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

Applicant: Sensefly S.A.

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

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

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

Abstract: 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.

公开(公告)号：EP3241741A4

公开(公告)日：2018-01-24

申请号：EP15875204

申请日：2015-12-29

Applicant: BEIJING ZERO ZERO INFINITY TECH CO LTD

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

IPC: B64C39/02

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

Abstract: 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.

公开(公告)号：EP2763896A1

公开(公告)日：2014-08-13

申请号：EP13795150.5

申请日：2013-11-13

Applicant: SZ DJI Technology Co., Ltd.

Inventor： WANG, Tao ,  ZHAO, Tao ,  CHEN, Shaojie ,  OU, Zhigang

IPC: B64D27/08

CPC classification number: B64C27/08 ,  A63H27/12 ,  B64C1/30 ,  B64C25/06 ,  B64C25/32 ,  B64C27/00 ,  B64C27/54 ,  B64C39/024 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2201/20 ,  B64D31/14 ,  B64D43/00 ,  G01R33/0047 ,  G01V3/16 ,  G05D1/00 ,  Y10T29/49117

Abstract: Methods and apparatus for unmanned aerial vehicle (UAV) with improved reliability are provided, wherein onboard sensors are located on said UAV at a position separated from onboard electrical components. Therefore, interference experienced by onboard sensors from onboard electrical components is reduced. In addition, user-configuration or assembly of electrical components is minimized to reduce user's errors.

Abstract translation: 本发明提供了可靠性提高的无人驾驶飞行器（UAV）的方法和装置。 根据本发明的一个方面，减少了来自车载电气部件的车载传感器所经受的干扰。 根据本发明的另一方面，电子部件的用户配置或组装被最小化以减少用户错误。

公开(公告)号：EP3241758A4

公开(公告)日：2018-01-24

申请号：EP15875205

申请日：2015-12-29

Applicant: BEIJING ZERO ZERO INFINITY TECH CO LTD

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

IPC: B64C39/02

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

Abstract: 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.

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

Applicant: Parrot Drones

Inventor： SANLAVILLE, Thierry ,  DUCLOUX, Maxime ,  MORRA, Flavien ,  FARGEAU, Karim

IPC: A63H27/00 ,  B64C39/02

CPC classification number: B64C25/20 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/18 ,  B64C2201/20

Abstract: 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.

Abstract translation: 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。

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

Applicant: Ewatt Technology Co.

Inventor： ZHAO, Guocheng ,  FAN, Hui ,  CHEN, Fangfang

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C27/001 ,  B64C27/08 ,  B64C27/32 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20

Abstract: 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.

Abstract translation: 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。

公开(公告)号：EP2763896A4

公开(公告)日：2015-03-11

申请号：EP13795150

申请日：2013-11-13

Applicant: SZ DJI TECHNOLOGY CO LTD

Inventor： WANG TAO ,  ZHAO TAO ,  CHEN SHAOJIE ,  OU ZHIGANG

IPC: B64C39/02

CPC classification number: B64C27/08 ,  A63H27/12 ,  B64C1/30 ,  B64C25/06 ,  B64C25/32 ,  B64C27/00 ,  B64C27/54 ,  B64C39/024 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2201/20 ,  B64D31/14 ,  B64D43/00 ,  G01R33/0047 ,  G01V3/16 ,  G05D1/00 ,  Y10T29/49117

公开(公告)号：KR1020170111891A

公开(公告)日：2017-10-12

申请号：KR1020160038148

申请日：2016-03-30

Applicant: 삼성전자주식회사

Inventor： 백상인 ,  이영배 ,  정의현 ,  윤병욱

IPC: B64C39/02 ,  B64C27/08 ,  B64C11/46 ,  B64C27/12

CPC classification number: B64C27/50 ,  B64C11/28 ,  B64C27/08 ,  B64C27/48 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/20

Abstract: 본발명의다양한실시예에따른무인비행체는, 본체; 상기본체로부터각각연장된복수의프레임들; 및상기프레임들각각에장착되어추력또는양력을발생시키는프로펠러를포함하는추력발생장치를포함할수 있으며, 상기프로펠러는, 상기프로펠러의회전축(rotation axis)을제공하며, 상기추력발생장치의작동에따라회전하는허브; 및상기허브에각각회동가능하게장착되며, 상기허브가회전함에따라상기회전축주위를선회하면서추력또는양력을발생시키는적어도한 쌍의블레이드들을포함할수 있고상기블레이드들이서로연동되어, 상기허브상에서서로나란한위치로정렬되거나상기프로펠러회전영역의지름방향으로정렬될수 있다. 상기와같은무인비행체는실시예에따라다양할수 있다.

