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公开(公告)号:US20120303179A1
公开(公告)日:2012-11-29
申请号:US13134009
申请日:2011-05-26
Applicant: Hagen Schempf
Inventor: Hagen Schempf
CPC classification number: B64C39/022 , B25J11/002 , B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/148 , F41H7/005 , G05D1/0038 , G05D1/0866 , G05D2201/0209
Abstract: A robot surveillance system includes a robot chassis, a drive subsystem for the chassis, a dock on the chassis, and a payout device associated with the chassis. A flying module is configured to be received in the dock and includes at least one rotor powered by a motor and a body portion including an imager. A tether is coupled to the payout device of the robot and to the flying module for allowing the flying module to climb out of the dock when powered to gain elevation for surveillance and imaging via the imager and for retracting the flying module to land on the robot and reside in the chassis dock after surveillance.
Abstract translation: 机器人监视系统包括机器人底盘,用于机箱的驱动子系统,底盘上的坞站以及与底盘相关联的支付设备。 飞行模块被配置为被接纳在码头中并且包括由马达供电的至少一个转子和包括成像器的主体部分。 系绳连接到机器人的支付装置和飞行模块,用于允许飞行模块在通电时获得升高以便通过成像器进行监视和成像并使飞行模块缩回到机器人上 并在监视后驻留在底盘底座。
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公开(公告)号:US20120112008A1
公开(公告)日:2012-05-10
申请号:US13211000
申请日:2011-08-16
Applicant: Gregory Holifield , Timothy Holifield , Alexander Barrett , Jason McKenna , Gilbert Barrett , Seth Broadfoot
Inventor: Gregory Holifield , Timothy Holifield , Alexander Barrett , Jason McKenna , Gilbert Barrett , Seth Broadfoot
CPC classification number: B64C27/02 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/148
Abstract: A high altitude tethered platform, includes an airborne subsystem having a flight platform capable of flight. A powered propeller is mounted on the flight platform. A ground subsystem having a control system, a power delivery system, and a tether system is physically and operatively coupled to the flight platform. The tether system transmits power between the control system and the flight platform.
Abstract translation: 一个高空拴系平台,包括一个具有能够飞行的飞行平台的机载子系统。 动力螺旋桨安装在飞行平台上。 具有控制系统,功率输送系统和系绳系统的地面子系统在物理上和操作上耦合到飞行平台。 系绳系统在控制系统和飞行平台之间传输电力。
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公开(公告)号:US20120037750A1
公开(公告)日:2012-02-16
申请号:US13124886
申请日:2009-04-24
Applicant: Valery Vyacheslavovich Dvoeglazov
Inventor: Valery Vyacheslavovich Dvoeglazov
CPC classification number: B66F19/00 , B64C27/20 , B64C39/022 , B64C2201/148
Abstract: The airlift comprises an engine-propeller unit and means for retention of the engine-propeller unit relative to the earth's surface, fixed on the above unit in the axis of rotation upward of the center of gravity of the engine-propeller unit. The means for retention of the engine-propeller unit relative to the earth's surface comprise solely a wire rope or a wire rope and an arm fixed inside the engine-propeller unit, or a wire rope and a frame embracing the engine-propeller unit fully or partially.
Abstract translation: 空运包括发动机 - 螺旋桨单元和用于将发动机 - 螺旋桨单元相对于地球表面保持的装置,其固定在上述单元上,在发动机 - 螺旋桨单元的重心的上方。 用于保持发动机 - 螺旋桨单元相对于地球表面的装置仅包括固定在发动机 - 螺旋桨单元内的钢丝绳或钢丝绳和臂,或者钢丝绳和包围发动机 - 螺旋桨单元的框架 部分地。
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公开(公告)号:US20110180667A1
公开(公告)日:2011-07-28
申请号:US12401523
申请日:2009-03-10
Applicant: Patrick O'BRIEN , Emray R. GOOSSEN , Steven D. MARTINEZ
Inventor: Patrick O'BRIEN , Emray R. GOOSSEN , Steven D. MARTINEZ
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/148
Abstract: A tether continuous energy supply system for an unmanned aerial vehicle comprising: a ground station, a ground station energy system, a spool coupled to the ground station energy system at a rotating joint, a tether that is wound about the spool, wherein a first end of the tether is coupled to the rotating joint, a tension control motor coupled to both the spool and the ground station energy system, an unmanned aerial vehicle coupled to a second end of the tether, a UAV energy system, a fluid that moves throughout the tether continuous energy supply system, a tension control system that receives and transmits signals from a plurality of sensors contained within the tether continuous energy supply system, and a distributed controls system that receives and transmits signals from the plurality of sensors contained within the tether continuous energy supply system.
