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1. 发明公开

EP3145735A4 UNMANNED AIR AND UNDERWATER VEHICLE 有权
公开(公告)号：EP3145735A4
公开(公告)日：2018-05-02
申请号：EP15795744
申请日：2015-05-21
申请人： UNIV RUTGERS
发明人： DIEZ-GARIAS FRANCISCO JAVIER , MAIA MARCO M
IPC分类号： B60F5/02
CPC分类号： B64C39/024 , A63H23/08 , A63H27/12 , B63G8/001 , B63G8/16 , B63G2008/002 , B63G2008/005 , B64C39/02 , B64C2201/027 , B64C2201/042 , B64C2201/12
摘要： An unmanned vehicle including a body and a frame structure extending from the body and supporting a plurality of propeller assemblies, each propeller assembly including at least one propeller and a corresponding motor with the motor housed in a watertight housing or coated and made corrosion resistant. The propellers comprise a first subset of propellers of the propeller assemblies and a second subset of propellers of the propeller assemblies which rotate in a plane positioned below a plane in which the first subset of propellers rotate, wherein said first and second subset of propellers are configured for independent operation of one another as the vehicle transitions from an air medium to a water medium.

2. 发明公开

EP3311898A1 TOY HELICOPTER AND BALANCING DEVICE THEREFOR 审中-公开
标题翻译：玩具直升机和平衡装置
公开(公告)号：EP3311898A1
公开(公告)日：2018-04-25
申请号：EP17157098.9
申请日：2017-02-21
申请人： Agatsuma Co., Ltd.
发明人： TODOKORO, Shinji
IPC分类号： A63H27/00
CPC分类号： A63H27/12 , A63H29/22 , A63H30/04
摘要： A toy helicopter configured to enhance a lateral stability by eliminating quickly a lateral tilt of a fuselage to restore its normal state includes a fuselage having a main body portion, a main rotor disposed above the main body portion and a balancing device fixed to an upper portion of the main body portion, the balancing device includes a long balance rod extending laterally across the fuselage, the balance rod has a protuberant portion at each end thereof and is allowed to oscillate so as to be held horizontal even though the fuselage is caused to tilt, and the balance rod is supported at a central portion thereof by a support portion.
摘要翻译：构造成通过快速消除机身的侧向倾斜以恢复其正常状态来增强横向稳定性的玩具直升机包括具有主体部分，设置在主体部分上方的主转子和固定到上部分的平衡装置的机身平衡装置包括横跨机身侧向延伸的长平衡杆，平衡杆在其每个端部处具有凸起部分，并且允许摆动以便保持水平，即使机身被致使倾斜平衡杆的中心部分由支撑部分支撑。

3. 发明公开

EP3212502A4 MULTI-ROTOR AERIAL VEHICLE 有权
公开(公告)号：EP3212502A4
公开(公告)日：2018-04-04
申请号：EP15854629
申请日：2015-10-28
申请人： ACC INNOVATION AB
发明人： LJUNG ANDERS
IPC分类号： B64D35/04 , A63H27/00 , B64C27/08 , B64C27/12 , B64C39/02 , B64D37/00
CPC分类号： B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
摘要： Multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″), wherein the control of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually controllable by means of at least one control valve 13, 23, 33 configured to control the flow of pressurized fluid from each hydraulic pump 12, 22, 32 to its dedicated hydraulic motor 11, 21, 31.

4. 发明公开

EP3247478A1 A TOY COMPRISING A ROTOR, AN ACTIVATION MECHANISM AND A LAUNCHING DEVICE 有权
标题翻译：一种玩具，包括转子，激活机构和发射装置
公开(公告)号：EP3247478A1
公开(公告)日：2017-11-29
申请号：EP16705019.4
申请日：2016-01-18
申请人： LEGO A/S
发明人： AINLEY, Timothy Mark , NIELSEN, Jesper Carol
IPC分类号： A63H27/14 , A63H33/08 , A63H27/00
CPC分类号： A63H27/00 , A63H1/04 , A63H27/12 , A63H27/14 , A63H33/08 , A63H33/086
摘要： A toy comprising a rotor, an actuator means, and a launch device, wherein the rotor comprises an actuator mechanism, and wherein a toy building element comprises a launch device in the form of a cavity configured for receiving the actuator mechanism, and wherein the actuator means can be inserted into a through-going slit opening to cooperate with the actuator mechanism to transfer momentum from the actuator means to the rotor, whereby the rotor can be rotated and launched from the launch device. The toy comprises at least two toy building elements, a first toy building element comprising the launch device and one or more of a first type of coupling means, and a second toy building element provided with one or more of a second types of coupling means that are geometrically configured to relative to the first type of coupling means, whereby the first and second types of coupling means can be releasably interconnected to form a spatial structure comprising the launch device.

