WO2017101589A1 - 一种无人机电池和无人机 - Google Patents
一种无人机电池和无人机 Download PDFInfo
- Publication number
- WO2017101589A1 WO2017101589A1 PCT/CN2016/103265 CN2016103265W WO2017101589A1 WO 2017101589 A1 WO2017101589 A1 WO 2017101589A1 CN 2016103265 W CN2016103265 W CN 2016103265W WO 2017101589 A1 WO2017101589 A1 WO 2017101589A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- drone
- battery
- snap button
- snap
- aerial vehicle
- Prior art date
Links
- 238000010586 diagram Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/39—Battery swapping
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/34—In-flight charging
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Definitions
- the present application relates to the field of drones, and in particular to a drone battery and a drone.
- UAVs originally used only for military use frequently appeared in the civilian market.
- drones can be used in many fields such as power inspection, map mapping, traffic control security, advertising celebrations, etc.
- the civil aircraft market for drones is infinitely large and has broad development space.
- Civil drones are generally controlled and set by wireless remote control devices or ground stations. During the flight, the drones will transmit flight data or other information such as video to the ground station. The ground station can learn about the current drones. Flight status and other data information.
- the snap button is used for hooking with one end of the detachable connection of the drone, and the hook is used for detachably attaching to the drone; a groove is formed between the hook and the buckle button body.
- the outer surface between one end and the other end of the snap button is further provided with a non-slip structure.
- the utility model further includes a reset spring piece, and the reset spring piece is disposed on the inner side of the buckle button.
- one end of the reset elastic piece is disposed on the housing, and the other end of the reset elastic piece is in contact with the snap button.
- the snap buttons are at least two, oppositely disposed at upper and lower ends of the housing relative to one side of the drone.
- a side of the buckle contacting the buckle button is provided with a hook.
- the buckle is disposed on the outer surface of the magazine.
- the buckles are at least two, and are disposed opposite to opposite sides of the magazine.
- FIG. 3 is a schematic diagram of a state in which a battery of a drone is connected to a body of a drone according to an embodiment of the present application;
- FIG. 1 is a schematic diagram of a structure of an unmanned aerial vehicle disclosed in the embodiment.
