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31. 发明授权

EP2739527B1 AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM WITH FLUID FILLING SYSTEM 有权
标题翻译：具有流体灌装系统的自主智能监控检测和有效载荷传送系统
公开(公告)号：EP2739527B1
公开(公告)日：2017-10-25
申请号：EP12866919.9
申请日：2012-08-06
申请人： Silicis Technologies Inc.
发明人： STIGLER, Michael, J. , SETAR, Nicholas, James
IPC分类号： B64B1/00
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system and associated operating method is disclosed including a ground station and one or more autonomous aerial vehicles. Each automomous vehicle is adapted to a) self-monitor a plurality of environment data; b) calculate, based at least in part upon the environment data, a soft wall radius from which it can return to the command and control interface station; c) receive a destination position to which it is commanded to fly; d) determine if the destination position is beyond the soft wall radius; and e) communicate an alert to the command and control interface station if the destination position is beyond the soft wall radius.

32. 发明公开

EP3109151A1 SYSTEMS AND METHODS FOR BUOYANCY MANAGEMENT IN AN AIRSHIP 有权
标题翻译： EINEM LUFTSCHIFF系统中的VERFAHREN ZUR AUFTRIEBSVERWALTUNG
公开(公告)号：EP3109151A1
公开(公告)日：2016-12-28
申请号：EP16179714.7
申请日：2010-03-12
申请人： Lockheed Martin Corporation
发明人： Greiner, Douglas H.
IPC分类号： B64B1/00 , B64B1/60 , B64B1/62 , B64B1/64 , B60V3/08
CPC分类号： B64B1/005 , B60V3/08 , B64B1/60 , B64B1/62 , B64B1/64 , B64B2201/00
摘要： An airship comprising a hull (102, 104) configured to be inflated with a first gas; a ballonet (106, 108) in the hull, the ballonet configured to be inflated with a second gas that is heavier than the first gas; a fan (118, 120) configured to draw the second gas into the ballonet; an inflatable landing system (122, 124); a duct (110, 112) configured in the ballonet to allow access to components in the airship; and a valve (126, 128) coupled to the ballonet. The valve provides a pathway for air to flow between the ballonet and a plenum chamber (130), the plenum chamber is formed by the airship, a landing surface, and the inflatable landing system when the inflatable landing system is in contact with the landing surface.
摘要翻译：一种飞艇，包括构造成用第一气体充气的船体（102,104）; 在所述船体中的气球（106,108），所述气球被配置为用比所述第一气体重的第二气体充气; 风扇（118,120），其构造成将第二气体吸入气囊; 充气着陆系统（122,124）; 构造在所述气球中以允许接近所述飞艇内的部件的管道（110,112）; 以及联接到所述气球的阀（126,128）。阀提供通道，用于空气在气球和增压室（130）之间流动，通气室由飞艇，着陆面以及充气着陆系统形成，当充气着陆系统与着陆面接触时。

33. 发明公开

EP2230173A2 Systems and methods for buoyancy management in an airship 有权转让
标题翻译： Systeme und Verfahren zur Auftriebssteuerung in einem Luftschiff
公开(公告)号：EP2230173A2
公开(公告)日：2010-09-22
申请号：EP10156400.3
申请日：2010-03-12
申请人： Lockheed Martin Corporation (Maryland Corp.)
发明人： Greiner, Douglas H
IPC分类号： B64B1/00 , B64B1/60 , B64B1/62 , B64B1/64
CPC分类号： B64B1/005 , B60V3/08 , B64B1/60 , B64B1/62 , B64B1/64 , B64B2201/00
摘要： An airship comprising a hull (102,104) configured to be inflated with a first gas; a ballonet (106,108) in the hull, the ballonet configured to be inflated with a second gas that is heavier than the first gas; a fan (118,120) configured to draw the second gas into the ballonet; an inflatable landing system (122,124); a duct (110,112) configured in the ballonet to allow access to components in the airship; and a valve (126,128) coupled to the ballonet. The valve provides a pathway for air to flow between the ballonet and a plenum chamber (130), the plenum chamber is formed by the airship, a landing surface, and the inflatable landing system when the inflatable landing system is in contact with the landing surface.
摘要翻译：一种飞艇，包括构造成用第一气体充气的船体（102,104）在所述船体中的气球（106,108），所述气球被配置为用比所述第一气体重的第二气体充气; 风扇（118,120），其构造成将第二气体吸入气囊; 充气着陆系统（122,124）; 配置在所述气球中以允许接近所述飞艇中的部件的管道（110,112）; 以及联接到所述气球的阀（126,128）。阀提供通道，用于空气在气球和增压室（130）之间流动，通气室由飞艇，着陆面以及充气着陆系统形成，当充气着陆系统与着陆面接触时。