5. 发明授权

EP2760739B1 CONTROL OF AN UNMANNED AERIAL VEHICLE 有权转让
标题翻译：无人驾驶飞机的控制
公开(公告)号：EP2760739B1
公开(公告)日：2017-11-22
申请号：EP12835896.7
申请日：2012-09-14
申请人： Singapore Technologies Aerospace Ltd
发明人： CHAN, Keen Ian
IPC分类号： B64C29/02 , B64C25/32 , B64C27/08 , B64C39/08 , B64C39/10 , B64C99/00 , B64C11/46 , A63H27/133 , A63H27/127 , A63H27/18 , B64C39/02
CPC分类号： B64C29/02 , A63H27/12 , B64C13/24 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/028 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/165 , G05D1/0669 , Y10T29/49826
摘要： An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method for assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises a wing structure comprising elongated equal first and second wings; a support structure comprising first and second sections coupled to a middle position of the wing structure and extending in opposite directions perpendicular to the wing structure; and four propellers, each mounted to a respective one of the first and second wings, and first and second sections, for powering the UAV during both vertical and horizontal flight modes.

6. 发明公开

EP3087003A4 AN UNMANNED AERIAL VEHICLE 有权转让
标题翻译： UNBEMANNTES LUFTFAHRZEUG
公开(公告)号：EP3087003A4
公开(公告)日：2017-09-13
申请号：EP13900333
申请日：2013-12-24
申请人： SINGAPORE TECH AEROSPACE LTD
发明人： CHAN KEEN IAN
IPC分类号： B64C29/02 , A63H27/127 , A63H27/133 , A63H27/18 , B64C11/48 , B64C39/02
CPC分类号： B64C29/02 , A63H27/12 , B64C11/48 , B64C27/08 , B64C27/10 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/122 , B64C2201/141
摘要： An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method of assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises an elongated wing structure having an elongated axis along the longest dimension of the elongated wing structure, the elongated wing structure having a middle location at a substantially halfway point; a connecting structure extending substantially perpendicularly from the elongated wing structure, the connecting structure being offset from the middle location of the elongated wing structure at a first position along the elongated axis; and at least three sets of propellers, wherein at least two sets of propellers are mounted on the connecting structure, and wherein at least one set of propellers is mounted at a second position offset from the middle location in an opposite direction away from the connecting structure.
摘要翻译：一种能够纵向和横向飞行模式的无人驾驶飞行器（UAV），一种组装无人飞行器的方法和一套用于组装无人飞行器的部件。无人飞行器包括细长机翼结构，细长机翼结构具有沿着细长机翼结构的最长尺寸的细长轴线，细长机翼结构具有在大体中途点处的中间位置; 连接结构，所述连接结构从所述细长机翼结构大致垂直地延伸，所述连接结构在所述细长机翼结构的中间位置沿着所述细长轴线在第一位置处偏移; 以及至少三组螺旋桨，其中至少两组螺旋桨安装在所述连接结构上，并且其中至少一组螺旋桨安装在第二位置，所述第二位置偏离所述中间位置在远离所述连接结构的相反方向上。

7. 发明授权

EP2541359B1 Procédé de contrôle dynamique d'attitude d'un drone, pour l'exécution automatique d'une figure de type salto 有权
标题翻译： Procédédecontrôledynamique d'attitude d'un drone，将自己的精神解放出来
公开(公告)号：EP2541359B1
公开(公告)日：2017-08-30
申请号：EP12173525.2
申请日：2012-06-26
申请人： Parrot Drones
发明人： Callou, François , Rischmuller, Michael
IPC分类号： G05D1/08 , A63H27/00
CPC分类号： G05D1/0858 , A63H27/12