- the unmanned aerial vehicle includes: an unmanned aerial vehicle body 1 and a drone battery 2 .
- the UAV battery includes: a battery body 21 And a housing 22 disposed at one end of the battery body 21.
- a buckle button 221 is disposed on a side of the housing 22 relative to the drone.
- One end of the snap button 221 is fixed to the housing 22, and the other end of the snap button 221 is detachably connected to the drone.
- the snap button 221 is disposed at the upper and lower ends of the housing 22, the inward movement can be pressed. After the hand is released, the snap button 221 can be automatically reset by the reset tab 222. Thereby, the detachable connection between the UAV battery and the UAV body can be realized, which facilitates the replacement of the UAV battery.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Toys (AREA)
- Battery Mounting, Suspending (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
一种无人机及其电池,其中,所述无人机电池,包括:电池本体和布置在电池本体一端的壳体,在壳体相对于无人机的一侧设置有卡扣按键,卡扣按键的一端固接在壳体上,卡扣按键的另一端用于与无人机可拆卸连接。由于在电池本体一端的壳体上设置有卡扣按键,从而能够实现无人机电池与无人机本体可拆卸连接,方便了无人机电池的更换。
Description
本申请涉及无人机领域,具体涉及一种无人机电池和无人机。
随着科学技术的进步和国民经济发展的需要,原先仅用于军用的无人机频繁出现在民用市场中。在民用市场中,无人机可用于电力巡检、地图测绘、交管安防、广告庆典等诸多领域,无人机民用市场无限巨大,具有广阔的发展空间。民用无人机一般通过无线遥控装置或地面站进行控制和设置,无人机在飞行过程中,会将飞行数据或者视频等其他信息传输到地面站中,通过地面站可以了解到当前无人机的飞行状态和其他数据信息。
现有技术中,无人机的本体上开设有凹腔,用于盛放无人机电源,例如锂电池。通常,在凹腔开口处设置有用于固定电池的密封板,以防止无人机在行驶过程中,电池从凹腔中脱落出来,一般而言,采用螺钉、螺栓或其它紧固部件对密封板和无人机本体进行固定。由此,导致当更换电池时,需要拧开螺钉螺栓,在更换电池后,再拧紧螺钉螺栓,从而造成了电池更换的不便。
发明内容
因此,本申请要解决的技术问题在于克服现有技术中的无人机电池更换不便的缺陷。
根据第一方面,本申请实施例公开了一种无人机电池,包括:
电池本体和布置在电池本体一端的壳体,在壳体相对于无人机的一侧设置有卡扣按键,卡扣按键的一端固接在壳体上,卡扣按键的另一端用于与无人机可拆卸连接。
进一步,卡扣按键用于与无人机可拆卸连接的一端具有挂钩,挂钩用于可分离挂接于无人机上;挂钩和卡扣按键本体之间形成凹槽。
进一步,卡扣按键的一端和另一端之间的外表面还设有防滑结构。
优选地,防滑结构是波纹状突起结构。
进一步,还包括复位弹片,复位弹片设置在卡扣按键的内侧,
进一步,复位弹片的一端设置在壳体上,复位弹片的另一端与卡扣按键相接触。
进一步,复位弹片呈镜像S型,镜像S型的一端卡设在壳体上,镜像S型的另一端的弧面与卡扣按键的下表面相顶接触。
优选地,卡扣按键至少为两个,相对布置在壳体相对于无人机的一侧的上下端。
根据第二方面,本申请实施例公开一种无人机,包括:
无人机本体,无人机本体上设置有无人机电池仓,无人机电池仓的仓口上与无人机电池壳体接触的端面设置有与卡扣按键可拆卸连接的卡扣。
进一步,卡扣与卡扣按键接触的一面设有卡勾。
进一步,卡扣设置在仓口的外表面。
进一步,卡扣至少为两个,相对布置在仓口相对的两侧。
进一步,还包括以上任一的无人机电池。
本申请技术方案,具有如下优点:
根据本申请实施例提供的无人机及其电池,由于在电池本体一端的壳体上设置有卡扣按键,从而能够实现无人机电池与无人机本体可拆卸连接,方便了无人机电池的更换。
作为优选的技术方案,在卡扣内侧设置有复位弹片,从而实现了卡扣按键的自动归位。
为了更清楚地说明本申请具体实施方式或现有技术中的技术方案,下面将对具体实施方式或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图是本申请的一些实施方式,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。
图1为本申请实施例中无人机拆解结构示意图;
图2为本申请实施例无人机电池结构示意图;
图3为本申请实施例中无人机电池连接至无人机本体的一种状态示意图;
图4为本申请实施例中无人机电池连接至无人机本体的另一种状态示意图。
下面将结合附图对本申请的技术方案进行清楚、完整地描述,显然,所描述的实施例是本申请一部分实施例,而不是全部的实施例。基于本申
请中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本申请保护的范围。
在本申请的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是直接相连,也可以通过中间媒介间接相连。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本申请中的具体含义。