34. 发明公开

EP1667900A2 SYSTEM AND APPLICATIONS OF LIGHTER-THAN-AIR (LTA) PLATFORMS 审中-公开
标题翻译：系统和轻于AIR平台的应用
公开(公告)号：EP1667900A2
公开(公告)日：2006-06-14
申请号：EP04789367.2
申请日：2004-09-30
申请人： Space Data Corporation
发明人： KNOBLACH, Gerald, M. , FRISCHE, Eric, A. , BARKLEY, Bruce, A.
IPC分类号： B64B1/00
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.

35. 发明申请

WO2013112198A2 AUTONOMOUS INTELLIGENCE SURVEILLANCE RECONNAISSANCE AND PAYLOAD DELIVERY SYSTEM AND METHOD OF USING SAME 审中-公开
标题翻译：自动智能监控和付费交付系统及其使用方法
公开(公告)号：WO2013112198A2
公开(公告)日：2013-08-01
申请号：PCT/US2012/049790
申请日：2012-08-06
申请人： SILICIS TECHNOLOGIES, INC. , STIGLER, Michael, J. , SETAR, Nicholas, James
发明人： STIGLER, Michael, J. , SETAR, Nicholas, James
IPC分类号： B26D1/00
CPC分类号： B64B1/12 , B64B1/005 , B64B1/10 , B64B1/14 , B64B1/18 , B64B1/22 , B64B1/24 , B64B1/36 , B64B1/60 , B64B1/62 , B64B1/64 , B64B1/66 , B64C39/024 , B64C2201/022 , B64C2201/126 , B64C2201/127 , B64C2201/141 , G05D1/0027 , G05D1/101 , G08G5/0069 , G09F21/04 , G09F21/06
摘要： An intelligence, surveillance, and reconnaissance system is disclosed including a ground station and one or more aerial vehicles. The aerial vehicles are autonomous systems capable of communicating intelligence data to the ground station and be used as part of a missile delivery package. A plurality of aerial vehicles can be configured to cast a wide net of reconnaissance over a large area on the ground including smaller overlapping reconnaissance areas provided by each of the plurality of the aerial vehicles.
摘要翻译：披露了一个智能，监视和侦察系统，包括地面站和一个或多个空中飞行器。飞行器是能够将情报数据传送到地面站的自主系统，并用作导弹发射包的一部分。多个飞行器可以被配置为在地面上的大面积上施放广泛的侦察网，包括由多个飞行器中的每一个提供的较小的重叠侦察区域。

