WO2018032265A1 - 一种无人机电池安装减震结构 - Google Patents

一种无人机电池安装减震结构 Download PDF

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Publication number
WO2018032265A1
WO2018032265A1 PCT/CN2016/095319 CN2016095319W WO2018032265A1 WO 2018032265 A1 WO2018032265 A1 WO 2018032265A1 CN 2016095319 W CN2016095319 W CN 2016095319W WO 2018032265 A1 WO2018032265 A1 WO 2018032265A1
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WO
WIPO (PCT)
Prior art keywords
battery
box body
cover body
self
locking screw
Prior art date
Application number
PCT/CN2016/095319
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English (en)
French (fr)
Inventor
张琬彬
Original Assignee
张琬彬
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 张琬彬 filed Critical 张琬彬
Priority to PCT/CN2016/095319 priority Critical patent/WO2018032265A1/zh
Publication of WO2018032265A1 publication Critical patent/WO2018032265A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • 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
    • H01M50/233—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions
    • H01M50/242—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries against vibrations, collision impact or swelling
    • 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 invention relates to the field of drone technology, and more particularly to a drone battery mounting shock absorbing structure.
  • UAVs are unmanned aircraft operated by radio remote control equipment and self-provided program control devices. Civil drones have important applications in aerial photography, agriculture, plant protection, disaster relief, etc. Most drones have their own batteries. Battery power is used as the power. The battery installation box currently used has poor protection against the battery, and it is easy to damage the battery in the event of an accidental collision.
  • the technical problem to be solved by the present invention is to provide a shock absorber structure for a UAV battery with good battery protection effect against the above-mentioned drawbacks of the prior art.
  • a drone battery mounting shock absorbing structure comprising a box body; wherein the box body is open at one end and the other end surface is provided with a wire hole; the inner wall of the box body is fixedly provided with a finite block and a plurality of wave shapes a buffer strip; further comprising a cover body engaged with the opening, the cover body is rotatably connected to the box body; the cover body is provided with a plurality of cushioning feet on the lower surface; the cover body is provided with a self-locking screw; The casing is provided with a screw hole that cooperates with the self-locking screw.
  • the unmanned aerial vehicle battery of the present invention is provided with a shock absorbing structure, wherein the limiting block is an excellent rubber block.
  • the unmanned aerial vehicle battery of the present invention is provided with a shock absorbing structure, wherein the cover body is provided with a through hole that cooperates with the self-locking screw, and the through hole is provided with an annular bayonet; the self-locking screw An annular groove is provided on the bayonet.
  • the unmanned aerial vehicle battery of the present invention is provided with a shock absorbing structure, wherein a plurality of through grooves are arranged on the upper and lower surfaces of the casing.
  • the utility model has the beneficial effects that: in use, the battery extends into the opening position of the box body, and the power line is connected through the line hole, and the limiting block limits the front end of the battery and acts as an insertion in-position signal, and the buffer strip is deformed and compacted.
  • the two sides of the battery, and the back cover is tightly closed, the cushioning foot is against the rear end of the battery, which effectively reduces vibration and displacement of the battery, and is easy to install and light in weight; the overall structure is simple and the cost is low.
  • FIG. 1 is a schematic view showing the structure of a shock absorber structure for a battery of a drone according to a preferred embodiment of the present invention.
  • the UAV battery installation damping structure of the preferred embodiment of the present invention includes a UAV battery mounting damping structure, including a box body 1 , the box body 1 is open at one end, and the other end surface is provided with The through hole 10; the inner wall of the casing 1 is fixedly provided with the limiting block 11 and the plurality of undulating buffer strips 12; further comprising a cover body 2 matched with the opening, the cover body 2 is rotatably connected with the casing 1; the lower surface of the cover body 2 is disposed There are a plurality of cushioning legs 20; the cover body 2 is provided with a self-locking screw 21; the casing 1 is provided with a screw hole 13 for engaging with the self-locking screw 21; in use, the battery extends into the opening position of the casing 1 and passes through The wire hole 10 is connected to the power line, and the limiting block 11 limits the front end of the battery and acts as an insertion in-position signal.
  • the buffer strip 12 is deformed and pressed against the two sides of the battery, and the rear cover is tightly closed to the cover body 2, and the cushioning foot 20 is pressed against the battery.
  • the end effectively reduces vibration and displacement of the battery, and is easy to install and light in weight; the overall structure is simple and the cost is low.
  • the limiting block 11 is an excellent rubber block, which improves the shock absorption buffer effect and further improves the protection effect.
  • the cover body 2 is provided with a through hole 22 for engaging with the self-locking screw 21 .
  • the through hole 22 is provided with an annular bayonet 220 .
  • the self-locking screw 21 is provided with an annular groove 210 for engaging with the bayonet 220 . The installation is more convenient and not easy to fall off.
  • the upper and lower surfaces of the casing 1 are provided with a plurality of through grooves (not shown) to reduce the overall weight and improve the heat dissipation effect.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Battery Mounting, Suspending (AREA)