Abstract translation: 一种用于无人驾驶飞行器的系绳连续能量供应系统,包括:地面站,地面站能量系统,在旋转接头处联接到地面站能量系统的线轴,围绕线轴缠绕的系绳,其中第一端 连接系统与旋转接头相耦合,张力控制马达耦合到线轴和地面站能量系统,联接到系绳第二端的无人驾驶飞行器,UAV能量系统, 系绳连续能量供应系统,张力控制系统,其接收并传输包含在系链连续能量供应系统内的多个传感器的信号;以及分布式控制系统,其接收并传输包含在系链连续能量内的多个传感器的信号 供应系统
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公开(公告)号:US20100013226A1
公开(公告)日:2010-01-21
申请号:US12349868
申请日:2009-01-07
Applicant: Eric Blumer , John Thurston , Paul Wingett , Louie Timothy Gaines , Yogendra Yogi Sheoran
Inventor: Eric Blumer , John Thurston , Paul Wingett , Louie Timothy Gaines , Yogendra Yogi Sheoran
CPC classification number: F03D1/00 , B64B1/50 , B64C31/06 , B64C2201/148 , F03D5/00 , F03D7/0204 , F05B2240/921 , Y02E10/28 , Y02E10/70 , Y02E10/723 , Y10S416/06 , Y10T74/19
Abstract: A wind turbine energy conversion device that can take advantage of the higher speed and more persistent winds at higher altitudes is hereinafter disclosed. The wind turbine energy conversion device includes an unmanned aerial vehicle (UAV) connected to one end of a tether (which may include multiple shorter tethers), the other end being connected to a terrestrial anchorage point. The UAV flies at altitudes where wind speeds can reach 40 mph or higher. The UAV comprises a flying wing with one or more trailing wind power turbines and flies airborne maneuvers designed to increase relative wind speed up to about four times the true wind speed.
Abstract translation: 以下公开了能够在更高海拔地区利用更高速度和更持久的风的风力涡轮机能量转换装置。 风力涡轮机能量转换装置包括连接到系绳一端的无人驾驶飞行器(UAV),其可以包括多个较短的系绳,另一端连接到陆地锚固点。 无人机在高度达到40英里/小时以上的高空飞行。 无人机包括具有一个或多个尾随风力涡轮机的飞翼,并且飞行空中机动设计,以将相对风速增加到真实风速的大约四倍。
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公开(公告)号:US07530527B2
公开(公告)日:2009-05-12
申请号:US10558312
申请日:2004-05-20
Applicant: Christopher Charles Kelleher
Inventor: Christopher Charles Kelleher
CPC classification number: B64C37/02 , B64C39/024 , B64C39/026 , B64C2201/021 , B64C2201/022 , B64C2201/042 , B64C2201/088 , B64C2201/101 , B64C2201/104 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/146 , B64C2201/148 , B64C2201/201 , B64D5/00
Abstract: A heavier-than-air air vehicle, particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for “perpetual” flight within the stratosphere, is carried to its operational altitude suspended on a tether from a helium balloon. The tether is attached at or towards a tip of the UAV's wing so that it is carried in effectively a 90° banked attitude. At the desired altitude the UAV's powerplant is started and it flies on its tether in an upwardly-spiralling path relative to the balloon until a level or near level attitude is attained, when the tether is released and the UAV is permitted to assume free flight.
Abstract translation: 一架重型空中飞行器,特别是用于在平流层内“永久”飞行的长寿命的太阳能无人驾驶飞行器(UAV)被运载到悬挂在氦球系绳上的作战高度。 系绳连接在无人机翼的顶端或朝向无人机翼的尖端,以便有效地承载90度的坦克姿态。 在所需的高度,UAV的动力装置启动,并且相对于气球以相对于气囊的向上螺旋方式飞行,直到达到水平或接近水平的姿态时,系绳被释放并且UAV被允许进行自由飞行。
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公开(公告)号:US07510142B2
公开(公告)日:2009-03-31
申请号:US11361122
申请日:2006-02-24
Applicant: Samuel A. Johnson
Inventor: Samuel A. Johnson
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/126 , B64C2201/148
Abstract: An aerial robot is disclosed. The aerial robot may include at least one pair of counter-rotating blades or propellers, which may be contained within a circumferential shroud or a duct. In one embodiment, the aerial robot may have the ability to hover and move indefinitely. Electric power to the robot may be provided by a tether or an on-board power supply. In tethered embodiments, a solid-state, electronic voltage transformer may be used to reduce a high voltage, low current source to lower voltage, higher current source. In one embodiment, secure data communication between a ground unit and the aerial robot is facilitated by impressing high bandwidth serial data onto the high voltage tether wires or a thin optical fiber which is co-aligned with the tether wires. In one embodiment, precise navigational and position controls, even under extreme wind loads, are facilitated by an on-board GPS unit and optical digital signal processors. In one embodiment, if the tether detaches, precision free-flight is possible with on-board batteries.
