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公开(公告)号：EP3145811A1
公开(公告)日：2017-03-29
申请号：EP15795669.9
申请日：2015-05-22
Applicant: Lily Robotics, Inc.
Inventor： BRADLOW, Henry W. , BALARESQUE, Antoine , ENGLIN, Robert N.
CPC classification number: G05D1/0661 , B64C19/00 , B64C27/00 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/08 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64C2201/146 , G05D1/0022 , G05D1/0094 , G05D1/0669 , G05D1/102
Abstract: An unmanned aerial vehicle (UAV) copter for consumer photography or videography can be launched by a user throwing the UAV copter into mid-air. The UAV copter can detect that the UAV copter has been thrown upward while propeller drivers of the UAV copter are inert. In response to detecting that the UAV copter has been thrown upward, the UAV copter can compute power adjustments for propeller drivers of the UAV copter to have the UAV copter reach a predetermined elevation above an operator device. The UAV copter can then supply power to the propeller drivers in accordance with the computed power adjustments.
Abstract translation: 无人驾驶飞机（UAV）用于消费者摄影或录像的直升机可以由用户将无人机直升机投入空中。 无人机直升机可以检测到无人机直升机的螺旋桨驱动器是惰性的，无人机直升机已经向上抛出。 无人机直升机响应于检测到无人机直升机已经向上飞行，可以计算无人机直升机螺旋桨驱动器的功率调整，使无人机直升机达到操作员设备上方的预定高度。 无人机直升机然后可以根据计算的功率调整向螺旋桨驱动器供电。
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152.发明公开AERIAL DEVICE CAPABLE OF CONTROLLED FLIGHT AND METHODS OF USING SUCH A DEVICE 审中-公开与受控飞行和方法使用这种设备的天线装置
公开(公告)号：EP3140192A2
公开(公告)日：2017-03-15
申请号：EP15728419.1
申请日：2015-05-07
Applicant: Imperial Innovations Limited
Inventor： KOVAC, Mirko , ALHINAI, Talib Muhammad Talib
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C25/00 , B64C39/02 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/08 , B64C2201/108 , B64C2201/12 , B64C2201/146 , B64C2201/18 , B64D2211/00 , G05D1/104
Abstract: There is provided a method of using a device capable of controlled flight in a surrounding environment, the device comprising: lifting means for providing lift to the device; object-retaining means for holding an object to be affixed to a target site; and a dispensing assembly for dispensing an adhesive, wherein the method comprises: controlling the lifting means so as to controllably fly the device in the surrounding environment; and using the device to affix an object held by the object-retaining means to a target site in the surrounding environment by dispensing an adhesive from the dispensing assembly. Thus, an aerial device, for example a robotic device, may be used to fly to a desired location and affix an object at the desired location, by dispensing, ejecting or otherwise applying an adhesive.
Abstract translation: 提供了一种使用能够在周围环境受控飞行的装置的方法，该装置包括：升降装置，用于提供电梯到所述装置; 对象的保持装置，用于保持物体被固定到目标部位; 和用于分配粘合剂，worin方法的分配组件包括：控制所述提升装置以便可控地飞行装置到周围环境中; 和使用该装置固定到对象通过从分配组件粘合剂的分配保持于保持对象的装置以在周围环境中的目标部位。 因此，与天线装置，例如一个机器人装置中，可以使用飞到期望的位置，并加盖粘合剂在期望的位置为对象，通过分配，喷射或以其他方式施加到。
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153.发明公开
公开(公告)号：EP2902320A1
公开(公告)日：2015-08-05
申请号：EP14382030.6
申请日：2014-01-30
Applicant: The Boeing Company
Inventor： Criado, Alfredo , Kawiecki, Grzegorz M. , Lemus Martin, Jose L. , Ferreyra, Eduardo G. , Pereira Mayan, Sergio
CPC classification number: B64F1/08 , B64C39/024 , B64C2201/08 , B64F1/10
Abstract: A method and apparatus for launch of unmanned air vehicles is disclosed. The method of launching an unmanned air vehicle (UAV), comprises: supporting the unmanned air vehicle on a surface vehicle, such as a dolly cart (50), for riding along the ground or across water; connecting a towline to the surface vehicle; and pulling the towline to force the unmanned air vehicle in a forward direction at a speed sufficient for take-off. The towline may be pulled by a winch system. In embodiments the UAV is positioned with a nose down angle on the surface vehicle. The nose down angle permits overspeed of the UAV and cart as it is pulled along the ground, as well as controlled take-off.
