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    MULTI-ROTOR STRUCTURE APPLIED TO UNMANNED AERIAL VEHICLE
    2.
    发明公开
    MULTI-ROTOR STRUCTURE APPLIED TO UNMANNED AERIAL VEHICLE 审中-公开
    多旋翼结构应用于无人机空中车辆

    公开(公告)号：EP3181449A3

    公开(公告)日：2017-09-13

    申请号：EP16201250.4

    申请日：2016-11-29

    申请人： Ewatt Technology Co.

    发明人： ZHAO, Guocheng ,  FAN, Hui ,  CHEN, Fangfang

    IPC分类号： B64C39/02

    CPC分类号： B64C39/024 ,  B64C27/001 ,  B64C27/08 ,  B64C27/32 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20

    摘要： The present invention discloses a multi-rotor structure applied to an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle includes a fuselage, first rotors, second rotors and rotor shafts; and the multi-rotor structure includes first rotary connecting pieces and second rotary connecting pieces. The first rotary connecting piece includes a first motor (41) and a first dismounting thread group, the first rotor (21) is detachably connected with the first motor through the first dismounting thread group to achieve the mounting or dismounting between the first rotor and the first motor by rotating the first rotor; the second rotary connecting piece includes a second motor and a second dismounting thread group, and the second rotor is detachably connected with the second motor through the second dismounting thread group to achieve the mounting or dismounting between the second rotor and the second motor by rotating the second rotor. The present invention has the advantages of being fast, portable and high in working efficiency.

    摘要翻译： 本发明公开了一种应用于无人机的多转子结构，属于无人机技术领域。 无人机包括机身，第一转子，第二转子和转子轴; 多转子结构包括第一旋转连接件和第二旋转连接件。 第一旋转连接件包括第一马达和第一拆卸线组，第一转子通过第一拆卸线组可拆卸地与第一电机连接，实现第一转子与第一拆卸线组之间的安装或拆卸， 通过旋转第一转子来驱动第一电动机 所述第二旋转连接件包括第二电机和第二拆卸线组，所述第二转子通过所述第二拆卸线组与所述第二电机可拆卸连接，实现所述第二转子与所述第二电机之间的安装或拆卸， 第二转子。 本发明具有快速，便携和工作效率高的优点。

    AIRCRAFT WITH DETACHABLE WINGS
    3.
    发明公开
    AIRCRAFT WITH DETACHABLE WINGS 有权
    FLUGZEUG MIT ABNEHMBARENFLÜGELN

    公开(公告)号：EP2903892A1

    公开(公告)日：2015-08-12

    申请号：EP13763040.6

    申请日：2013-09-13

    申请人： Sensefly S.A.

    发明人： BEYELER, Antoine ,  KLAPTOCZ, Adam ,  ROBERTS, James F. ,  ZIMMERMANN, Loic ,  ZUFFEREY, Jean-Christophe ,  LAZZARATTO-PINÖSCH, Andreas

    IPC分类号： B64C1/26

    CPC分类号： B64C1/26 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/187 ,  B64C2201/20

    摘要： This invention relates to a connection set that is used to attach and transfer force and torque between a wing (2a, 2b), comprising a lifting surface and a control surface (9) connected together by a hinge, and the central body (1) of an aircraft, which contains a servo-motor (10) used for actuating said control surface (9). The wing (2a, 2b) is connected to the central body (1) using a connection set comprised of two components. First, an attachment mechanism (3, 4, 5, 6) is used to align the wings (2a, 2b) relative to the central body (1) and to transfer the aerodynamic forces acting on the wing (2a, 2b) to the central body (1), preventing the wing (2a, 2b) from bending at its connection point. Second, a torque coupling mechanism (7, 8) is used to actuate the control surfaces that are present on the wings using servomotors (10) that are embedded within the central body (1). The connection set is engaged and disengaged using a single motion and does not require additional connection of electrical cables or mechanical fixations.

    摘要翻译： 本发明涉及一种用于在包括提升表面和通过铰链连接在一起的控制表面（9）的翼（2a，2b）之间附接和传递力和扭矩的连接组，以及中心体（1） 其包含用于致动所述控制表面（9）的伺服电动机（10）。 翼（2a，2b）使用由两个部件组成的连接组件连接到中心体（1）。 首先，使用附接机构（3,4,5,6）来相对于中心体（1）对准翼（2a，2b）并将作用在机翼（2a，2b）上的空气动力传递到 中心体（1），防止机翼（2a，2b）在其连接点处弯曲。 第二，扭矩联接机构（7,8）用于使用嵌入在中心体（1）内的伺服电动机（10）致动存在于机翼上的控制表面。 连接组使用单一动作进行接合和分离，不需要额外连接电缆或机械固定。

    AIRCRAFT WITH DETACHABLE WINGS
    4.
    发明授权
    AIRCRAFT WITH DETACHABLE WINGS 有权
    飞机与可拆卸的翅膀

    公开(公告)号：EP2903892B1

    公开(公告)日：2018-05-02

    申请号：EP13763040.6

    申请日：2013-09-13

    申请人： Sensefly S.A.