Abstract translation: 公开了一种空中机器人。 空中机器人可以包括至少一对反向旋转叶片或螺旋桨,其可以包含在周向护罩或管道内。 在一个实施例中,空中机器人可能具有无限期地悬停和移动的能力。 机器人的电力可以由系绳或车载电源提供。 在连接的实施例中,可以使用固态电子电压互感器来将高电压,低电流源降低到更低的电压,更高的电流源。 在一个实施例中,通过将高带宽串行数据压印到高压系绳线上或与系绳相配合的薄光纤来实现地面单元与空中机器人之间的安全数据通信。 在一个实施例中,甚至在极端风力负载下的精确导航和位置控制也由车载GPS单元和光学数字信号处理器促成。 在一个实施例中,如果系绳分离,则使用车载电池可以进行精确的自由飞行。
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公开(公告)号:US07264204B1
公开(公告)日:2007-09-04
申请号:US11311582
申请日:2005-12-12
Applicant: Helmut Portmann
Inventor: Helmut Portmann
IPC: B64F1/02
CPC classification number: B64C39/024 , B63B35/50 , B63B35/52 , B64C2201/148 , B64C2201/165 , B64C2201/182 , B64C2201/205
Abstract: Launch and recovery of an aerial vehicle by a forwardly moving surface vehicle relies on a winch module having a winch to selectively reel out and reel in a towline and a sensor capable of sensing tension in the towline. A lifting body assembly having a pair of lifting bodies and a snagging wire is connected to the towline. The lifting bodies lift and laterally extend the snagging wire between the lifting bodies. An aerial vehicle flying through the air engages the snagging wire by a hook. A first signal representative of tension of the towline causes the winch to reel in the towline and to bring the aerial vehicle to the surface vehicle, and a second sensor associated with the hook generates a second signal representative of tension in the hook and causes the aerial vehicle to cut its motor.
Abstract translation: 通过前方移动的地面车辆发射和恢复航空器依赖于具有绞盘的绞盘模块,以选择性地卷起并卷绕在拖链中,并且能够感测到能够感测到拖链中的张力的传感器。 具有一对提升体和阻塞线的提升体组件连接到该拖绳。 升降体提升并横向延伸提升体之间的阻塞线。 空中飞行的空中飞行器通过一个钩子与阻塞线接合。 代表牵引线张力的第一信号使绞盘卷入拖缆并将空中飞行器带到地面车辆,并且与挂钩相关联的第二传感器产生代表钩中的张力的第二信号,并使天线 车辆切断电机。
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公开(公告)号:US07149611B2
公开(公告)日:2006-12-12
申请号:US10639267
申请日:2003-08-12
Applicant: Michael S. Beck , Wendell H. Chun , Jon T. Stinchcomb
Inventor: Michael S. Beck , Wendell H. Chun , Jon T. Stinchcomb
IPC: G01M17/00
CPC classification number: B64C39/028 , B60K7/0007 , B60K17/046 , B60K17/356 , B60T1/062 , B62D61/10 , B62D61/12 , B64B1/50 , B64C27/20 , B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/108 , B64C2201/127 , B64C2201/148 , B64C2201/162 , B64C2201/208
Abstract: A virtual sensor mast for a ground vehicle and a method for operating a ground vehicle using a virtual sensor mast are disclosed. The virtual sensor mast includes an unmanned airborne vehicle capable of lifting itself from the ground vehicle upon deployment therefrom; a sensor suite mounted to the unmanned airborne vehicle; and a tether between the unmanned airborne vehicle and the ground vehicle over which the sensor suite is capable of communicating sensed data upon deployment. The method includes elevating a tethered unmanned airborne vehicle from the ground vehicle to a predetermined height; sensing environmental conditions surrounding the ground vehicle; and terminating the deployment.
Abstract translation: 公开了一种用于地面车辆的虚拟传感器桅杆和使用虚拟传感器桅杆操作地面车辆的方法。 虚拟传感器桅杆包括能够在其从其展开时从地面车辆提升自身的无人机载机; 安装在无人机载体上的传感器套件; 以及在无人驾驶的机载车辆和地面车辆之间的系绳,传感器套件能够在部署时传送感测数据。 该方法包括:将有系带的无人机载体从地面车辆升高到预定的高度; 感测地面车辆周围的环境条件; 并终止部署。
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公开(公告)号:US06908702B2
公开(公告)日:2005-06-21
申请号:US10428804
申请日:2003-05-05
Applicant: James Frederick McElroy , K. R. Sridhar
Inventor: James Frederick McElroy , K. R. Sridhar
CPC classification number: H01M8/186 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/101 , B64C2201/127 , B64C2201/148 , B64C2201/165 , B64D27/24 , B64D2041/005 , B64D2211/00 , H01M8/04007 , H01M8/2475 , H01M2250/20 , Y02E60/528 , Y02T50/44 , Y02T50/55 , Y02T50/62 , Y02T90/32 , Y02T90/36 , Y10S429/901
Abstract: A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air.
Abstract translation: 一个中性浮力的飞艇,如飞艇,包含一个提升机体,允许飞艇在空气中保持中性浮力,而位于飞艇上的燃料电池。 一种在中性浮力飞艇中产生动力的方法,包括向固体氧化物燃料电池提供燃料和氧化剂以产生动力,并将热量从燃料电池提供到位于远处的提升体,其中提升体允许飞艇 在空气中保持中性浮力。
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