Abstract translation: 公开了用于发射无人驾驶飞行器的方法和装置。 发射无人驾驶飞行器（UAV）的方法包括：将无人驾驶飞行器支撑在诸如小车（50）的地面车辆上，以沿着地面或横贯水面行驶; 将拖缆连接到地面车辆; 并拉动拖缆，以足够的起飞速度迫使无人驾驶的飞行器向前进。 拖绳可以由绞车系统拉动。 在实施例中，无人机以表面车辆上的下倾角定位。 鼻角下降角度允许无人机和推车在沿地面拉动以及受控起飞时超速。
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公开(公告)号：EP2475575A4
公开(公告)日：2015-07-08
申请号：EP10833732
申请日：2010-09-09
Applicant: AEROVIRONMENT INC
Inventor： MIRALLES CARLOS THOMAS , PLUMB NICK , TAO TONY SHUO , OLSEN NATHAN
CPC classification number: B64C13/28 , B64C3/44 , B64C3/50 , B64C3/56 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/08 , B64C2201/102 , B64C2201/121 , B64C2201/14 , B64C2201/145 , B64C2201/146
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）的系统，其被配置为经由具有弹性安装的后缘的机翼来控制俯仰，滚动和/或偏航，所述后翼与机身偏转致动器喇叭相对。 实施例包括一个或多个方向舵元件，其可以由设置在机身壳体内的效应器构件可旋转地附接和致动，并且部分地可部分地接合一个或多个舵元件。
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公开(公告)号：EP2889221A1
公开(公告)日：2015-07-01
申请号：EP14187036.0
申请日：2014-09-30
Applicant: The Boeing Company
Inventor： Ouellette, Rich P.
CPC classification number: B64D41/00 , B64C2201/06 , B64C2201/08 , B64D27/24 , B64D2027/026 , B64F1/04 , B64F3/02 , Y10S903/902
Abstract: A short takeoff and landing fixed wing aircraft (200) includes a primary powertrain (302) to provide power to a propulsion unit (208), a secondary powertrain (304) to provide power to the propulsion unit (208), and a detachable power coupling to transfer power to the secondary powertrain (304) from a source external to the fixed wing aircraft during takeoff.
Abstract translation: 短距起飞和降落固定翼飞机（200）包括向推进单元（208）提供动力的主动力系（302），向推进单元（208）提供动力的次动力系（304），以及可拆卸动力 耦合以在起飞期间将动力从固定翼飞机外部的源传递到次动力传动系（304）。
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Patent Agency Ranking
公开(公告)号：EP2879954A2
公开(公告)日：2015-06-10
申请号：EP13845941.7
申请日：2013-07-25
Applicant: Bye UAS Inc.
Inventor： BYE, George , BICKEL, Matt
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/086 , B64C2201/104 , B64C2201/126 , B64C2201/165 , B64C2201/167 , B64C2201/185 , B64C2211/00
Abstract: The present invention provides an Unmanned Aircraft System, including an integrated unmanned aerial vehicle and all related components and subsystems that can be packaged and transported as a kit, and customized to fit desired mission profiles, and easily repaired by replacement of damaged components or subsystems. The present invention further provides unmanned aircraft system components and subsystems that facilitate low power and low noise operation, and extended flight times.
