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1. WO2020134235 - UNMANNED AERIAL VEHICLE AND WING ASSEMBLY THEREOF

Publication Number WO/2020/134235
Publication Date 02.07.2020
International Application No. PCT/CN2019/107550
International Filing Date 24.09.2019
IPC
B64C 1/26 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
26Attaching the wing or tail units or stabilising surfaces
B64C 1/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
CPC
B64C 1/26
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
26Attaching the wing or tail units or stabilising surfaces
B64C 2201/021
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
02characterized by type of aircraft
021Airplanes, i.e. having wings and tail planes
B64C 2201/104
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
10characterised by the lift producing means
104Fixed wings
B64C 3/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
3Wings
Applicants
  • 深圳市道通智能航空技术股份有限公司 AUTEL ROBOTICS CO., LTD. [CN]/[CN]
Inventors
  • 梁智颖 LIANG, Zhiying
Agents
  • 深圳市六加知识产权代理有限公司 LIUJIA CHINA IP LAW OFFICE
Priority Data
201811622482.928.12.2018CN
Publication Language Chinese (ZH)
Filing Language Chinese (ZH)
Designated States
Title
(EN) UNMANNED AERIAL VEHICLE AND WING ASSEMBLY THEREOF
(FR) VÉHICULE AÉRIEN SANS PILOTE ET ENSEMBLE AILE ASSOCIÉ
(ZH) 一种无人飞行器及其机翼组件
Abstract
(EN)
An unmanned aerial vehicle (500) and a wing assembly thereof (100). The wing assembly (100) is used for being mounted on a fuselage (200) of the unmanned aerial vehicle (500) and comprises wings (10); and a rotary lock cylinder (20), wherein the rotary lock cylinder (20) is provided with a rotary axis (O); one end of the rotary lock cylinder (20) is mounted on the wings (10), and the other end of the rotary lock cylinder (20) is used for being mounted on the fuselage (200); and the rotary lock cylinder (20) can rotate around the rotary axis (O) with respect to the wings (10), so that the other end of the rotary lock cylinder (20) is detached from the fuselage (200). By mounting the rotary lock cylinder (20) on the wings (10), so that the wings (10) can be conveniently detached from the fuselage (200) by rotating the rotary lock cylinder (20) to be detached from the fuselage (200).
(FR)
La présente invention concerne un véhicule aérien sans pilote (500) et un ensemble aile associé (100). L'ensemble aile (100) est utilisé pour être monté sur un fuselage (200) du véhicule aérien sans pilote (500) et comprend des ailes (10) ; et un cylindre de verrouillage rotatif (20), le cylindre de verrouillage rotatif (20) étant doté d'un axe de rotation (O) ; une extrémité du cylindre de verrouillage rotatif (20) étant montée sur les ailes (10), et l'autre extrémité du cylindre de verrouillage rotatif (20) étant utilisée pour être montée sur le fuselage (200) ; et le cylindre de verrouillage rotatif (20) peut tourner autour de l'axe de rotation respectif (O) par rapport aux ailes (10), de sorte que l'autre extrémité du cylindre de verrouillage rotatif (20) est détachée du fuselage (200). Par le montage du cylindre de verrouillage rotatif (20) sur les ailes (10), les ailes (10) peuvent être facilement détachées du fuselage (200) en faisant tourner le cylindre de verrouillage rotatif (20) devant être détaché du fuselage (200).
(ZH)
一种无人飞行器(500)及其机翼组件(100),其中所述机翼组件(100)用于安装于无人飞行器(500)的机身(200),所述机翼组件(100)包括:机翼(10);以及旋转锁芯(20),所述旋转锁芯(20)具有旋转轴线(O),所述旋转锁芯(20)的一端安装于所述机翼(10),所述旋转锁芯(20)的另一端用于安装于所述机身(200);其中,所述旋转锁芯(20)可绕所述旋转轴线(O)相对于所述机翼(10)旋转,以使得所述旋转锁芯(20)的另一端与所述机身(200)相拆卸。通过在所述机翼(10)上安装所述旋转锁芯(20),通过旋转所述旋转锁芯(20)与所述机身(200)相拆卸,以方便将机翼(10)从机身(200)上拆卸下来。
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