此外,下面所描述的本申请不同实施方式中所涉及的技术特征只要彼此之间未构成冲突就可以相互结合。
实施例1
请参考图1,为本实施例公开的一种无人机结构示意,该无人机包括:无人机本体1和无人机电池2。
为实现无人机电池与无人机本体可拆卸连接,方便无人机电池的更换,本实施例公开了一种无人机电池,请参考图2,该无人机电池包括:电池本体21和布置在电池本体21一端的壳体22。在壳体22相对于无人机的一侧设置有卡扣按键221,卡扣按键221的一端固接在壳体22上,卡扣按键221的另一端用于与无人机可拆卸连接。在优选的实施例中,卡扣按键221与无人机可拆卸连接的一端具有挂钩2211,用于可分离挂接于无人机上;该挂钩和卡扣按键本体之间形成凹槽,以防止卡扣按键本体和无人机之间形成机构干涉。在具体实施例中,卡扣按键221至少为两个,相对布置在壳体22相对于无人机的一侧的上下端。在优选的实施例中,为了提高卡扣按键接触的摩擦力,防止用户在接触卡扣按键时打滑,卡扣按键的一端和另
一端之间的外表面还设有防滑结构2212。该防滑结构是波纹状突起结构。
为了实现卡扣按键221的自动归位,在优选的实施例中,该无人机电池还包括复位弹片222。复位弹片222设置在卡扣按键221的内侧,复位弹片222的一端设置在壳体22上,复位弹片222的另一端与卡扣按键221相接触。具体地,复位弹片222的另一端与卡扣按键221相抵触。
在优选的实施例中,为了使得复位弹片222更好地卡设在卡扣按键221的内侧,复位弹片222呈镜像S型。镜像S型的一端卡设在壳体22上,例如,可以通过卡扣按键221与复位弹片222该端接触的一端压紧复位弹片222的该端;镜像S型的另一端的弧面与卡扣按键221的下表面相顶接触,从而使得复位弹片222能够更好地向卡扣按键221提供归位动力。
本实施例公开的无人机电池,由于卡扣按键221设置于壳体22上下两端,可按压向内移动,松开手后,在复位弹片222作用下卡扣按键221可以自动复位。从而能够实现无人机电池与无人机本体可拆卸连接,方便了无人机电池的更换。
实施例2
请参考图1,为本实施例公开的一种无人机,包括无人机本体1,所述无人机本体1上设置有无人机电池仓11。请参考图3,无人机电池仓11的仓口上与无人机电池壳体接触的端面设置有与卡扣按键可拆卸连接的卡扣12。在具体实施例中,卡扣12可以设置在仓口的外表面。在优选的实施例中,卡扣12与卡扣按键接触的一面设有卡勾121,具体地,卡勾向仓口内侧勾,卡勾与卡扣按键221的挂钩相配合,以更好地实现卡扣按键221与无人机本体的连接。优选地,卡扣至少为两个,相对布置在仓口相对的两
侧,具体地,应与卡扣按键在连接至无人机本体时卡扣按键的位置相匹配。
在具体实施例中,当无人机电池2需要装到无人机本体1上时,只需拿起无人机电池2放无人机电池仓11的仓口上并向无人机电池仓11内推,卡扣按键221在无人机电池仓11仓口的上、下卡扣12的挤压下,自动压下复位弹片222,便可推进去,如图3所示;同时,当卡扣按键221完全推进去后,复位弹片222自动回弹把卡扣按键221复位,请参考图4,使无人机电池2被无人机电池仓11仓口的上、下卡扣12紧紧的卡住。同样,当需要取出无人机电池2时,只需要手指上下按下卡扣按键221,同时往外拔电池,即可取出。
显然,上述实施例仅仅是为清楚地说明所作的举例,而并非对实施方式的限定。对于所属领域的普通技术人员来说,在上述说明的基础上还可以做出其它不同形式的变化或变动。这里无需也无法对所有的实施方式予以穷举。而由此所引伸出的显而易见的变化或变动仍处于本申请创造的保护范围之中。
Claims (13)
- 一种无人机电池,包括电池本体和布置在所述电池本体一端的壳体,其特征在于,在所述壳体相对于无人机的一侧设置有卡扣按键,所述卡扣按键的一端固接在所述壳体上,所述卡扣按键的另一端用于与所述无人机可拆卸连接。
- 如权利要求1所述的无人机电池,其特征在于,所述卡扣按键用于与所述无人机可拆卸连接的一端具有挂钩,所述挂钩用于可分离挂接于所述无人机上;所述挂钩和卡扣按键本体之间形成凹槽。
- 如权利要求1或2所述的无人机电池,其特征在于,所述卡扣按键的一端和另一端之间的外表面还设有防滑结构。
- 如权利要求3所述的无人机电池,其特征在于,所述防滑结构是波纹状突起结构。
- 如权利要求1-4中任意一项所述的无人机电池,其特征在于,还包括复位弹片,所述复位弹片设置在所述卡扣按键的内侧。
- 如权利要求5所述的无人机电池,其特征在于,所述复位弹片的一端设置在所述壳体上,所述复位弹片的另一端与所述卡扣按键相接触。
- 如权利要求5或6所述的无人机电池,其特征在于,所述复位弹片呈镜像S型,镜像S型的一端卡设在所述壳体上,镜像S型的另一端的弧面与所述卡扣按键的下表面相顶接触。
- 如权利要求1-7中任意一项所述的无人机电池,其特征在于,所述卡扣按键至少为两个,相对布置在所述壳体相对于无人机的一侧的上下端。
- 一种无人机,包括无人机本体,所述无人机本体上设置有无人机电 池仓,其特征在于,所述无人机电池仓的仓口上与无人机电池壳体接触的端面设置有与卡扣按键可拆卸连接的卡扣。
- 如权利要求9所述的无人机,其特征在于,所述卡扣与所述卡扣按键接触的一面设有卡勾。
- 如权利要求9或10所述的无人机,其特征在于,所述卡扣设置在所述仓口的外表面。
- 如权利要求9-11中任一所述的无人机,其特征在于,所述卡扣至少为两个,相对布置在所述仓口相对的两侧。
- 如权利要求9-12中任一所述的无人机,其特征在于,所述无人机还包括如权利要求1-8中任一所述的无人机电池。
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP16863190.1A EP3244468B1 (en) | 2015-12-14 | 2016-10-25 | Unmanned aerial vehicle |
EP20215496.9A EP3840111B1 (en) | 2015-12-14 | 2016-10-25 | Unmanned aerial vehicle comprising battery |