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公开(公告)号：TWI607793B
公开(公告)日：2017-12-11
申请号：TW105109182
申请日：2016-03-24
Applicant: 英華達股份有限公司 , INVENTEC APPLIANCES CORP
Inventor： 蔡培倫 , TSAI, PEI LUN
CPC classification number: G05D1/0816 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/08 , B64C2201/108 , G01W1/02 , G05D1/0669 , G05D13/00
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公开(公告)号：TW201728365A
公开(公告)日：2017-08-16
申请号：TW105109182
申请日：2016-03-24
Applicant: 英華達股份有限公司 , INVENTEC APPLIANCES CORP
Inventor： 蔡培倫 , TSAI, PEI LUN
CPC classification number: G05D1/0816 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/08 , B64C2201/108 , G01W1/02 , G05D1/0669 , G05D13/00
Abstract: 無人旋翼機包括機身、複數個旋翼及感測器，機身包括中控模組及訊號處理模組，中控模組與旋翼連接，用於控制旋翼；感測器配置於無人旋翼機的機身上，用於偵測無人旋翼機的旋轉變化值；訊號處理模組連接感測器及中控模組，用於接收並分析感測器的訊號，再由中控模組控制後續飛行動作。
Abstract in simplified Chinese: 无人旋翼机包括机身、复数个旋翼及传感器，机身包括中控模块及信号处理模块，中控模块与旋翼连接，用于控制旋翼；传感器配置于无人旋翼机的机身上，用于侦测无人旋翼机的旋转变化值；信号处理模块连接传感器及中控模块，用于接收并分析传感器的信号，再由中控模块控制后续飞行动作。
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公开(公告)号：TW201643579A
公开(公告)日：2016-12-16
申请号：TW104119320
申请日：2015-06-15
Applicant: 鴻海精密工業股份有限公司 , HON HAI PRECISION INDUSTRY CO., LTD.
Inventor： 李後賢 , LEE, HOU-HSIEN , 李章榮 , LEE, CHANG-JUNG , 羅治平 , LO, CHIH-PING
CPC classification number: G05D1/042 , B64C39/024 , B64C2201/027 , B64C2201/08 , B64C2201/108 , B64C2201/141 , G05D1/0669 , G05D1/0816 , G05D1/0858
Abstract: 一種無人飛行載具自動啟動系統及方法，該無人飛行載具包括加速度感測器、電子陀螺儀、致動單元及螺旋槳馬達。當無人飛行載具被使用者向上拋出時，該系統藉由無人飛行載具內建之電子陀螺儀對無人飛行載具機身之傾斜狀況進行偵測以取得無人飛行載具機身相對於空間三軸之水平狀態資料，依據所偵測之水平狀態資料計算各位置螺旋槳馬達所需調整之轉速平衡資料，並即時驅動致動單元根據所述轉速平衡資料即時調整無人飛行載具各位置螺旋槳馬達之轉速狀況，以保持無人飛行載具處於水平懸浮平衡狀態。
Abstract in simplified Chinese: 一种无人飞行载具自动启动系统及方法，该无人飞行载具包括加速度传感器、电子陀螺仪、致动单元及螺旋桨马达。当无人飞行载具被用户向上抛出时，该系统借由无人飞行载具内置之电子陀螺仪对无人飞行载具机身之倾斜状况进行侦测以取得无人飞行载具机身相对于空间三轴之水平状态数据，依据所侦测之水平状态数据计算各位置螺旋桨马达所需调整之转速平衡数据，并实时驱动致动单元根据所述转速平衡数据实时调整无人飞行载具各位置螺旋桨马达之转速状况，以保持无人飞行载具处于水平悬浮平衡状态。
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公开(公告)号：US20190220038A1
公开(公告)日：2019-07-18
申请号：US16243019
申请日：2019-01-08
Applicant: GEOSAT Aerospace & Technology
Inventor： Lung-Shun SHIH , Fu-Kai YANG , Yi-Feng CHENG , Chao-Wen FU , Meng-Yan SHEN
CPC classification number: G05D1/0661 , B64C9/00 , B64C39/024 , B64C2009/005 , B64C2201/08 , B64C2201/12 , G05D1/085
Abstract: The present application provides methods and systems for launching an unmanned aerial vehicle (UAV). An exemplary system for launching a UAV includes a detector configured to detect acceleration of the UAV in a launch mode. The exemplary system may also include a memory storing instructions and a processor configured to execute the instructions to cause the system to: obtain a signal configured to notify the UAV to enter the launch mode, determine whether the acceleration of the UAV satisfies a condition corresponding to threshold acceleration in the launch mode, and responsive to the determination that the acceleration of the UAV satisfies the condition, turn on a motor of the UAV.
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