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公开(公告)号：WO2015057832A1
公开(公告)日：2015-04-23
申请号：PCT/US2014/060681
申请日：2014-10-15
Applicant: ELWHA LLC , HYDE, Roderick A. , WOOD, Lowell L., Jr.
Inventor： HYDE, Roderick A. , WOOD, Lowell L., Jr. , DUNCAN, William David , KARE, Jordin T. , MALASKA, Stephen L. , MYHRVOLD, Nathan P. , PETROSKI, Robert C. , WEAVER, Thomas Allan
CPC classification number: B64C39/024 , B64C39/022 , B64C2201/021 , B64C2201/042 , B64C2201/046 , B64C2201/063 , B64C2201/066 , B64C2201/12 , B64C2201/127 , B64C2201/145 , B64C2201/146 , B64C2201/208 , B64F1/00 , G05D1/0094
Abstract: A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.
Abstract translation: 机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。 车辆和飞行器构造成使得当飞行器被支撑在飞行器着陆部分上时，车辆能够向飞机提供燃料和电能中的至少一种。
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公开(公告)号：WO2006037237B1
公开(公告)日：2006-06-15
申请号：PCT/CA2005001557
申请日：2005-10-11
Applicant: FUGRO AIRBORNE SURVEYS CORP , MILES PHILIP JOHN , PARTNER RICHARD THOMAS , KEELER KENNETH RONALD , MCCONNELL TERENCE JAMES
Inventor： MILES PHILIP JOHN , PARTNER RICHARD THOMAS , KEELER KENNETH RONALD , MCCONNELL TERENCE JAMES
CPC classification number: B64C39/024 , B64C2201/084 , B64C2201/127 , B64C2201/141 , B64C2201/182 , B64C2201/208 , G01V3/165
Abstract: An un-manned airborne vehicle (UAV), for acquiring aeromagnetic data for geophysical surveying at low altitude on land or over water, comprising an extended fuselage that is adapted to hold and maintain magnetometer and a magnetic compensation magnetometer at a minimum distance from the avionics and propulsion systems of the UAV. The magnetometer measures magnetic anomalies and the magnetic compensation magnetometer measures magnetic responses corresponding to the pitch, yaw and roll of the UAV. A data acquisition system stores and removes the magnetic response measurements from the magnetic anomaly measurements. The data acquisition system also stores a survey flight plan and transmits the same to the avionics system. The generator of the UAV is shielded and the propulsion system is stabilized to reduce magnetic and vibrational noises that can interfere with the operation of the magnetometer.
Abstract translation: 一种无人载客空中飞行器（UAV），用于获取陆上或水上低空地球物理测量的航空数据，包括一个延伸的机身，适用于将磁力计和磁性补偿磁力计保持在离飞行距离最小的距离 和无人机的推进系统。 磁力计测量磁异常，磁补偿磁力计测量对应于无人机的俯仰，偏航和滚动的磁响应。 数据采集系统从磁异常测量中存储和去除磁响应测量。 数据采集系统还存储一个调查飞行计划，并将其传送到航空电子系统。 无人机的发电机被屏蔽并且推进系统被稳定以减少可能干扰磁力计操作的磁和振动噪声。
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113.发明授权
公开(公告)号：EP3045393B1
公开(公告)日：2018-12-12
申请号：EP13875320.7
申请日：2013-12-13
Applicant: Korea Aerospace Research Institute
Inventor： LEE, Sang Cherl , REW, Dong Young , SIM, Eun Sup , CHOI, Gi Hyuk , CHO, Dong Hyun , KIM, Hae Dong , KIM, Jeong Hoon , KIM, In Kyu , MOON, Sang Man , HAN, Sang Hyuck , MOON, Sung Tae , SUK, Jin Young , KIM, Jin-Won , NO, Tae Soo , GONG, Hyeon Cheol , KIM, Min Ki , KIM, Jong Chul
CPC classification number: B64F1/222 , B64C39/024 , B64C2201/042 , B64C2201/141 , B64C2201/145 , B64C2201/208 , B64F1/007 , B64F1/362 , E04H6/44 , G05D1/042 , G08G5/0013 , G08G5/0069 , G08G5/025
Abstract: An apparatus and method of charging and housing of an unmanned vertical take-off and landing (VTOL) aircraft is disclosed. The apparatus includes an accommodator to accommodate an aircraft, a landing platform on which the aircraft lands, a housing portion to monitor state data by housing or charging the aircraft, and a sensor to assist in landing of the aircraft by allowing the aircraft to communicate with the apparatus. The apparatus enhances operational efficiency by reducing a travel time of the aircraft.
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公开(公告)号：EP3372492A1
公开(公告)日：2018-09-12
申请号：EP16881084.4
申请日：2016-12-22
Applicant: Goertek Technology Co., Ltd.
