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公开(公告)号：US20140259549A1
公开(公告)日：2014-09-18
申请号：US13804984
申请日：2013-03-14
Inventor： James M. Freeman , Roger D. Schmidgall , Brian N. Harvey , Nathan Lee Tofte
IPC: F16G11/12
CPC classification number: B64C39/022 , A63H27/04 , A63H30/02 , B64C39/024 , B64C2201/145 , B64C2201/148 , F16G11/12 , Y10T24/10 , Y10T24/31 , Y10T29/49826
Abstract: A tethering system for a remote-controlled device comprising a tether line having a first end adapted to be connected to a ground support and a second end adapted to be connected to the remote-controlled device. The system further includes an anchor-point disposed between the first and second ends of the tether line, the anchor point having an eyelet for securing the tether line and allowing the tether line to slide through the eyelet during use. The anchor-point and eyelet enable the tether line to flex or bend and the remote-controlled device to maneuver one or more of over or around the target area without interfering with any nearby obstructions.
Abstract translation: 一种用于遥控装置的系绳系统，包括具有适于连接到地面支架的第一端的系绳线和适于连接到遥控装置的第二端。 系统还包括设置在系绳线的第一和第二端之间的锚定点，锚定点具有用于固定系绳的孔眼，并且允许系绳在使用期间通过孔眼滑动。 锚点和孔眼使得系绳弯曲或弯曲，并且远程控制装置在目标区域周围或周围操纵一个或多个，而不会干扰任何附近的障碍物。
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公开(公告)号：US08590829B2
公开(公告)日：2013-11-26
申请号：US13263080
申请日：2010-04-06
Applicant: Ronen Keidar , Shay Cohen
Inventor： Ronen Keidar , Shay Cohen
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/148 , Y10T74/12 , Y10T74/1293
Abstract: A method, system and a floating unit. The floating unit includes a propeller, a frame, a propeller motor that is configured to rotate the propeller about a first axis; wherein the propeller motor is coupled to the frame, a movable steering element; a controller, for controlling at least one of the propeller motor and the movable steering unit to affect at least one of a location and an orientation of the floating unit; and an interfacing module for coupling a payload to the floating unit and for receiving power from a connecting element that couples the floating unit to a ground unit; wherein the power received by the power interface is utilized to power the propeller motor and the controller.
Abstract translation: 一种方法，系统和浮动单元。 浮动单元包括螺旋桨，框架，螺旋桨马达，其构造成围绕第一轴线旋转螺旋桨; 其中所述螺旋桨电动机联接到所述框架，可移动转向元件; 控制器，用于控制所述螺旋桨马达和所述可动转向单元中的至少一个以影响所述浮动单元的位置和取向中的至少一个; 以及用于将有效载荷耦合到浮动单元并用于从连接浮动单元到地面单元的连接元件接收功率的接口模块; 其中由电力接口接收的功率用于为螺旋桨电动机和控制器供电。
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公开(公告)号：US20120091258A1
公开(公告)日：2012-04-19
申请号：US13263080
申请日：2010-04-06
Applicant: Ronen Keidar , Shay Cohen
Inventor： Ronen Keidar , Shay Cohen
IPC: B64C39/02
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , B64C2201/148 , Y10T74/12 , Y10T74/1293
Abstract: A method, system and a floating unit. The floating unit includes a propeller, a frame, a propeller motor that is configured to rotate the propeller about a first axis; wherein the propeller motor is coupled to the frame, a movable steering element; a controller, for controlling at least one of the propeller motor and the movable steering unit to affect at least one of a location and an orientation of the floating unit; and an interfacing module for coupling a payload to the floating unit and for receiving power from a connecting element that couples the floating unit to a ground unit; wherein the power received by the power interface is utilized to power the propeller motor and the controller.
