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1. CN108513563 - 无人机

专利局 中国
申请号 201780005482.1
申请日 30.08.2017
公布号 108513563
公布日 07.09.2018
公布类型 A
国际专利分类
B64C 39/02
B作业;运输
64飞行器;航空;宇宙航行
C飞机;直升飞机
39其他飞行器
02以特殊用途为特点的
B64C 1/30
B作业;运输
64飞行器;航空;宇宙航行
C飞机;直升飞机
1机身;机身,机翼,稳定面或类似部件共同的结构特征
30可相对移动以减小飞机外形尺寸的机身部件
B64C 1/06
B作业;运输
64飞行器;航空;宇宙航行
C飞机;直升飞机
1机身;机身,机翼,稳定面或类似部件共同的结构特征
06框架;桁条;大梁
CPC
B64C 1/063
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
06Frames; Stringers; Longerons ; ; Fuselage sections
061Frames
063Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
B64C 1/30
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
30Parts of fuselage relatively movable to reduce overall size for storage
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64C 39/024
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
024of the remote controlled vehicle type, i.e. RPV
B64C 2201/027
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
02characterized by type of aircraft
027Flying platforms
B64C 2201/108
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
10characterised by the lift producing means
108using rotors, or propellers
申请人 SZ DJI TECHNOLOGY CO LTD
深圳市大疆创新科技有限公司
发明人 XU ZHENHUA
徐振华
代理人 北京博思佳知识产权代理有限公司 11415
标题
(EN) Drone
(ZH) 无人机
摘要
(EN)
A drone (1) comprises a fuselage body (10) and a plurality of arm assemblies (201, 202) disposed on the fuselage body (10). Each of the arm assemblies (201, 202) includes a machine arm (221, 222) connected with the fuselage body (10) and a drive mechanism (211, 212) for driving the arm (221, 222) to rotate. The arm (221, 222) includes an unfolded state and a folded state, and each of the driving mechanisms (211, 212) drives the corresponding arm (221, 222) to rotate relative to the body (10) to cause the arm (221, 222) ) Switch between the expanded state and the collapsed state. The drone (1)drives the arm (221, 222) to automatically open or close by the driving mechanism (211, 212), which simplifies the user's operation steps and is more convenient to use.

(ZH)
一种无人机(1)包括机身主体(10)和设置于机身主体(10)的多个机臂组件(201、202),每个机臂组件(201、202)均包括连接于机身主体(10)的机臂(221、222)和用于驱动机臂(221、222)转动的驱动机构(211、212)。机臂(221、222)包括展开状态和折叠状态,每个驱动机构(211、212)驱动对应的机臂(221、222)相对于机身主体(10)转动,使机臂(221、222)在展开状态和折叠状态之间切换。该无人机(1)通过驱动机构(211、212)驱动机臂(221、222)自动打开或收起,简化了用户的操作步骤,更加便于使用。

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