US15/598,914 US10224526B2 (en) | 2015-12-14 | 2017-05-18 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US15/671,371 US9979000B2 (en) | 2015-12-14 | 2017-08-08 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US15/812,836 US10090496B2 (en) | 2015-12-14 | 2017-11-14 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US15/812,805 US10074836B2 (en) | 2015-12-14 | 2017-11-14 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US15/812,860 US10115944B2 (en) | 2015-12-14 | 2017-11-14 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US15/812,773 US10044013B2 (en) | 2015-12-14 | 2017-11-14 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
US16/180,520 US10442533B2 (en) | 2015-12-14 | 2018-11-05 | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
US16/565,911 US10745128B2 (en) | 2015-12-14 | 2019-09-10 | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
US16/986,661 US11254429B2 (en) | 2015-12-14 | 2020-08-06 | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201521037540.3U CN205376593U (zh) | 2015-12-14 | 2015-12-14 | 一种无人机电池和无人机 |
CN201521037540.3 | 2015-12-14 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15/598,914 Continuation-In-Part US10224526B2 (en) | 2015-12-14 | 2017-05-18 | Battery used for unmanned aerial vehicle and an unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2017101589A1 true WO2017101589A1 (zh) | 2017-06-22 |
Family
ID=56280580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2016/103265 WO2017101589A1 (zh) | 2015-12-14 | 2016-10-25 | 一种无人机电池和无人机 |
Country Status (5)
Country | Link |
---|---|
US (6) | US10224526B2 (zh) |
EP (2) | EP3244468B1 (zh) |
CN (1) | CN205376593U (zh) |
DE (3) | DE202016008454U1 (zh) |
WO (1) | WO2017101589A1 (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019215658A1 (en) * | 2018-05-10 | 2019-11-14 | Dronus S.R.L. | Base of stationing and automatic management for drones |
CN112740468A (zh) * | 2020-03-02 | 2021-04-30 | 深圳市大疆创新科技有限公司 | 锁定组件与可移动平台 |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9592744B2 (en) | 2013-12-06 | 2017-03-14 | SZ DJI Technology Co., Ltd | Battery and unmanned aerial vehicle with the battery |
US10086939B2 (en) * | 2015-11-25 | 2018-10-02 | Chien-Kai Chiu | Plug-and-play multifunctional attachment of remote control rotorcraft |
US10442533B2 (en) | 2015-12-14 | 2019-10-15 | Autel Robotics Co., Ltd. | Battery used for unmanned aerial vehicle and unmanned aerial vehicle |
CN205376593U (zh) | 2015-12-14 | 2016-07-06 | 深圳市道通智能航空技术有限公司 | 一种无人机电池和无人机 |
KR101919574B1 (ko) * | 2016-05-27 | 2018-11-19 | 주식회사 유비파이 | 무인항공기 |
WO2018010122A1 (en) * | 2016-07-13 | 2018-01-18 | SZ DJI Technology Co., Ltd. | Vehicle chassis and vehicle,method,and kit relating to the same |