Inventor： HU, Tengfei
CPC classification number: B64F1/04 , B64C39/024 , B64C2201/021 , B64C2201/066 , B64C2201/088 , B64C2201/18 , B64C2201/208 , B64F1/02 , B64F1/362 , H01F7/202 , H02J7/025 , H02N15/00
Abstract: Disclosed is an unmanned aerial vehicle take-off and landing control system and a control method. The control system comprises a magnet assembly provided at the side of an unmanned aerial vehicle (1) and a magnetic field assembly provided at the side of a parking platform. An electrified coil (2) is provided in the magnetic field assembly. A current is supplied into the electrified coil (2). A supporting magnetic field is generated by the magnetic field assembly at the side of the parking platform, so that a thrust force acting on the unmanned aerial vehicle (1) is formed. A resultant force is formed by the thrust force and a lift force or resistance force in the process of take-off or landing of the unmanned aerial vehicle (1) to supplement the lift force or the resistance. In the process of take-off or landing of the unmanned aerial vehicle (1), the current in the electrified coil (2) is changed to form a uniform magnetic field, the thrust force acting on the unmanned aerial vehicle (1) is generated to supplement the lift force or the resistance in the process of take-off and landing , thereby improving the safety performance of the unmanned aerial vehicle (1), reducing the energy consumption of the unmanned aerial vehicle (1) when it is used, and prolonging the service life of the unmanned aerial vehicle (1).
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公开(公告)号：EP3288830A2
公开(公告)日：2018-03-07
申请号：EP16728069.2
申请日：2016-04-29
Applicant: Yearwood, Clebert O'Bryan Ricardo
Inventor： Yearwood, Clebert O'Bryan Ricardo
CPC classification number: H04N7/181 , B25J11/002 , B60P3/025 , B60P3/32 , B64C39/024 , B64C2201/042 , B64C2201/08 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/182 , B64C2201/201 , B64C2201/208 , E04H1/1238 , E04H2001/1283 , F41H7/005 , F41H11/00 , G06K9/00288 , G06K9/00771 , G06K9/325 , G08B13/19632 , H04N7/18
Abstract: There is disclosed a deployable surveillance, security and/or enforcement unit, comprising: a container configured for deployment from a vehicle or by air at a surveillance, security and/or enforcement location; and two or more removable modules having equipment for performing surveillance, security and/or enforcement operations, wherein the container has a housing with at least one opening for receiving the two or more modules into the container. The unit may be comprised as part of a vehicle. The advantage of this arrangement is that it is flexible and can be deployed to meet temporary requirements, changing requirements, and can be easily equipped to meet differing roles. The deployable surveillance, security and/or enforcement unit may comprise removable modules including: a command module; a reconnaissance module; a sampling and diagnostic laboratory module; a decontamination module; and/or a utilities module.
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Patent Agency Ranking
公开(公告)号：EP3274256A2
公开(公告)日：2018-01-31
申请号：EP16812080.6
申请日：2016-03-25
Applicant: Planck Aerosystems, Inc.
Inventor： TWINING, David Merrick , WELLS, Joshua
CPC classification number: G05D1/0684 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/141 , B64C2201/18 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64D45/00 , B64D45/04 , B64F1/12 , G01C21/20 , G05D1/0669
Abstract: Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain its position hovering over the landing area. The aircraft estimates a future attitude of the surface of the landing area and determines a landing time that corresponds to a desired attitude of the surface of the landing area. The unmanned aircraft executes a landing maneuver to bring the aircraft into contact with the surface of the landing area at the determined landing time.
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117.发明公开
公开(公告)号：EP3216335A1
公开(公告)日：2017-09-13
申请号：EP17401021.5
申请日：2017-03-02
Applicant: Amazonen-Werke H. Dreyer GmbH & Co. KG
Inventor： Wild, Karl
CPC classification number: A01C21/007 , A01B79/005 , A01C17/008 , B64C39/024 , B64C2201/125 , B64C2201/208 , G01P5/00
Abstract: System und Verfahren zur Erfassung des Windes (10) bei Verteilvorgängen in der Landwirtschaft durch eine Erfassungsvorrichtung wenigstens eines im Wesentlichen vorzugsweise senkrecht start- und landefähiges, vorzugsweise autonom agierenden, unbemannten Luftfahrzeugs (12), welches wenigstens eine Einheit zur Erfassung von Umgebungsparametern aufweist, welches eine Einheit zum Empfangen von Steuersignalen von einer Basisstation und/oder Senden von Steuersignalen an ein landwirtschaftliches Arbeitsgerät (5) und eine Einheit zur Übermittlung der erfassten Umgebungsparameter an eine Basisstation und/oder an ein landwirtschaftliches Arbeitsgerät (5) aufweist. Um eine Echtzeit-Anpassung der Betriebsparameter einer landwirtschaftlichen Verteilmaschine an die vorherrschenden Windverhältnisse (10) zu ermöglichen, werden die Windverhältnisse über einer zu bearbeitenden Fläche (1) mithilfe der Erfassung von Windindikatoren (15) und/oder geeigneten Sensoren zur Erfassung von Windgeschwindigkeit(en) und/oder -richtung(en) erfasst.
