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31. 发明公开

EP3385162A1 BASISFAHRZEUG FÜR EIN AUFKLÄRUNGSFAHRZEUG SOWIE VERFAHREN DAFÜR UND SYSTEM DAMIT 审中-公开
公开(公告)号：EP3385162A1
公开(公告)日：2018-10-10
申请号：EP17165512.9
申请日：2017-04-07
申请人： Pfoertzsch, Antony
发明人： Pfoertzsch, Antony
IPC分类号： B64C39/02 , B64F1/00 , G05D1/02 , G21C17/013 , G08G5/00 , H02J7/02
CPC分类号： G05D1/021 , B64C39/024 , B64C39/028 , B64C2201/027 , B64C2201/066 , B64C2201/126 , B64C2201/127 , B64C2201/20 , B64C2201/208 , B64F1/00 , G05D2201/0207 , G08G5/0069 , H02J7/0027 , H02J7/025 , H02J7/355 , H02J50/00
摘要： Die Erfindung betrifft ein Basisfahrzeug (10) für ein Aufklärungsfahrzeug (22), das einen Antrieb (18) zur Fortbewegung des Basisfahrzeugs (10) sowie eine Steuerung zur unbemannten Fortbewegung des Basisfahrzeugs (10) umfasst. Außerdem umfasst das Basisfahrzeug (10) eine Energietransfereinheit (12) zum Transferieren von Energie an mindestens ein unbemanntes Aufklärungsfahrzeug (22) und eine Kommunikationseinheit mit einer Drahtlosschnittstelle zumindest zum Austausch von Positionsdaten des Basisfahrzeugs (10) mit dem mindestens einen Aufklärungsfahrzeug (22).
Ferner betrifft die Erfindung ein Verfahren zum Betreiben eines Basisfahrzeugs (10) sowie ein System mit mindestens einem Basisfahrzeug (10) und mindestens einem Aufklärungsfahrzeug (22).

32. 发明授权

EP3182390B1 AUTONOMOUS SAFETY AND SECURITY DEVICE ON AN UNMANNED PLATFORM UNDER COMMAND AND CONTROL OF A CELLULAR PHONE 有权
公开(公告)号：EP3182390B1
公开(公告)日：2018-09-26
申请号：EP16202230.5
申请日：2016-12-05
申请人： Micro APPS Group Inventions LLC
发明人： SCHNEIDER, Marc , BRYAN, Lee , SCOTT, Patricia L. , KOGAN, Vladimir F. , SCULLY, Wendy C. , SCULLY, Jack T.
IPC分类号： G08B15/00
CPC分类号： G08B25/016 , B64C39/024 , B64C2201/027 , B64C2201/12 , B64C2201/126 , B64C2201/146 , F41H9/10 , F41H11/00 , G08B13/1965 , G08B15/00 , G08B21/0247 , H04W4/90
摘要： A safety and security device is housed on either an unmanned aerial vehicle or its land-based docking station and is combined with a cellular telephone for self-defense purposes. The phone broadcasts both recorded audio and video warnings on the device. A flashing light may be activated on the aerial platform or the docking station. The device may be integrated into a modular unit that combines numerous defensive mechanisms. These defensive mechanisms operate autonomously and respond to perceived threats.

33. 发明授权

EP3069995B1 UNMANNED AERIAL VEHICLE AND METHOD OF CONTROLLING THE SAME 失效
标题翻译：无人驾驶航空器及其控制方法
公开(公告)号：EP3069995B1
公开(公告)日：2018-03-28
申请号：EP15003180.5
申请日：2015-11-06
申请人： LG Electronics Inc.
发明人： Cho, Taehoon , Shin, Choonghwan
IPC分类号： B60Q7/00 , B64C39/02 , B64F1/22 , G08G1/04 , G08G1/0955 , G08G1/16 , G08G7/00
CPC分类号： B64C39/024 , A62C3/0242 , B60P3/11 , B60Q1/525 , B60Q7/00 , B60Q7/005 , B64C2201/027 , B64C2201/042 , B64C2201/08 , B64C2201/108 , B64C2201/126 , B64C2201/141 , B64C2201/185 , B64C2201/208 , B64F1/222 , G05D1/0088 , G05D1/101 , G08G1/04 , G08G1/09 , G08G1/0955 , G08G1/16 , G08G1/162 , G08G1/205 , G08G7/00
摘要： An unmanned aerial vehicle system according to the present invention includes a housing (2000) mounted on a vehicle (10) and having an inner space, the housing provided with a launching unit, an unmanned aerial vehicle (1000) accommodated in the housing and configured to be launched from the housing when a driving state of the vehicle meets a preset condition, wing units (1210) mounted to the unmanned aerial vehicle and configured to allow the flight of the unmanned aerial vehicle in response to the launch from the housing, an output unit disposed on the unmanned aerial vehicle, and a controller configured to control the wing units to move the unmanned aerial vehicle to a position set based on information related to the driving state when the unmanned aerial vehicle is launched, and control the output unit to output warning information related to the driving state.