8. 发明公开

EP3084544A4 DEPLOYMENT OF MOBILE AUTOMATED VEHICLES 有权
标题翻译： EINSATZ AUTOMATISIERTER MOBILER FAHRZEUGE
公开(公告)号：EP3084544A4
公开(公告)日：2017-08-23
申请号：EP14872228
申请日：2014-12-16
申请人： AMAZON TECH INC
发明人： WORLEY III WILLIAM SPENCER , CLAYTON ERIC MATHEW
IPC分类号： G05D1/02 , A63H17/26 , A63H27/00 , A63J1/00 , B60L11/18 , B64C39/02 , G05D1/10 , H04B1/3822 , H04W4/02 , H04W88/08
CPC分类号： H04W88/08 , A63H17/26 , A63H27/12 , A63J1/00 , B60L11/1816 , B60L11/182 , B60L11/1824 , B64C39/024 , B64C2201/122 , G05D1/0297 , G05D1/104 , H04B1/3822 , H04W4/021

9. 发明授权

EP2613214B1 Procédé de pilotage d'un drone à voilure tournante pour opérer une prise de vue par une caméra embarquée avec minimisation des mouvements perturbateurs 有权
标题翻译： Procédéde pilotage d'un droneàvoilure tournante pouropérerune prize de vue par unecaméraembarquéeavec minimization des mouvements perturbateurs
公开(公告)号：EP2613214B1
公开(公告)日：2017-08-02
申请号：EP13150137.1
申请日：2013-01-03
申请人： Parrot Drones
发明人： Rischmuller, Michael , Callou, François
IPC分类号： G05D1/00 , H04N5/232 , A63H30/04 , A63H27/00
CPC分类号： G05D1/0038 , A63H27/12 , A63H30/04 , G05D1/0094 , H04N5/23216 , H04N5/23245 , H04N5/23248

10. 发明授权

EP2780228B1 TRANSFORMABLE AERIAL VEHICLE 有权转让
标题翻译：可转换的空中车辆
公开(公告)号：EP2780228B1
公开(公告)日：2017-06-07
申请号：EP13826711.7
申请日：2013-12-25
申请人： SZ DJI Technology Co., Ltd.
发明人： ZHAO, Tao , DU, Hao , WANG, Mingxi , WANG, Tao
IPC分类号： B64C27/02 , B64C27/32 , B64C39/02 , B64C1/00 , B64C27/08 , A63H27/00 , B64C1/06 , B64D47/00 , B64D47/08 , G05D1/04
CPC分类号： B64C39/024 , A63H27/12 , B64C1/00 , B64C1/061 , B64C1/063 , B64C25/32 , B64C27/08 , B64C39/028 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/14 , B64C2201/146 , B64C2201/165 , B64D47/00 , B64D47/08 , G05D1/042
摘要： Discloses a transformable aerial vehicle (100) and a control method thereof. The transformable aerial vehicle (100) includes: a central body (10) and at least two transformable frame assemblies (20) respectively disposed on the central body (10), each of the least two transformable frame assemblies (20) having a proximal portion pivotally coupled to the central body (10) and a distal portion; an actuation assembly (13, 5) mounted on the central body (10) and configured to pivot the at least two transformable frame assemblies (20) to a plurality of different vertical angles relative to the central body (10); and a plurality of propulsion units (30) mounted on the at least two transformable frame assemblies (20) and operable to move the transformable aerial vehicle (100).
摘要翻译：提供了用于可变形的飞行器的系统，装置和方法。在一个方面，可变形的飞行器包括：中央主体和分别设置在中央主体上的至少两个可变形的框架组件，所述至少两个可变形的框架组件中的每一个具有枢转地联接到中央主体的近侧部分和远侧部分 ; 致动组件，所述致动组件安装在所述中央主体上并且构造成使所述至少两个框架组件相对于所述中央主体枢转至多个不同的竖直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形空中交通工具的多个推进单元。

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