CN106275460A (zh) * | 2016-08-15 | 2017-01-04 | 张琬彬 | 一种无人机电池安装结构 |
CN107074372B (zh) * | 2016-11-02 | 2019-03-29 | 深圳市大疆创新科技有限公司 | 一种电池收纳装置及无人机 |
CN206179949U (zh) * | 2016-11-11 | 2017-05-17 | 深圳市大疆创新科技有限公司 | 无人机电池仓及无人机 |
CN206528646U (zh) * | 2017-02-24 | 2017-09-29 | 深圳市大疆创新科技有限公司 | 电池仓及无人飞行器 |
CN107891991A (zh) * | 2017-05-11 | 2018-04-10 | 天宇科技有限公司 | 无人机 |
KR102323447B1 (ko) * | 2017-06-08 | 2021-11-08 | 삼성전자주식회사 | 가변형 무인비행체 |
CN109075276A (zh) * | 2017-08-04 | 2018-12-21 | 深圳市大疆灵眸科技有限公司 | 电池安装结构及摇轮控制器 |
USD862285S1 (en) * | 2017-08-25 | 2019-10-08 | MerchSource, LLC | Drone |
USD864082S1 (en) * | 2017-10-09 | 2019-10-22 | Guangdong Shiji Technology Co., Ltd | Quadcopter |
USD864083S1 (en) * | 2017-10-09 | 2019-10-22 | Guangdong Shiji Technology Co., Ltd | Quadcopter |
USD858353S1 (en) * | 2017-10-30 | 2019-09-03 | Shenzhen Valuelink E-Commerce Co., Ltd. | Drone |
USD858352S1 (en) * | 2017-10-30 | 2019-09-03 | Shenzhen Valuelink E-Commerce Co., Ltd. | Drone |
USD864022S1 (en) * | 2018-03-30 | 2019-10-22 | Shenzhen Valuelink E-Commerce Co., Ltd. | Unmanned aerial vehicle |
USD860047S1 (en) * | 2018-04-08 | 2019-09-17 | Shenzhen Valuelink E-Commerce Co., Ltd. | Unmanned aerial vehicle |
USD873175S1 (en) * | 2018-05-23 | 2020-01-21 | Shenzhen Hubsan Technology Co., Ltd. | Drone |
CN110232842A (zh) * | 2018-05-25 | 2019-09-13 | 袁幸福 | 一种逻辑思维训练机及其算法步骤 |
CN111356639A (zh) * | 2019-03-19 | 2020-06-30 | 深圳市大疆创新科技有限公司 | 无人机和电池 |
DE102020104783A1 (de) | 2020-02-24 | 2021-08-26 | Volocopter Gmbh | Batteriehaltevorrichtung, Batteriesystem, Fluggerät und Verfahren zum Wechseln einer Batterie für ein Fluggerät |
CN112531244B (zh) * | 2020-12-03 | 2023-03-24 | 安徽信息工程学院 | 一种基于新能源汽车的高稳定性锂电池组 |
DE102021105378A1 (de) | 2021-03-05 | 2022-09-08 | Volocopter Gmbh | Verfahren zur Kühlung einer Batterie und Kühlsystem |
DE102021105375A1 (de) | 2021-03-05 | 2022-09-08 | Volocopter Gmbh | Batteriekühlvorrichtung und Verfahren zur Kühlung einer Batteriezelle eines elektrisch angetriebenen Fluggerätes |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101472413A (zh) * | 2007-12-27 | 2009-07-01 | 鸿富锦精密工业(深圳)有限公司 | 翻盖型电子装置外壳 |
CN204596856U (zh) * | 2015-04-17 | 2015-08-26 | 深圳一电科技有限公司 | 电池包及无人机 |
CN205376593U (zh) * | 2015-12-14 | 2016-07-06 | 深圳市道通智能航空技术有限公司 | 一种无人机电池和无人机 |
Family Cites Families (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0734083B1 (en) | 1995-02-23 | 1999-12-01 | Makita Corporation | Attachment structure of battery pack to power-driven tools |
US5589288A (en) | 1995-07-31 | 1996-12-31 | Black & Decker, Inc. | Cordless power tool having a push button battery release arrangement |
CA2190572A1 (en) | 1995-11-24 | 1997-05-25 | Wille Kottke | Battery latch for a communication device |
