公开(公告)号：EP4046906A1

公开(公告)日：2022-08-24

申请号：EP20878980.0

申请日：2020-10-21

Applicant: Autel Robotics Co., Ltd.

Inventor： QIU, Longxue

IPC: B64C1/26 ,  F16B12/10

Abstract: The present invention discloses an unmanned aerial vehicle, including a body and wings. A first connection portion is disposed on one of the body and the wing. A second connection portion is disposed on the other of the body and the wing. The first connection portion and the second connection portion are detachably connected. The first connection portion is engaged with the second connection portion. The body and the wing are locked by rotating or sliding the second connection portion. The body can be conveniently assembled with or disassembled from the wing and the connection part meets the reliability of strength and rigidity and does not affect the flight performance.

公开(公告)号：EP3366972A1

公开(公告)日：2018-08-29

申请号：EP16897680.1

申请日：2016-08-01

Applicant: Autel Robotics Co., Ltd.

Inventor： QIU, Longxue ,  WANG, Jiakun ,  WANG, Zengfei

IPC: F16M11/04

CPC classification number: F16M11/041 ,  B64C39/024 ,  B64C2201/127 ,  B64D47/08 ,  F16M11/06 ,  F16M13/02 ,  F16M2200/025

Abstract: The present application provides a clamping apparatus, which includes: a carrier portion, which is formed on a regularly shaped panel, where a track slot is formed in a length direction in the carrier portion; a movable unit, mounted at an end of the carrier portion and capable of being separated from the carrier portion along a length direction of the track slot; and a clamping unit, mounted on a movable unit and configured to prevent, in at least four directions, a clamped object from being separated from the carrier portion. In the present application, the clamping unit is mounted on a movable apparatus capable of extending along the length direction of the carrier portion, resolving a problem in the prior art that a size range of clamped objects applicable to the clamping apparatus is limited. The clamping unit is configured to prevent, in the at least four directions, the clamped object from being separated from the carrier portion, effectively preventing the clamped object from being separated from the carrier portion and allowing the clamped object to be protected even in a complex environment.

公开(公告)号：EP3351845A1

公开(公告)日：2018-07-25

申请号：EP16858777.2

申请日：2016-07-26

Applicant: Autel Robotics Co., Ltd.

Inventor： LIANG, Zhiying ,  QIU, Longxue

IPC: F16M13/02 ,  B64D47/08

CPC classification number: B64D47/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/02 ,  B64C2201/127 ,  F16M11/041 ,  F16M13/02 ,  G03B15/006 ,  G03B17/561

Abstract: The present application provides a gimbal quick assembly/disassembly apparatus and an unmanned aerial vehicle having the same. The gimbal quick assembly/disassembly apparatus includes a fuselage seat component, a gimbal seat component and a locking component. The fuselage seat component is fixedly mounted on a bearing member, the gimbal seat component is fixedly mounted on a gimbal and the gimbal seat component includes a gimbal seat. The locking component is mounted on the fuselage seat component or on the gimbal seat component and the gimbal seat component and the fuselage seat component are detachably mounted together by using the locking component, so that the gimbal is detachably mounted on the bearing member. The unmanned aerial vehicle includes the gimbal quick assembly/disassembly apparatus and a photographing apparatus. The photographing apparatus is disposed on a gimbal and the bearing member is a fuselage of the unmanned aerial vehicle. The gimbal is detachably mounted on the unmanned aerial vehicle, resolving problems of complex assembled/disassembled operations and low efficiency that are caused when the gimbal is fixedly mounted on the unmanned aerial vehicle and realizing quick assembly/disassembly of the gimbal to/from the unmanned aerial vehicle.

公开(公告)号：EP3244468A1

公开(公告)日：2017-11-15

申请号：EP16863190.1

申请日：2016-10-25

Applicant: Autel Robotics Co., Ltd.

Inventor： QIU, Longxue ,  WU, Xingwen

IPC: H01M2/10

CPC classification number: H01M2/1083 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/06 ,  H01M2220/20

Abstract: The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.

Abstract translation: 本发明公开了一种无人机及其电池。 电池包括电池主体和设置在电池主体的一端上的外壳。 壳体在无人驾驶飞行器的对面设置有夹紧按钮。 夹紧按钮的一端固定在壳体上，另一端用于与无人驾驶飞行器可拆卸地连接。 夹式按钮使得电池可拆卸地与无人机的主体连接在一起，并且更换电池非常方便。