Abstract

一种无人机电池安装减震结构，包括盒体(1)，盒体(1)一端开口设置，另一端表面设置有过线孔(10)；盒体(1)内壁固定设置有限位块(11)和多个波浪形缓冲条(12)；还包括与开口配合的盖体(2)，盖体(2)与盒体(1)转动连接；盖体(2)下表面设置有多个缓冲垫脚(20)；盖体(2)上设置有自锁螺丝(21)；盒体(1)上设置有与自锁螺丝(21)配合的螺孔(13)；使用时，电池延盒体(1)开口位置装入，通过过线孔(10)连接出电源线，同时限位块(11)对电池前端进行限位并作为插入到位信号，缓冲条(12)发生形变压紧电池两侧，而后盖紧盖体(2)，缓冲垫脚(20)抵住电池后端，有效减少震动以及电池发生位移情况，且安装简便，重量较轻；整体结构简单，成本低。

Description

一种无人机电池安装减震结构 技术领域
本发明涉及无人机技术领域，更具体地说，涉及一种无人机电池安装减震结构。
 背景技术
无人机是利用无线电遥控设备和自备的程序控制装置操纵的不载人飞机，民用无人机在航拍、农业、植保、救灾等领域有着较重要应用；无人机大都自带电池，依靠电池电能作为动力，目前使用的电池安装盒对电池保护力度较差，发生意外碰撞时易损坏电池。
 技术问题
本发明要解决的技术问题在于，针对现有技术的上述缺陷，提供一种对电池保护效果好的无人机电池安装减震结构。
 技术解决方案
本发明解决其技术问题所采用的技术方案是：
构造一种无人机电池安装减震结构，包括盒体；其中，所述盒体一端开口设置，另一端表面设置有过线孔；所述盒体内壁固定设置有限位块和多个波浪形缓冲条；还包括与所述开口配合的盖体，所述盖体与所述盒体转动连接；所述盖体下表面设置有多个缓冲垫脚；所述盖体上设置有自锁螺丝；所述盒体上设置有与所述自锁螺丝配合的螺孔。
本发明所述的无人机电池安装减震结构，其中，所述限位块为优力胶块。
本发明所述的无人机电池安装减震结构，其中，所述盖体上设置有与所述自锁螺丝配合的通孔，所述通孔内设置有环形卡口；所述自锁螺丝上设置有与所述卡口配合的环形槽。
本发明所述的无人机电池安装减震结构，其中，所述盒体上下表面设置有多个通槽。
 有益效果
本发明的有益效果在于：使用时，电池延盒体开口位置装入，通过过线孔连接出电源线，同时限位块对电池前端进行限位并作为插入到位信号，缓冲条发生形变压紧电池两侧，而后盖紧盖体，缓冲垫脚抵住电池后端，有效减少震动以及电池发生位移情况，且安装十分简便，重量较轻；整体结构简单，成本低。
附图说明
为了更清楚地说明本发明实施例或现有技术中的技术方案，下面将结合附图及实施例对本发明作进一步说明，下面描述中的附图仅仅是本发明的部分实施例，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附图：
图1是本发明较佳实施例的无人机电池安装减震结构结构示意图。
 本发明的实施方式
为了使本发明实施例的目的、技术方案和优点更加清楚，下面将结合本发明实施例中的技术方案进行清楚、完整的描述，显然，所描述的实施例是本发明的部分实施例，而不是全部实施例。基于本发明的实施例，本领域普通技术人员在没有付出创造性劳动的前提下所获得的所有其他实施例，都属于本发明的保护范围。
本发明较佳实施例的无人机电池安装减震结构如图1所示，包括一种无人机电池安装减震结构，包括盒体1，盒体1一端开口设置，另一端表面设置有过线孔10；盒体1内壁固定设置有限位块11和多个波浪形缓冲条12；还包括与开口配合的盖体2，盖体2与盒体1转动连接；盖体2下表面设置有多个缓冲垫脚20；盖体2上设置有自锁螺丝21；盒体1上设置有与自锁螺丝21配合的螺孔13；使用时，电池延盒体1开口位置装入，通过过线孔10连接出电源线，同时限位块11对电池前端进行限位并作为插入到位信号，缓冲条12发生形变压紧电池两侧，而后盖紧盖体2，缓冲垫脚20抵住电池后端，有效减少震动以及电池发生位移情况，且安装十分简便，重量较轻；整体结构简单，成本低。
如图1所示，限位块11为优力胶块，提高减震缓冲效果，进而提高保护效果。
如图1所示，盖体2上设置有与自锁螺丝21配合的通孔22，通孔22内设置有环形卡口220；自锁螺丝21上设置有与卡口220配合的环形槽210；安装更加便利且不易脱落。
如图1所示，盒体1上下表面设置有多个通槽（图中未显示），减轻整体重量同时提高散热效果。
应当理解的是，对本领域普通技术人员来说，可以根据上述说明加以改进或变换，而所有这些改进和变换都应属于本发明所附权利要求的保护范围。