    发明人： BEYELER, Antoine ,  KLAPTOCZ, Adam ,  ROBERTS, James F. ,  ZIMMERMANN, Loic ,  ZUFFEREY, Jean-Christophe ,  LAZZARATTO-PINÖSCH, Andreas

    IPC分类号： B64C1/26 ,  B64C39/02 ,  B64C39/10

    CPC分类号： B64C1/26 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/187 ,  B64C2201/20

    摘要： This invention relates to a connection set that is used to attach and transfer force and torque between a wing (2a, 2b), comprising a lifting surface and a control surface (9) connected together by a hinge, and the central body (1) of an aircraft, which contains a servo-motor (10) used for actuating said control surface (9). The wing (2a, 2b) is connected to the central body (1) using a connection set comprised of two components. First, an attachment mechanism (3, 4, 5, 6) is used to align the wings (2a, 2b) relative to the central body (1) and to transfer the aerodynamic forces acting on the wing (2a, 2b) to the central body (1), preventing the wing (2a, 2b) from bending at its connection point. Second, a torque coupling mechanism (7, 8) is used to actuate the control surfaces that are present on the wings using servomotors (10) that are embedded within the central body (1). The connection set is engaged and disengaged using a single motion and does not require additional connection of electrical cables or mechanical fixations.

    FOLDABLE UNMANNED AERIAL VEHICLE
    5.
    发明公开
    FOLDABLE UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：EP3241741A4

    公开(公告)日：2018-01-24

    申请号：EP15875204

    申请日：2015-12-29

    申请人： BEIJING ZERO ZERO INFINITY TECH CO LTD

    发明人： ZHANG TONG ,  WANG MENGQIU ,  WANG ZHAOZHE ,  ZHANG XUYANG ,  ZHANG GUANQUN ,  GONG SHUANG ,  ZHANG YALIN ,  WANG JINGLONG ,  LIU LIXIN

    IPC分类号： B64C39/02

    CPC分类号： B64C27/006 ,  B64C1/30 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/201

    摘要： A fully-protected unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and a rotor (2) connected to the unmanned aerial vehicle body (1), and further comprises a protection housing (3) connected to the unmanned aerial vehicle body (1). The protection housing (3) is a hollowed-out closed housing and has a hollow cavity (31), and the rotor (2) is installed in the hollow cavity (31). Because the rotor is installed in the hollow cavity of the protection housing, the rotor cannot make contact with a human body, so that the unmanned aerial vehicle can be released or reclaimed by an operator with the hand, and the operation portability and safety of the rotor are improved. The hollowed-out structure provides a forming space of lift for the rotor and normal flight of the unmanned aerial vehicle is ensured. The rotor is installed in the protection housing that is connected to the unmanned aerial vehicle body, so that the overall height of the unmanned aerial vehicle is reduced, and the portability of the unmanned aerial vehicle is further improved.

    FULLY-PROTECTED UNMANNED AERIAL VEHICLE
    7.
    发明公开
    FULLY-PROTECTED UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：EP3241758A4

    公开(公告)日：2018-01-24

    申请号：EP15875205

    申请日：2015-12-29

    申请人： BEIJING ZERO ZERO INFINITY TECH CO LTD

    发明人： ZHANG TONG ,  WANG MENGQIU ,  WANG ZHAOZHE ,  ZHANG XUYANG ,  ZHANG GUANQUN ,  GONG SHUANG ,  ZHANG YALIN ,  WANG JINGLONG ,  LIU LIXIN

    IPC分类号： B64C39/02

    CPC分类号： B64C27/006 ,  B64C1/30 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/201

    摘要： A fully-protected unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and a rotor (2) connected to the unmanned aerial vehicle body (1), and further comprises a protection housing (3) connected to the unmanned aerial vehicle body (1). The protection housing (3) is a hollowed-out closed housing and has a hollow cavity (31), and the rotor (2) is installed in the hollow cavity (31). Because the rotor is installed in the hollow cavity of the protection housing, the rotor cannot make contact with a human body, so that the unmanned aerial vehicle can be released or reclaimed by an operator with the hand, and the operation portability and safety of the rotor are improved. The hollowed-out structure provides a forming space of lift for the rotor and normal flight of the unmanned aerial vehicle is ensured. The rotor is installed in the protection housing that is connected to the unmanned aerial vehicle body, so that the overall height of the unmanned aerial vehicle is reduced, and the portability of the unmanned aerial vehicle is further improved.

