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1. WO2020107407 - MOTOR MOUNT, MOTOR ASSEMBLY, ARM ASSEMBLY, AND UNMANNED AERIAL VEHICLE

Publication Number WO/2020/107407
Publication Date 04.06.2020
International Application No. PCT/CN2018/118573
International Filing Date 30.11.2018
IPC
B64D 27/26 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
B64C 27/10 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
10arranged coaxially
B64C 27/14 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
12Rotor drives
14Direct drive between power plant and rotor hub
CPC
B64C 1/16
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
16specially adapted for mounting power plant
B64C 27/10
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
10arranged coaxially
B64C 27/14
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
12Rotor drives
14Direct drive between power plant and rotor hub
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 27/26
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
H02K 5/00
HELECTRICITY
02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
KDYNAMO-ELECTRIC MACHINES
5Casings; Enclosures; Supports
Applicants
  • 深圳市大疆创新科技有限公司 SZ DJI TECHNOLOGY CO., LTD. [CN]/[CN]
Inventors
  • 王建伟 WANG, Jianwei
  • 吴晓龙 WU, Xiaolong
  • 卢绰莹 LU, Chuoying
Agents
  • 深圳市力道知识产权代理事务所(普通合伙) SHENZHEN LIDAO INTELLECTUAL PROPERTY AGENCY (GENERAL PARTNERSHIP)
Priority Data
Publication Language Chinese (ZH)
Filing Language Chinese (ZH)
Designated States
Title
(EN) MOTOR MOUNT, MOTOR ASSEMBLY, ARM ASSEMBLY, AND UNMANNED AERIAL VEHICLE
(FR) SUPPORT DE MOTEUR, ENSEMBLE MOTEUR, ENSEMBLE BRAS ET VÉHICULE AÉRIEN SANS PILOTE
(ZH) 电机安装座、电机组件、机臂组件及无人机
Abstract
(EN)
A motor mount (400), a motor assembly, an arm assembly, and an unmanned aerial vehicle (100). The motor mount is used for connecting a motor (500) and an arm (300) of the unmanned aerial vehicle, and comprises: a mounting structure (410) having a bearing part (411) and a mounting part (412) provided on the bearing part, the mounting part being detachably connected to the motor; a connection structure (420), the upper end of the connection structure being connected to the mounting structure; and a clamping structure (430), the clamping structure being a non-closed annular structure connected to the lower end of the connection structure and being used for clamping the arm.
(FR)
La présente invention concerne un support de moteur (400), un ensemble moteur, un ensemble bras et un véhicule aérien sans pilote (100). Le support de moteur est utilisé pour raccorder un moteur (500) et un bras (300) du véhicule aérien sans pilote et comprend : une structure de montage (410) présentant une partie palier (411) et une partie de montage (412) disposée sur la partie palier, la partie de montage étant raccordée de manière amovible au moteur ; une structure de raccordement (420), l'extrémité supérieure de la structure de raccordement étant raccordée à la structure de montage ; et une structure de serrage (430), la structure de serrage étant une structure annulaire non fermée raccordée à l'extrémité inférieure de la structure de raccordement et étant utilisée pour serrer le bras.
(ZH)
一种电机安装座(400)、电机组件、机臂组件及无人机(100)。该电机安装座,用于连接无人机的电机(500)和机臂(300),包括安装结构(410),具有承载部(411)以及设于承载部上的安装部(412),安装部用于与电机可拆卸连接;连接结构(420),连接结构的上端连接至安装结构;夹持结构(430),为非封闭的环状结构,与连接结构的下端连接,用于夹持机臂。
Also published as
Latest bibliographic data on file with the International Bureau