Claims (4)

  1. 一种无人机电池安装减震结构，包括盒体；其特征在于，所述盒体一端开口设置，另一端表面设置有过线孔；所述盒体内壁固定设置有限位块和多个波浪形缓冲条；还包括与所述开口配合的盖体，所述盖体与所述盒体转动连接；所述盖体下表面设置有多个缓冲垫脚；所述盖体上设置有自锁螺丝；所述盒体上设置有与所述自锁螺丝配合的螺孔。
  2. 根据权利要求1所述的无人机电池安装减震结构，其特征在于，所述限位块为优力胶块。
  3. 根据权利要求1所述的无人机电池安装减震结构，其特征在于，所述盖体上设置有与所述自锁螺丝配合的通孔，所述通孔内设置有环形卡口；所述自锁螺丝上设置有与所述卡口配合的环形槽。
  4. 根据权利要求1所述的无人机电池安装减震结构，其特征在于，所述盒体上下表面设置有多个通槽。
PCT/CN2016/095319 2016-08-15 2016-08-15 一种无人机电池安装减震结构 WO2018032265A1 (zh)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113054314A (zh) * 2021-03-16 2021-06-29 岭南师范学院 一种多散热模式作用下的汽车动力电池强化传热系统

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CN202839804U (zh) * 2012-10-25 2013-03-27 浙江杰斯特电器有限公司 弹片衬板
CN105539857A (zh) * 2016-01-22 2016-05-04 无锡觅睿恪科技有限公司 无人机用电池卡接结构
CN106207034A (zh) * 2016-08-15 2016-12-07 张琬彬 一种无人机电池安装减震结构

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Publication number Priority date Publication date Assignee Title
CN2299791Y (zh) * 1997-09-19 1998-12-09 财团法人工业技术研究院 电动车辆的电池盒与车架结构
JP2001256939A (ja) * 2000-03-14 2001-09-21 Matsushita Electric Ind Co Ltd 電池パック
CN201021111Y (zh) * 2007-03-19 2008-02-13 美尔顿车业(东莞)有限公司 一种安装于电动车上的电池盒组件
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113054314A (zh) * 2021-03-16 2021-06-29 岭南师范学院 一种多散热模式作用下的汽车动力电池强化传热系统
CN113054314B (zh) * 2021-03-16 2022-09-13 岭南师范学院 一种多散热模式作用下的汽车动力电池强化传热系统

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