Abstract translation: 一种方法，系统和浮动单元。 浮动单元包括螺旋桨，框架，螺旋桨马达，其构造成围绕第一轴线旋转螺旋桨; 其中所述螺旋桨电动机联接到所述框架，可移动转向元件; 控制器，用于控制所述螺旋桨马达和所述可动转向单元中的至少一个以影响所述浮动单元的位置和取向中的至少一个; 以及用于将有效载荷耦合到浮动单元并用于从连接浮动单元到地面单元的连接元件接收功率的接口模块; 其中由电力接口接收的功率用于为螺旋桨电动机和控制器供电。
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公开(公告)号：US20110315810A1
公开(公告)日：2011-12-29
申请号：US12803254
申请日：2010-06-23
Applicant: Dimitri Petrov
Inventor： Dimitri Petrov
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/148 , B64C2201/208
Abstract: An airborne surveillance platform supporting optoelectronic and electronic sensors, including level sensors, is automatically stabilized in a horizontal plane by varying the length of two tethers out of three. Error signals from the level sensors are transmitted over a wireless link to control components on a rotating platform on the host vehicle, which automatically vary the length of tethers. Applications include images of the surrounding terrain generated by a video camera and a thermal imager in military, police and civil emergency operations.
Abstract translation: 包括液位传感器在内的支持光电子和电子传感器的机载监控平台通过改变三个系统中的两个系绳的长度在水平面中自动稳定。 来自液位传感器的误差信号通过无线链路传输，以控制主车辆上的旋转平台上的组件，这自动改变系绳的长度。 应用包括在军事，警察和民用应急行动中由摄像机和热像仪产生的周围地形的图像。
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公开(公告)号：US20040167682A1
公开(公告)日：2004-08-26
申请号：US10639267
申请日：2003-08-12
Applicant: Lockheed Martin Corporation
Inventor： Michael S. Beck , Wendell H. Chun , Jon T. Stinchcomb
IPC: G06F017/00
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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Patent Agency Ranking
公开(公告)号：US20030089821A1
公开(公告)日：2003-05-15
申请号：US10323512
申请日：2002-12-18
Inventor： Carlos T. Miralles , Bart D. Hibbs
IPC: B64C003/56
CPC classification number: B64G1/222 , B64C1/30 , B64C3/56 , B64C39/024 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/126 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64C2201/146 , B64C2201/148 , B64C2201/185 , B64C2201/203 , B64G1/105 , B64G1/62
Abstract: Disclosed is a spacecraft carrying a number of pods, each containing an aircraft that has been folded to fit in the pod. Each aircraft has a vertical stabilizer and outboard wing-portions that fold around fore-and-aft axes. Each aircraft also has a fuselage that folds around a lateral axis. The spacecraft releases one or more of the pods into an atmosphere. Each of the pods is configured with an ablative heat shield and parachutes to protect its aircraft when the pod descends through the atmosphere. The pod releases its aircraft at a desired altitude or location, and the aircraft unfolds while free-falling. The aircraft then acquires and follows a flight path, and activates scientific experiments and instruments that it carries. The aircraft relays results and readings from the experiments and instruments to the spacecraft, which in turn relays the results and readings to a mission command center.
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公开(公告)号：US20020100838A1
公开(公告)日：2002-08-01
申请号：US10013094
申请日：2001-10-29
Inventor： Brian T. McGeer , Andreas H. von Flotow , Cory Roeseler , Clifford Jackson
IPC: B64F001/12
CPC classification number: B64C39/024 , B64C25/68 , B64C2201/104 , B64C2201/148 , B64C2201/182 , B64C2201/205 , B64F1/02
Abstract: A method and an apparatus for capturing a flying object (5) are revealed. The apparatus includes a generally linear fixture (2), such as a length of rope; a means for suspending (1) the fixture (2) across the path of the flying object (5); and one or more hooks (19) on the flying object (5). The method involves suspending the fixture (2) such that its orientation includes a component normal to the flying object's line of approach; striking the fixture (2) with the flying object (5), which causes the flying object (5) to rotate and decelerate, while the fixture (2) slides along a surface of the flying object (5) into a hook (19); capturing the fixture (2) in the hook (19); and retrieving the flying object (5) from the fixture (2).