Abstract translation: 由感测装置的至少一个优选地基本上垂直起飞和着陆能力的系统和方法，用于检测在Verteilvorgängen在农业风（10）的，优选地自主操作，无人飞行载具（12）具有至少一个单元，用于检测环境参数，这 用于从基站接收控制信号和/或向农具（5）发送控制信号的单元以及用于将检测到的环境参数传送到基站和/或农具（5）的单元。 为了使农业分配器与盛行风条件（10）的操作参数的实时调整，风条件是一个表面的上方被加工（1），使用的风指标的检测（15）和/或合适的传感器用于检测风速（S ）和/或方向。
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118.发明公开APPARATUS FOR CHARGING AND HOUSING UNMANNED VERTICAL TAKEOFF AND LANDING AIRCRAFT AND METHOD FOR SAME 有权设备装载和储存无人垂直和土地推出ENDER飞机及其方法
公开(公告)号：EP3045393A4
公开(公告)日：2017-04-19
申请号：EP13875320
申请日：2013-12-13
Applicant: KOREA AEROSPACE RES INST
Inventor： LEE SANG CHERL , REW DONG YOUNG , SIM EUN SUP , CHOI GI HYUK , CHO DONG HYUN , KIM HAE DONG , KIM JEONG HOON , KIM IN KYU , MOON SANG MAN , HAN SANG HYUCK , MOON SUNG TAE , SUK JIN YOUNG , KIM JIN-WON , NO TAE SOO , GONG HYEON CHEOL , KIM MIN KI , KIM JONG CHUL
CPC classification number: B64F1/222 , B64C39/024 , B64C2201/042 , B64C2201/141 , B64C2201/145 , B64C2201/208 , B64F1/007 , B64F1/362 , E04H6/44 , G05D1/042 , G08G5/0013 , G08G5/0069 , G08G5/025
Abstract: An apparatus and method of charging and housing of an unmanned vertical take-off and landing (VTOL) aircraft is disclosed. The apparatus includes an accommodator to accommodate an aircraft, a landing platform on which the aircraft lands, a housing portion to monitor state data by housing or charging the aircraft, and a sensor to assist in landing of the aircraft by allowing the aircraft to communicate with the apparatus. The apparatus enhances operational efficiency by reducing a travel time of the aircraft.
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公开(公告)号：EP3069995A1
公开(公告)日：2016-09-21
申请号：EP15003180.5
申请日：2015-11-06
Applicant: LG Electronics Inc.
Inventor： Cho, Taehoon , Shin, Choonghwan
CPC classification number: B64C39/024 , A62C3/0242 , B60P3/11 , B60Q7/00 , B60Q7/005 , B64C2201/027 , B64C2201/08 , B64C2201/108 , B64C2201/126 , B64C2201/141 , B64C2201/208 , B64F1/222 , G05D1/0088 , G05D1/101 , G08G1/04 , G08G1/09 , G08G1/0955 , G08G1/16 , G08G1/162 , G08G1/205 , G08G7/00
Abstract: 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.
Abstract translation: 根据本发明的无人驾驶飞行器系统包括安装在车辆（10）上并具有内部空间的壳体（2000），壳体设置有发射单元，容纳在壳体中的无人驾驶飞行器（1000） 当所述车辆的驾驶状态达到预设状态时从所述壳体发射，所述机翼单元（1210）安装到所述无人驾驶飞行器并且被配置为允许所述无人驾驶飞行器响应于从所述壳体的发射而飞行， 输出单元，以及控制器，被配置为基于与所述无人驾驶飞行器的驾驶状态相关的信息，控制所述机翼单元将所述无人机移动到设定的位置，并将所述输出单元控制为 输出与驾驶状态相关的警告信息。
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公开(公告)号：EP3044092A2
公开(公告)日：2016-07-20
申请号：EP14844886.3
申请日：2014-09-11
Applicant: Silicis Technologies Inc.
Inventor： STIGLER, Michael J. , SETAR, Nicholas James
IPC: B64F1/12
CPC classification number: B60P3/11 , B60P7/06 , B60P7/0876 , B64B1/10 , B64B1/50 , B64B1/58 , B64B1/66 , B64C39/022 , B64C39/024 , B64C2201/022 , B64C2201/06 , B64C2201/101 , B64C2201/12 , B64C2201/121 , B64C2201/125 , B64C2201/127 , B64C2201/148 , B64C2201/208 , B64F1/14 , B64F3/02 , G08C17/02
Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.
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