TW376204U (en) | 1998-05-12 | 1999-12-01 | Mitac Int Corp | Safety device of slip-proof for the battery case |
US6136467A (en) | 1998-08-02 | 2000-10-24 | Motorola, Inc. | Latch system for battery housing |
US6660427B1 (en) | 2000-11-06 | 2003-12-09 | Motorola Inc. | Latch assembly for portable electronic device |
CN2451270Y (zh) | 2000-11-29 | 2001-10-03 | 陈颖 | 直流充电便携式电钻 |
US20020125857A1 (en) | 2001-03-09 | 2002-09-12 | Thomas Mastaler | Battery adapter for a cordless power tool system and related method |
US6729413B2 (en) * | 2001-08-24 | 2004-05-04 | Black & Decker Inc. | Power tool with battery pack ejector |
US6623049B2 (en) | 2001-12-21 | 2003-09-23 | Motorola, Inc. | Battery latch |
US7989969B2 (en) | 2002-06-06 | 2011-08-02 | Black & Decker Inc. | Universal power tool battery pack coupled to a portable internal combustion engine |
US7589500B2 (en) | 2002-11-22 | 2009-09-15 | Milwaukee Electric Tool Corporation | Method and system for battery protection |
NZ534475A (en) | 2004-08-02 | 2007-01-26 | Tait Electronics Ltd | Battery latching assembly of portable communication device, with contacts that slide apart to latch and are squeezed together to unlatch |
JP4026632B2 (ja) * | 2004-08-12 | 2007-12-26 | セイコーエプソン株式会社 | 小型飛行体 |
KR100651987B1 (ko) | 2004-09-18 | 2006-12-01 | 엘지전자 주식회사 | 이동통신 단말기 |
JP5103726B2 (ja) | 2005-10-28 | 2012-12-19 | マックス株式会社 | 電池パック |
JP4993176B2 (ja) | 2006-09-07 | 2012-08-08 | 日立工機株式会社 | 電池パック及び電池パックを用いた電動工具 |
JP4600415B2 (ja) * | 2007-03-30 | 2010-12-15 | ソニー株式会社 | バッテリパック |
US8534717B2 (en) | 2009-04-30 | 2013-09-17 | Motorola Solutions, Inc. | Interconnect assembly |
CN102484227B (zh) * | 2009-08-05 | 2014-12-24 | 贝洱两合公司 | 用于储能器的固定装置 |
CN201528005U (zh) | 2009-11-19 | 2010-07-14 | 南京德朔实业有限公司 | 电池包锁定装置 |
CN201728641U (zh) | 2010-07-23 | 2011-02-02 | 宁波良业电器有限公司 | 便于装卸的电池包 |
DE102011003538A1 (de) * | 2011-02-02 | 2012-08-02 | Behr Gmbh & Co. Kg | Verspannungsbügel |
CN103561916B (zh) * | 2011-08-01 | 2016-07-27 | 英格索尔-兰德公司 | 包括具有非连结线性滑动件的动力工具的装置及相关联的方法 |
JP2013226855A (ja) | 2012-04-24 | 2013-11-07 | Sumitomo Electric Ind Ltd | 飛行体用電源装置及び航空機 |
US8973861B2 (en) | 2012-10-29 | 2015-03-10 | Shenzhen Hubsan Technology Co., Ltd. | Tetra-propeller aircraft |
US9592744B2 (en) | 2013-12-06 | 2017-03-14 | SZ DJI Technology Co., Ltd | Battery and unmanned aerial vehicle with the battery |
USD740222S1 (en) | 2014-04-11 | 2015-10-06 | SZ DJI Technology Co., Ltd. | Chargeable battery |
FR3020282B1 (fr) | 2014-04-24 | 2016-05-13 | Parrot | Platine universelle de montage pour drone a voilure tournante |
US9393683B2 (en) | 2014-05-02 | 2016-07-19 | M. W. Bevins Co. | Conductive boot for power tool protection |