34. 发明公开

EP2727835A3 Aircraft deployment and retrieval of unmanned aerial vehicles 有权转让
标题翻译：飞机部署和撤回无人机
公开(公告)号：EP2727835A3
公开(公告)日：2018-02-28
申请号：EP13189903.1
申请日：2013-10-23
申请人： The Boeing Company
发明人： Hanna, Mark , Poling, David R
IPC分类号： B64C39/02 , B64D1/10 , B64D1/12
CPC分类号： B64C39/024 , B64C2201/082 , B64C2201/126 , B64C2201/182 , B64C2201/206
摘要： An aircraft system incorporates a first aircraft 48a, 48b having a grappling device 26 including a first gripper 30 with a first actuator 36a and a second gripper 32 with a second actuator 36b. The first gripper and the second gripper are movable between an open and a closed position to engage a hooking device 18 and pivot together to change a capture angle. A first controller 72 receives a command and operates the actuators in response to open and close the first and second grippers of the grappling device. The controller also receives a second command and operates the first and second actuators to pivot the grippers and provide grappling at a range of capture angles. A second aircraft 10, which may be a UAV, incorporates the hooking device 18. The hooking device includes a ring 20 rotatable from the surface and a third actuator 22 to rotate the ring between a stowed and an extended position.
摘要翻译：飞行器系统包括具有擒抱装置26的第一飞机48a，48b，擒纵装置26包括具有第一致动器36a的第一抓具30和具有第二致动器36b的第二抓具32。第一夹持器和第二夹持器可在打开位置和闭合位置之间移动，以接合挂钩装置18并且一起枢转以改变捕捉角度。第一控制器72接收命令并响应于打开和关闭擒抱装置的第一和第二抓具而操作致动器。控制器还接收第二命令并且操作第一致动器和第二致动器以枢转抓具并且提供捕捉角范围的抓斗。第二架飞机10可以是无人飞行器，其包括挂钩装置18.挂钩装置包括可从表面旋转的环20和第三致动器22，以在收起位置和展开位置之间旋转环。

35. 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.

36. 发明公开

EP3182390A1 AUTONOMOUS SAFETY AND SECURITY DEVICE ON AN UNMANNED PLATFORM UNDER COMMAND AND CONTROL OF A CELLULAR PHONE 有权
标题翻译：的说明和控制移动电话的无人操纵的平台独立的安全装置
公开(公告)号：EP3182390A1
公开(公告)日：2017-06-21
申请号：EP16202230.5
申请日：2016-12-05
申请人： Micro APPS Group Inventions LLC
发明人： SCHNEIDER, Marc , BRYAN, Lee , SCOTT, Patricia L. , KOGAN, Vladimir F. , SCULLY, Wendy C. , SCULLY, Jack T.
IPC分类号： G08B15/00
CPC分类号： G08B25/016 , B64C39/024 , B64C2201/027 , B64C2201/126 , F41H9/10 , F41H11/00 , G08B13/1965 , G08B15/00 , G08B21/0247 , H04W4/90
摘要： A safety and security device is housed on either an unmanned aerial vehicle or its land-based docking station and is combined with a cellular telephone for self-defense purposes. The phone broadcasts both recorded audio and video warnings on the device. A flashing light may be activated on the aerial platform or the docking station. The device may be integrated into a modular unit that combines numerous defensive mechanisms. These defensive mechanisms operate autonomously and respond to perceived threats.
摘要翻译：的安全和保安设备采用的无人机或陆基对接站的任，并与自卫目的的移动电话相结合。手机广播这两种设备上录制的音频和视频警告。闪烁的光可以在空中平台或对接站上被激活。该设备可以被集成到一个模块单元确实结合了许多防御机制。这些防御机制自动操作和感知的威胁。