36. 发明申请

WO2011117619A2 AERIAL VEHICLE AND METHOD OF FLIGHT 审中-公开
标题翻译：空中客车和飞行方法
公开(公告)号：WO2011117619A2
公开(公告)日：2011-09-29
申请号：PCT/GB2011/050562
申请日：2011-03-22
申请人： ATHENE WORKS LIMITED , DEAKIN, Nicholas James
发明人： DEAKIN, Nicholas James
IPC分类号： B64B1/62
CPC分类号： B64B1/02 , B64B1/08 , B64B1/10 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/38 , B64B1/64 , B64B2201/00 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/165 , B64C2201/167 , H01Q1/36 , H01Q9/27
摘要： An aerial vehicle is described which comprises: a first compartment for holding a lighter than air gas; a second compartment for holding atmospheric air and having an inlet and an outlet; a solar panel for converting sunlight into electricity; a compressor for pumping atmospheric air through the inlet into the second compartment; control means for controlling the pitch and yaw of the vehicle; and a controller for controlling the buoyancy of the vehicle via the compressor and the outlet such that the vehicle is either lighter than the surrounding air and rising or heavier than the surrounding air and falling, and for controlling the control means such that the rising and falling motion includes a horizontal component. In another embodiment the solar panel is replaced by an engine and a fuel tank for storing fuel for the engine is also provided. The aerial vehicle can remain airborne for extended periods by using buoyancy propulsion. In the embodiments including a solar panel, a system including a light transmission station may be provided to supply energy to the solar panel from the light transmission station rather than relying on the incident sunlight alone. A method of flight using buoyancy propulsion is also described.
摘要翻译：描述了一种飞行器，其包括：用于保持比空气气体轻的第一隔室; 用于容纳大气并具有入口和出口的第二隔室; 用于将阳光转化为电的太阳能电池板; 用于将大气通过所述入口泵送到所述第二隔室中的压缩机; 用于控制车辆的俯仰和偏航的控制装置; 以及用于经由压缩机和出口控制车辆的浮力的控制器，使得车辆比周围空气要轻，并且比周围空气上升或者重，并且下降，并且用于控制控制装置使得上升和下降运动包括水平分量。在另一个实施例中，太阳能电池板被发动机代替，并且还提供了用于储存用于发动机的燃料的燃料箱。航空器可以通过使用浮力推进长时间保持空中。在包括太阳能电池板的实施例中，可以提供包括光传输站的系统，以从光传输站向太阳能电池板提供能量，而不是仅依赖于入射的太阳光。还描述了使用浮力推进的飞行方法。

37. 发明申请

WO2005032936A3 SYSTEM AND APPLICATIONS OF LIGHTER-THAN-AIR (LTA) PLATFORMS 审中-公开
标题翻译：轻型（LTA）平台的系统和应用
公开(公告)号：WO2005032936A3
公开(公告)日：2008-12-18
申请号：PCT/US2004032206
申请日：2004-09-30
申请人： SPACE DATA CORP , KNOBLACH GERALD M , FRISCHE ERIC A , BARKLEY BRUCE A
发明人： KNOBLACH GERALD M , FRISCHE ERIC A , BARKLEY BRUCE A
IPC分类号： G05D1/00 , B64B20060101 , B64B1/40 , B64B1/44 , B64B1/64 , B64B1/70 , H04B7/185 , H04W4/02
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
摘要翻译：提供了与轻于空气（LTA）自由浮动平台相关的创新新方法，便于合法的变送器操作，适当的平台飞行终止，环境可接受的着陆和这些设备的恢复。新的系统和方法涉及上升速率控制，LTA平台的地理位置，包括着陆有效载荷和地面车辆位置以及可操纵的恢复系统。

38. 发明申请

WO2005032936A2 SYSTEM AND APPLICATIONS OF LIGHTER-THAN-AIR (LTA) PLATFORMS 审中-公开
标题翻译：轻型（LTA）平台的系统和应用
公开(公告)号：WO2005032936A2
公开(公告)日：2005-04-14
申请号：PCT/US2004/032206
申请日：2004-09-30
申请人： SPACE DATA CORPORATION , KNOBLACH, Gerald, M. , FRISCHE, Eric, A. , BARKLEY, Bruce, A.
发明人： KNOBLACH, Gerald, M. , FRISCHE, Eric, A. , BARKLEY, Bruce, A.
IPC分类号： B64B
CPC分类号： G01S5/06 , B64B1/40 , B64B1/44 , B64B1/62 , B64B1/64 , B64B1/70 , B64C19/00 , G01S5/12 , G01S19/42 , G05D1/042 , H04B7/18502 , H04B7/18504 , H04B7/18576 , H04W4/023 , H04W4/027
摘要： Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
摘要翻译：提供了与轻于空气（LTA）自由浮动平台相关的创新新方法，便于合法的变送器操作，适当的平台飞行终止，环境可接受的着陆和这些设备的恢复。新的系统和方法涉及上升速率控制，LTA平台的地理位置，包括着陆有效载荷和地面车辆位置以及可操纵的恢复系统。