Abstract translation: 揭示了用于捕获飞行物体（5）的方法和装置。 该装置包括大致线性的固定装置（2），例如一段绳索; 用于将（1）固定装置（2）悬挂在飞行物体（5）的路径上的装置; 和飞行物体（5）上的一个或多个钩（19）。 该方法涉及将固定装置（2）悬挂使得其取向包括垂直于飞行物体接近线的部件; （2）沿着飞行物体（5）的表面滑动到钩（19）中时，使飞行物体（5）与飞行物体（5）撞击，使飞行物体（5）旋转和减速， ; 捕获挂钩（19）中的固定装置（2）; 以及从所述固定装置（2）检索所述飞行物体（5）。
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公开(公告)号：US5035382A
公开(公告)日：1991-07-30
申请号：US339090
申请日：1989-04-17
Applicant: Peter B. S. Lissaman , W. Ray Morgan , Martyn B. Cowley , Charles J. Sink , William D. Watson
Inventor： Peter B. S. Lissaman , W. Ray Morgan , Martyn B. Cowley , Charles J. Sink , William D. Watson
CPC classification number: A63H27/00 , B64C39/024 , B64D47/08 , B64C2201/042 , B64C2201/104 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/148 , B64C2201/165 , B64C2201/187 , B64C2201/201 , B64C2201/203
Abstract: A terrain surveillance, powered aircraft is disclosed to have an on-board video camera that is not gimballed relative to the aircraft, the aircraft typically comprising multiple components; the method of the invention including: assembling the components into aircraft configuration at or near a launch site; launching the aircraft at that site with no human pilot on board same; remotely controlling the flight path of the aircraft by radio or cable link, to fly to a location for terrain surveillance; operating the on-board video camera to survey the terrain while varying yaw of the aircraft to provide sweep viewing of the terrain; and recovering the aircraft by controlling its flight to steeply descend to a landing zone.
Abstract translation: 公开了一种地形监视，动力飞机，具有相对于飞机而不是游戏的车载摄像机，该飞机通常包括多个部件; 本发明的方法包括：将组件组装成发射场所处或附近的飞行器构型; 在该地点发射飞机，没有人造飞行员在船上; 通过无线电或有线链路远程控制飞机的飞行路径，飞到一个地形进行地形监视; 操作车载摄像机以在改变飞行器的偏航的同时对地形进行调查，以提供对地形的扫描观察; 并通过控制飞机陡降到着陆区来恢复飞机。
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公开(公告)号：US4795111A
公开(公告)日：1989-01-03
申请号：US15100
申请日：1987-02-17
Applicant: Paul S. Moller
Inventor： Paul S. Moller
CPC classification number: B64C39/024 , B64C27/00 , B64C27/20 , B64C2201/027 , B64C2201/108 , B64C2201/121 , B64C2201/127 , B64C2201/146 , B64C2201/148 , B64C2201/162
Abstract: A flying platform, propelled by at least one ducted fan causing a vertically downwardly directed airstream in and through a cylindrical duct. A vane system in the duct has two mutually perpendicular pairs of diametrically opposite first vanes, each extending in from the duct rim toward the center of the duct. Each pair of first vanes provides a pair of generally vertical walls parallel to a diametral line across the duct, and they define duct passages between the pairs of vanes and define quadrants between adjacent pairs. Each first vane has an upper, fixed, rigid portion and a variable camber flap depending therefrom. A first servomotor with linkages vary the camber of each pair of flaps, so that the camber of the flaps of each pair is at all times the same amount but in opposite directions. Preferably, there are also four second vanes, one bisecting each quadrant, and a symmetric pair of spoilers is mounted on each second vane. Each pair of spoilers is independently movable, as a pair continuously between a position substantially blocking airflow through the outer portion of said quadrant and a position permitting substantially full airflow therethrough. A second servomotor with linkages symmetrically varies the position of its spoilers. There may be a radio receiver responsive to remote control signals for actuating each servomotor and its linkages.
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公开(公告)号：US20230288925A1
公开(公告)日：2023-09-14
申请号：US17653990
申请日：2022-03-08
Applicant: THE BOEING COMPANY
Inventor： Darcy Lynn Davidson, JR. , Matthew Jacob Bartow , David B. Rathbun
CPC classification number: G05D1/0022 , G05D1/0016 , B64C39/024 , B64C2201/148 , B64C2201/122 , B64C2201/128
Abstract: An authorization system includes a controller of an external computing device communicatively connected to an unmanned aerial vehicle (UAV). The controller obtains a mission kit that includes software for controlling a piece of equipment configured to be assembled on the UAV. The controller receives a license that is associated with a user and determines, based on the license, whether the piece of equipment is authorized for operation on the UAV as controlled by the user. Responsive to determining that the piece of equipment is authorized, the controller initiates transmission of at least some of the software of the mission kit to the UAV for installation by the UAV to allow the user to operate the piece of equipment.
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