37. 发明公开

EP3112261A1 WIDE AREA SENSING SYSTEM, IN-FLIGHT DETECTION METHOD, AND NON-TRANSITORY COMPUTER READABLE MEDIUM STORING PROGRAM OF WIDE AREA SENSING SYSTEM 审中-公开
标题翻译：大面积的传感器系统，检测方法在飞行中和非暂时性计算机可读介质，具有存储于其上的程序的大面积传感器系统
公开(公告)号：EP3112261A1
公开(公告)日：2017-01-04
申请号：EP15186253.9
申请日：2015-09-22
申请人： Kabushiki Kaisha TOPCON
发明人： TANAHASHI, Atsushi
IPC分类号： B64C13/20 , B64C29/00 , B64C39/02
CPC分类号： G05D1/102 , B64C13/20 , B64C19/00 , B64C27/00 , B64C27/26 , B64C27/30 , B64C29/0033 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/123 , B64C2201/126 , B64C2201/127 , B64C2201/146 , G05D1/0011 , G05D1/0088
摘要： A wide area sensor system includes an unmanned airplane (12) being switchable between an airplane mode for high speed flight and a VTOL mode for low speed flight, a state detection sensor (34) provided in the unmanned airplane (12), the state detection sensor (34) being driven to detect a state of a detection target (42), and an external control apparatus (11) that controls flight of the unmanned airplane and driving of the state detection sensor. The external control (11) apparatus performs high speed sensing by driving the state detection sensor while performing the high speed flight of the unmanned airplane in the airplane mode. The control apparatus performs low speed sensing by driving the state detection sensor while performing the low speed flight of the unmanned airplane in the VTOL mode.
摘要翻译：广域传感器系统包括在无人驾驶飞机（12）是飞机模式为高速飞行和垂直起降模式低速飞行，在无人飞机（12）提供了一种状态检测传感器（34），状态检测之间切换传感器（34）被驱动来检测检测对象（42），以及外部控制装置（11）所做的状态检测传感器的无人驾驶飞机和驱动的飞行控制的状态。外部控制（11）装置，通过驱动状态检测传感器，同时执行在飞机模式无人驾驶飞机的高速飞行执行高速的感测。的控制装置通过驱动状态检测传感器，同时执行在VTOL模式无人驾驶飞机的低速飞行执行低速感测。

38. 发明公开

EP2281747A3 Aircraft 有权转让
标题翻译：飞机
公开(公告)号：EP2281747A3
公开(公告)日：2013-04-17
申请号：EP10251365.2
申请日：2010-07-30
申请人： QinetiQ Limited
发明人： Kelleher, Christopher Charles
IPC分类号： B64C23/06 , B64C39/02
CPC分类号： B64C39/024 , B64C23/069 , B64C23/076 , B64C2201/021 , B64C2201/126 , Y02T50/164
摘要： An aircraft, particularly a solar powered, high altitude, long endurance, unmanned aerial vehicle, is equipped with a combination of canted down, raked back wing tips 7 and trailing "tip tails" 10 carried on booms 9 from the tip regions of the mainplane 4. Each tip tail is positioned to be subject to the upwash field of the respective wing tip vortex, at least in the cruise condition of the aircraft. The wing tip form can achieve a reduction in induced drag and help to relieve wing root bending moment while the tip tails can act through their connections to the mainplane to provide torsional relief to the latter, particularly under lower incidence/higher speed conditions. In the higher incidence/lower speed cruise condition, however, the presence of the tip tails in the upwash fields of the wing tip vortices means that they can generate lift with a component in the forward direction of flight and hence contribute to the thrust requirements of the aircraft.

39. 发明公开

EP2576342A1 RECONFIGURABLE BATTERY-OPERATED VEHICLE SYSTEM 审中-公开
标题翻译：可重新配置的电池供电的车辆系统
公开(公告)号：EP2576342A1
公开(公告)日：2013-04-10
申请号：EP11787032.9
申请日：2011-05-26
申请人： AeroVironment, Inc.
发明人： FISHER, Christopher, E. , TOKUMARU, Phillip, T. , SCHMALZEL, Marc, L. , ZWAAN, John, Peter , TYLER, Jeremy, D. , MCALLISTER, Justin, B. , TORRES, Gabriel , BELIK, Pavel
IPC分类号： B64C27/00
CPC分类号： B64C39/028 , A63H27/04 , A63H27/12 , B63B7/04 , B63H21/17 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/126 , B64C2201/146
摘要： A quadrotor UAV including ruggedized, integral-battery, load- bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module, and skids configured as landing gear. The two arms are replaceable with arms having wheels for ground vehicle use, with arms having floats and props for water-surface use, and with arms having pitch-controlled props for underwater use. The control module is configured to operate as an unmanned aerial vehicle, an unmanned ground vehicle, an unmanned (water) surface vehicle, and an unmanned underwater vehicle, depending on the type of arms that are attached.

40. 发明公开

EP2151379A3 Modular pods for use with an unmanned aerial vehicle 有权
标题翻译：使用模块化容器无人机
公开(公告)号：EP2151379A3
公开(公告)日：2012-04-11
申请号：EP09161737.3
申请日：2009-06-02
申请人： Honeywell International Inc.
发明人： Collette, Daniel Ross , Helsing, JR., Joseph Scott
IPC分类号： B64C27/20 , B64C39/02
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162 , B64C2211/00
摘要： A pod (240) for an unmanned aerial vehicle is provided that may be removed and reattached to the vehicle. The pod comprises an outer shell, within which a variety of payloads may be carried. A first surface on the vehicle frame comprises a plurality of connects or electrical traces. The plurality of attachments are used to removably attach the pods to the first surface. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.

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