39. 发明申请

WO2002087112A2 UNMANNED LIGHTER-THAN-AIR SAFE TERMINATION AND RECOVERY METHODS 审中-公开
标题翻译：不安全的照明安全终止和恢复方法
公开(公告)号：WO2002087112A2
公开(公告)日：2002-10-31
申请号：PCT/US2002/012228
申请日：2002-04-18
申请人： SPACE DATA CORPORATION , KNOBLACH, Gerald, M. , FRISCHE, Eric, A.
发明人： KNOBLACH, Gerald, M. , FRISCHE, Eric, A.
IPC分类号： H04B7/185
CPC分类号： G05D1/042 , B64B1/40 , B64B1/44 , B64B1/64 , B64B1/70 , G01S19/13 , H04B7/18504
摘要： Innovative new methods in connection with lighter-than-air free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. Especially, termination of radio transmissions and flight related to regional, governmental and international border requirements, regulations and laws. The new methods comprise specific criteria, detection of the criteria and elements of operation for reducing or preventing illegal transmissions, for producing rapid descend to the ground, for environmentally acceptable landing and for facilitating recovery all with improved safety and enhanced compliance with known regulations.
摘要翻译：提供了与轻于空气的浮动平台相关的创新的新方法，便于合法的变送器操作，适当的平台飞行终止，环境可接受的着陆以及这些设备的恢复。特别是终止与区域，政府和国际边界要求，条例和法律有关的无线电传输和飞行。新方法包括具体标准，检测用于减少或防止非法传输的标准和操作要素，用于快速下降到地面，环境可接受的着陆和便于恢复，所有这些都是通过改进的安全性和加强对已知规定的遵守。

40. 发明授权

KR101913719B1 부양장치가 장착된 드론 有权
公开(公告)号：KR101913719B1
公开(公告)日：2018-10-31
申请号：KR1020170085646
申请日：2017-07-05
申请人： 공주대학교 산학협력단
发明人： 박성영
IPC分类号： B64C39/02 , B64C27/08 , B64D43/00 , B64C27/12 , B64D47/08 , B64D1/22 , B64B1/62 , B64B1/64
CPC分类号： B64C39/024 , B64B1/62 , B64B1/64 , B64C27/08 , B64C27/12 , B64C2201/024 , B64C2201/101 , B64C2201/108 , B64D1/22 , B64D43/00 , B64D47/08
摘要： 부양장치가장착된드론이개시된다. 본발명에따른부양장치가장착된드론은, 원격제어장치와제어신호를상호통신하면서공중비행하여물품을이동시키는것으로, 회전력에의해양력을발생시켜공중비행하면서사용자가원하는방향으로이동되도록구비되는비행수단과, 상기비행수단이양측에결합되어공중비행되면서원격제어장치와제어신호를상호통신하는드론몸체와, 상기드론몸체의상부일측에구비되어제어신호에의해부양력이가변되도록기체를주입또는배출시키는부양조절장치를포함하여구성된다. 이에따르면, 사용자에의해원격제어되어공중을비행함으로교통체증등에따른이동의지연이발생되지않으며, 공기보다가벼운기체가충전되는부력구가구비되어중량물의운반시무게로인해드론에가해지는하중을저감시켜드론의비행을용이하게하고, 배터리에충전된전기에너지가방전되어드론의회전익이작동을정지하여도부력구에충전된기체로인해지상으로서서히하강되므로드론의추락으로인한기물및 드론의파손과인명피해와같은안전사고를방지하는효과가있다.

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