飞行器的支撑基座，使得其不会向后或悬浮并且不俯仰; 沿着预定路线放置的引导方式; 引导装置，用于沿着引导方向引导支撑基座; 以及用于沿着引导方向驱动支撑基座的驱动装置。

3. 发明授权

US07594624B2 Flying vehicle-launching apparatus and method 有权
标题翻译：飞行器发射装置及方法
公开(公告)号：US07594624B2
公开(公告)日：2009-09-29
申请号：US11763662
申请日：2007-06-15
申请人： Masatada Yamamoto
发明人： Masatada Yamamoto
IPC分类号： B64F1/04 , B60L13/00
CPC分类号： B64F1/04 , B64G1/002 , B64G1/14 , B64G5/00
摘要： A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways. In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.
摘要翻译：用于通过沿预定方向加速车辆来发射飞行飞行器的飞行器发射装置和方法包括飞行车辆支撑平台，引导装置和驱动装置。飞行车辆支撑平台支撑飞行的飞行器，从而可以从其上脱离。引导装置通过两个或更多个分离和平行的引导方式支撑飞行车辆支撑平台，并且沿着导向引导飞行车辆支撑平台。在飞行车辆发射方法中，利用飞行车辆加速装置启动加速后的飞行飞行器的推进发动机。飞行的飞行器以预定的攻角从飞行加速装置释放，在达到预定速度后与加速方向正相关。

4. 发明授权

US07232092B2 Flying vehicle-launching apparatus and method 有权
标题翻译：飞行器发射装置及方法
公开(公告)号：US07232092B2
公开(公告)日：2007-06-19
申请号：US10921263
申请日：2004-08-18
申请人： Masatada Yamamoto
发明人： Masatada Yamamoto
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64G1/002 , B64G1/14 , B64G5/00
摘要： A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways.In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.
摘要翻译：用于通过沿预定方向加速车辆来发射飞行飞行器的飞行器发射装置和方法包括飞行车辆支撑平台，引导装置和驱动装置。飞行车辆支撑平台支撑飞行的飞行器，从而可以从其上脱离。引导装置通过两个或更多个分离和平行的引导方式支撑飞行车辆支撑平台，并且沿着导向引导飞行车辆支撑平台。在飞行车辆发射方法中，利用飞行车辆加速装置启动加速后的飞行飞行器的推进发动机。飞行的飞行器以预定的攻角从飞行加速装置释放，在达到预定速度后与加速方向正相关。

5. 发明申请

US20080087764A1 FLYING VEHICLE-LAUNCHING APPARATUS AND METHOD 有权
标题翻译：飞行车辆起动装置和方法
公开(公告)号：US20080087764A1
公开(公告)日：2008-04-17
申请号：US11763662
申请日：2007-06-15
申请人： Masatada Yamamoto
发明人： Masatada Yamamoto
IPC分类号： B64F1/04
CPC分类号： B64F1/04 , B64G1/002 , B64G1/14 , B64G5/00
摘要： A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways. In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.
摘要翻译：用于通过沿预定方向加速车辆来发射飞行飞行器的飞行器发射装置和方法包括飞行车辆支撑平台，引导装置和驱动装置。飞行车辆支撑平台支撑飞行的飞行器，从而可以从其上脱离。引导装置通过两个或更多个分离和平行的引导方式支撑飞行车辆支撑平台，并且沿着导向引导飞行车辆支撑平台。在飞行车辆发射方法中，利用飞行车辆加速装置启动加速后的飞行飞行器的推进发动机。飞行的飞行器以预定的攻角从飞行加速装置释放，在达到预定速度后与加速方向正相关。

6. 发明申请

US20050082424A1 Flying vehicle-launching apparatus and method 有权
标题翻译：飞行器发射装置及方法
公开(公告)号：US20050082424A1
公开(公告)日：2005-04-21
申请号：US10921263
申请日：2004-08-18
申请人： Masatada Yamamoto
发明人： Masatada Yamamoto
IPC分类号： B64F1/04 , B64G1/00 , B64G1/14 , B64G5/00
CPC分类号： B64F1/04 , B64G1/002 , B64G1/14 , B64G5/00
摘要： A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways. In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.
摘要翻译：用于通过沿预定方向加速车辆来发射飞行飞行器的飞行器发射装置和方法包括飞行车辆支撑平台，引导装置和驱动装置。飞行车辆支撑平台支撑飞行的飞行器，从而可以从其上脱离。引导装置通过两个或更多个分离和平行的引导方式支撑飞行车辆支撑平台，并且沿着导向引导飞行车辆支撑平台。在飞行车辆发射方法中，利用飞行车辆加速装置启动加速后的飞行飞行器的推进发动机。飞行的飞行器以预定的攻角从飞行加速装置释放，在达到预定速度后与加速方向正相关。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式