    DRONE MUNI DE SUPPORTS DE DRONE RELEVABLES
    8.
    发明公开
    DRONE MUNI DE SUPPORTS DE DRONE RELEVABLES 审中-公开
    DRONE拥有可靠的无声支架

    公开(公告)号：EP3210658A1

    公开(公告)日：2017-08-30

    申请号：EP17154744.1

    申请日：2017-02-06

    申请人： Parrot Drones

    发明人： SANLAVILLE, Thierry ,  DUCLOUX, Maxime ,  MORRA, Flavien ,  FARGEAU, Karim

    IPC分类号： A63H27/00 ,  B64C39/02

    CPC分类号： B64C25/20 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/18 ,  B64C2201/20

    摘要： L'invention concerne un drone à voilure tournante comprenant un corps de drone, des bras de liaison (24, 26, 28, 30) s'étendant à partir du corps et portant à leur extrémité un bloc propulseur, et au moins deux supports de drone (66) s'étendant à partir du corps de drone. Les supports comprennent respectivement un moyen de relevage de sorte que les supports de drone soient aptes à être relevés lorsque le drone est en vol, en venant en alignement avec les bras de liaison. Les supports de drone peuvent notamment former le bord d'attaque des bras de liaison arrière et/ou le bord de fuite des bras de liaison avant du drone.

    摘要翻译： 本发明涉及一种旋翼无人机，其包括无人驾驶飞机本体，从本体延伸并在其端部承载推进单元的连接臂（24,26,28,30）以及至少两个支撑构件。 无人机（66）从无人机主体延伸。 支架分别包括升降装置，使得无人驾驶飞机在飞行中能够升起无人驾驶飞机支架，与连接臂对齐。 无人机支撑件尤其可以形成后连杆臂的前缘和/或无人驾驶飞机的前连杆臂的后缘。

    MULTI-ROTOR STRUCTURE APPLIED TO UNMANNED AERIAL VEHICLE
    9.
    发明公开
    MULTI-ROTOR STRUCTURE APPLIED TO UNMANNED AERIAL VEHICLE 审中-公开
    爱尔兰人民共和国罗姆富尔群岛

    公开(公告)号：EP3181449A2

    公开(公告)日：2017-06-21

    申请号：EP16201250.4

    申请日：2016-11-29

    申请人： Ewatt Technology Co.

    发明人： ZHAO, Guocheng ,  FAN, Hui ,  CHEN, Fangfang

    IPC分类号： B64C39/02

    CPC分类号： B64C39/024 ,  B64C27/001 ,  B64C27/08 ,  B64C27/32 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20

    摘要： The present invention discloses a multi-rotor structure applied to an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle includes a fuselage, first rotors, second rotors and rotor shafts; and the multi-rotor structure includes first rotary connecting pieces and second rotary connecting pieces. The first rotary connecting piece includes a first motor (41) and a first dismounting thread group, the first rotor (21) is detachably connected with the first motor through the first dismounting thread group to achieve the mounting or dismounting between the first rotor and the first motor by rotating the first rotor; the second rotary connecting piece includes a second motor and a second dismounting thread group, and the second rotor is detachably connected with the second motor through the second dismounting thread group to achieve the mounting or dismounting between the second rotor and the second motor by rotating the second rotor. The present invention has the advantages of being fast, portable and high in working efficiency.

    摘要翻译： 本发明公开了一种应用于无人机的多转子结构，属于无人驾驶飞行器技术领域。 无人机包括机身，第一转子，第二转子和转子轴; 并且多转子结构包括第一旋转连接件和第二旋转连接件。 第一旋转连接件包括第一电动机（41）和第一拆卸螺纹组，第一转子（21）通过第一拆卸螺纹组与第一电动机可拆卸地连接，以实现第一转子和第二转子之间的安装或拆卸 第一电机通过旋转第一转子; 所述第二旋转连接件包括第二电动机和第二拆卸螺纹组，所述第二转子通过所述第二拆卸螺纹组与所述第二电动机可拆卸地连接，以通过旋转所述第二转子和所述第二电动机来实现所述第二转子和所述第二电动机之间的安装或拆卸 第二转子。 本发明具有快速便携，工作效率高的优点。