Abstract translation: 根据本发明的各种实施例，一种无人驾驶飞行器包括：主体; 多个框架，每个框架从主体延伸; 并且安装在每个框架上以产生推力或升力的推力发生器，螺旋桨提供螺旋桨的旋转轴线， 旋转轮毂; 并且至少一对叶片可旋转地安装在轮毂上并随着轮毂旋转产生推力或提升而绕旋转轴线旋转，并且叶片彼此互锁， 位置或螺旋桨旋转区域的径向。 如上所述的无人驾驶飞行器可根据实施例而改变。

公开(公告)号：KR1020170101958A

公开(公告)日：2017-09-06

申请号：KR1020177020953

申请日：2015-12-29

Applicant: 베이징 제로 제로 인피니티 테크놀로지 씨오., 엘티디

Inventor： 장통 ,  왕멩치우 ,  왕자오체 ,  장주양 ,  장구안쿤 ,  공슈앙 ,  장야린 ,  왕징롱 ,  리우리신

IPC: B64C39/02 ,  B64C27/00 ,  B64C27/08 ,  B64C1/30

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

Abstract: 완전보호무인기는무인기본체(1) 및그것과연결되는회전날개(2)를포함하고, 무인기본체(1)와연결되는보호하우징(3)을더 포함한다. 보호하우징(3)은메쉬형의폐쇄하우징이고중공의캐비티(31)를구비하며, 회전날개(2)가중공의캐비티(31) 내에장착된다. 회전날개가보호하우징의중공의캐비티에장착되므로, 회전날개가인체와접촉되지않아, 조작자가무인기를수동으로비행및 회수할수 있어, 회전날개의조작의편리성과안전성이향상되며; 중공의구조는회전날개에양력형성공간을제공하여, 무인기의정상적인비행을보장한다. 회전날개가무인기본체와연결되는보호하우징내에장착되므로, 무인기의전체적인높이가감소되어휴대성이향상된다.

Abstract translation: 全保护无人机包括无人飞行器本体1和连接到无人飞行器本体1的旋转叶片2，并且包括连接到无人飞行器1的保护壳体3。 保护壳体3是具有空腔31的网状闭合壳体，并安装在旋转叶片2的重量的空腔31中。 由于旋转叶片安装在保护壳体的空腔内，因此旋转叶片不与人体接触，操作人员可以手动飞行和取回无人机，从而提高旋翼的操作方便性和安全性。 中空结构在旋翼中提供升力形成空间以确保无人机的正常飞行。 由于旋翼安装在与无人机连接的保护外壳中，无人机的整体高度降低以提高便携性。

公开(公告)号：KR101589263B1

公开(公告)日：2016-01-28

申请号：KR1020150094614

申请日：2015-07-02

Applicant: 한국항공우주연구원

Inventor： 이선호

IPC: B64C39/02 ,  B64C11/28 ,  B64C27/50 ,  B64C27/08 ,  B64C27/20 ,  B64C11/00

CPC classification number: B64C1/30 ,  B64C11/00 ,  B64C11/28 ,  B64C27/08 ,  B64C27/20 ,  B64C27/50 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20

Abstract: 본발명은본체부와, 프로펠러가설치된복수의프로펠러부와, 상기프로펠러부가상기본체부상에겹쳐지게배치된상태를유지하도록상기프로펠러부를록킹시키는록킹유닛과, 상기본체부와각 프로펠러부를연결하며상기록킹유닛의록킹이해제됨에따라상기프로펠러부를상기본체부의주변위치로전개시키는전개부를포함하는프로펠러부전개식무인비행체를개시한다.

Abstract translation: 公开了一种具有螺旋桨展开功能的无人驾驶飞行器，包括：主体部分; 安装螺旋桨的多个螺旋桨部件; 锁定单元，其锁定所述螺旋桨部分以保持布置在所述主体部分上的所述螺旋桨部分的状态重叠; 以及当锁定单元的锁定被释放时，将每个螺旋桨部分连接到主体部分并且将螺旋桨部分展开到主体部分的周围的展开部分。 因此，与现有技术相比，本发明减小了体积和重量。