CN106458318A (zh) | 2014-05-23 | 2017-02-22 | 莉莉机器人公司 | 用于照相和/或摄像的无人航拍直升机 |
JP6395835B2 (ja) * | 2014-08-08 | 2018-09-26 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co.,Ltd | Uavのバッテリー電源バックアップシステムおよび方法 |
CN204230319U (zh) | 2014-08-29 | 2015-03-25 | 深圳市大疆创新科技有限公司 | 电动装置、电池模块以及电池仓 |
CN204144349U (zh) | 2014-08-29 | 2015-02-04 | 深圳市大疆创新科技有限公司 | 电动装置、电池模块以及电池单元 |
CN204230318U (zh) | 2014-08-29 | 2015-03-25 | 深圳市大疆创新科技有限公司 | 电动装置、电池模块以及电池仓 |
CN204223172U (zh) | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | 旋翼飞行器电池安装结构 |
CN104505477B (zh) | 2014-12-16 | 2016-08-31 | 湖南基石信息技术有限公司 | 电池封装结构及电池 |
CN204415738U (zh) | 2014-12-29 | 2015-06-24 | 深圳一电科技有限公司 | 电池及无人机 |
CN204614830U (zh) | 2015-04-08 | 2015-09-02 | 优利科技有限公司 | 飞行器的电池组件及包含其的飞行器 |
CN204651359U (zh) | 2015-06-01 | 2015-09-16 | 深圳市大疆创新科技有限公司 | 电池组件及应用该电池的电子装置 |
US10336451B2 (en) | 2015-06-30 | 2019-07-02 | Gopro, Inc. | Coupling assembly for a removable propeller |
CN204966559U (zh) | 2015-09-08 | 2016-01-13 | 深圳市大疆创新科技有限公司 | 移动装置及其电池模组 |
CN205005377U (zh) | 2015-09-08 | 2016-01-27 | 深圳市大疆创新科技有限公司 | 移动装置及其电池模组 |
WO2017041220A1 (zh) | 2015-09-08 | 2017-03-16 | 深圳市大疆创新科技有限公司 | 移动装置及其电池模组和锁定装置 |
CN205159402U (zh) | 2015-11-30 | 2016-04-13 | 零度智控(北京)智能科技有限公司 | 一种无人机用电池结构 |
CN205645917U (zh) | 2016-03-31 | 2016-10-12 | 优利科技有限公司 | 电池结构及飞行器 |
WO2017204592A1 (ko) | 2016-05-27 | 2017-11-30 | 주식회사 유비파이 | 무인항공기 |
CN206077007U (zh) | 2016-09-27 | 2017-04-05 | 深圳市大疆创新科技有限公司 | 电池卡合机构、电池和无人机以及充电装置 |
CN206719560U (zh) | 2017-04-26 | 2017-12-08 | 深圳市大疆创新科技有限公司 | 一种无人飞行器 |
-
2015
- 2015-12-14 CN CN201521037540.3U patent/CN205376593U/zh not_active Ceased
-
2016
- 2016-10-25 EP EP16863190.1A patent/EP3244468B1/en active Active
- 2016-10-25 WO PCT/CN2016/103265 patent/WO2017101589A1/zh active Application Filing
- 2016-10-25 DE DE202016008454.3U patent/DE202016008454U1/de active Active
- 2016-10-25 EP EP20215496.9A patent/EP3840111B1/en active Active
- 2016-10-25 DE DE202016008452.7U patent/DE202016008452U1/de active Active
- 2016-10-25 DE DE202016008455.1U patent/DE202016008455U1/de active Active
-
2017
- 2017-05-18 US US15/598,914 patent/US10224526B2/en active Active
- 2017-08-08 US US15/671,371 patent/US9979000B2/en active Active
- 2017-11-14 US US15/812,805 patent/US10074836B2/en active Active
- 2017-11-14 US US15/812,836 patent/US10090496B2/en active Active
- 2017-11-14 US US15/812,773 patent/US10044013B2/en not_active Expired - Fee Related
- 2017-11-14 US US15/812,860 patent/US10115944B2/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101472413A (zh) * | 2007-12-27 | 2009-07-01 | 鸿富锦精密工业(深圳)有限公司 | 翻盖型电子装置外壳 |
CN204596856U (zh) * | 2015-04-17 | 2015-08-26 | 深圳一电科技有限公司 | 电池包及无人机 |
CN205376593U (zh) * | 2015-12-14 | 2016-07-06 | 深圳市道通智能航空技术有限公司 | 一种无人机电池和无人机 |
Non-Patent Citations (1)
Title |
---|
See also references of EP3244468A4 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019215658A1 (en) * | 2018-05-10 | 2019-11-14 | Dronus S.R.L. | Base of stationing and automatic management for drones |
US11745875B2 (en) | 2018-05-10 | 2023-09-05 | Dronus S.P.A. | Base of stationing and automatic management for drones |
CN112740468A (zh) * | 2020-03-02 | 2021-04-30 | 深圳市大疆创新科技有限公司 | 锁定组件与可移动平台 |
Also Published As
Publication number | Publication date |
---|---|
US10090496B2 (en) | 2018-10-02 |
US20170256763A1 (en) | 2017-09-07 |
US10044013B2 (en) | 2018-08-07 |
US20180069218A1 (en) | 2018-03-08 |
DE202016008454U1 (de) | 2018-01-22 |
EP3244468A1 (en) | 2017-11-15 |
EP3840111B1 (en) | 2024-01-17 |
US20180069217A1 (en) | 2018-03-08 |
US9979000B2 (en) | 2018-05-22 |
US10224526B2 (en) | 2019-03-05 |
US10074836B2 (en) | 2018-09-11 |
US20170338455A1 (en) | 2017-11-23 |
DE202016008455U1 (de) | 2018-01-18 |
US10115944B2 (en) | 2018-10-30 |
DE202016008452U1 (de) | 2018-01-18 |
EP3244468B1 (en) | 2021-03-03 |
EP3244468A4 (en) | 2017-12-13 |
EP3840111A1 (en) | 2021-06-23 |
CN205376593U (zh) | 2016-07-06 |
US20180076431A1 (en) | 2018-03-15 |
US20180069216A1 (en) | 2018-03-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2017101589A1 (zh) | 一种无人机电池和无人机 | |
US10442533B2 (en) | Battery used for unmanned aerial vehicle and unmanned aerial vehicle | |
US20190337618A1 (en) | Uav system | |
CN205131669U (zh) | 一种带有气体监测装置的无人机 | |
CN209008869U (zh) | 无人机吊舱安装结构及无人机设备 | |
US10086939B2 (en) | Plug-and-play multifunctional attachment of remote control rotorcraft | |
CN201849660U (zh) | 多旋翼飞行器的支臂结构 | |
CN105784003A (zh) | 一种带多功能机器人的无人机装置 | |
WO2015188560A1 (zh) | 一种多功能闪光灯 | |
CN205539876U (zh) | 防丢镜头盖 | |
CN105979130B (zh) | 云台结构和摄像模组 | |
CN209023127U (zh) | 一种应用在固定翼无人机上的电池安装结构 | |
CN203761484U (zh) | 一种无人直升机的夜间探照及视频拍摄装置 | |
CN205845287U (zh) | 一种无人机地面控制系统 | |
CN205334036U (zh) | 一种实现智能芯片可拆卸的投影机 | |
CN104542340A (zh) | 一种防宠物走丢的定位装置 | |
CN207759045U (zh) | 一种无人机电池插拔固定装置 | |
CN210122189U (zh) | 拆卸结构、机翼、机身主体和飞行器 | |
CN211281496U (zh) | 一种无人机电池仓安装装置 | |
CN203787087U (zh) | 一种计算机u盘保护装置 | |
CN215205366U (zh) | 一种通用搭载无人机 | |
CN205454266U (zh) | 一种新型智能家居控制器安装结构 | |
CN205591470U (zh) | 一种防止板材意外掉落的龙骨固定 | |
CN218022192U (zh) | 一种物流无人机用可脱离载货货仓 | |
CN206004769U (zh) | 一种红外遥控照相机 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
REEP | Request for entry into the european phase |
Ref document number: 2016863190 Country of ref document: EP |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 16863190 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |