WO2018032267A1 - Unmanned aerial vehicle battery mounting structure - Google Patents

Unmanned aerial vehicle battery mounting structure Download PDF

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Publication number
WO2018032267A1
WO2018032267A1 PCT/CN2016/095321 CN2016095321W WO2018032267A1 WO 2018032267 A1 WO2018032267 A1 WO 2018032267A1 CN 2016095321 W CN2016095321 W CN 2016095321W WO 2018032267 A1 WO2018032267 A1 WO 2018032267A1
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WO
WIPO (PCT)
Prior art keywords
plate
mounting
cover plate
battery
cavity
Prior art date
Application number
PCT/CN2016/095321
Other languages
French (fr)
Chinese (zh)
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/CN2016/095321 priority Critical patent/WO2018032267A1/en
Publication of WO2018032267A1 publication Critical patent/WO2018032267A1/en

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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
    • H01M50/244—Secondary casings; Racks; Suspension devices; Carrying devices; Holders characterised by their mounting method
    • 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 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 of them are directly installed or fixed with a cable tie, etc. It is inconvenient to install and disassemble.
  • the technical problem to be solved by the present invention is to provide a UAV battery mounting structure that is convenient to install and disassemble, in view of the above-mentioned drawbacks of the prior art.
  • a drone battery mounting structure comprising a mounting plate and a cover plate; wherein the mounting plate is provided with a first cavity for mounting a battery; and the cover plate is provided with a corresponding corresponding to the first cavity a second cavity; further comprising a connection structure connecting the mounting plate and the cover plate, the connection structure comprising a first connection plate fixed to the mounting plate, a second connection plate fixed to the cover plate, and a hinge connecting the first connecting plate and the second connecting plate, wherein the hinge is provided with a torsion spring; the rear end of the mounting plate is provided with a first mounting screw hole; Second, install the screw holes.
  • the hinge is provided with an opening groove that cooperates with both end portions of the torsion spring.
  • the UAV battery mounting structure of the present invention wherein the first cavity and the bottom of the second cavity are provided with a buffer pad.
  • the unmanned battery installation structure of the present invention wherein the first cavity and the second cavity sidewall are provided with a shock absorbing strip.
  • the utility model has the beneficial effects that: when the battery is installed, the cover plate is opened upward, and the position of the first cavity is correspondingly inserted into the battery, and the torsion spring elastically acts to fix the cover plate and the lower package on the mounting plate for fixing, and then pass the first A mounting screw hole and a second mounting screw hole are used for screw fixing, the fixing effect is good, the disassembly and assembly is convenient, and the overall weight is small; the overall structure is simple and the cost is low.
  • FIG. 1 is a schematic view showing the structure of a battery installation structure of a drone according to a preferred embodiment of the present invention.
  • the unmanned battery installation structure of the preferred embodiment of the present invention includes a mounting plate 1 and a cover plate 2; the mounting plate 1 is provided with a first cavity 10 for mounting a battery; and the cover plate 2 is provided with a second cavity 20 corresponding to the first cavity 10; further comprising a connecting structure 3 connecting the mounting plate 1 and the cover plate 2, the connecting structure 3 comprising a first connecting plate 30 fixed to the mounting plate 1 and fixed to the cover plate 2 a second connecting plate 31 and a hinge 32 connecting the first connecting plate 30 and the second connecting plate 31.
  • the hinge 32 is provided with a torsion spring (not shown); the rear end of the mounting plate 1 is provided with a first mounting screw hole 11; the rear end of the cover plate 2 is provided with a second mounting screw hole 21; when the battery is installed, the cover plate 2 is opened upward, the position of the first cavity 10 is correspondingly inserted into the battery, and the torsion spring (not shown) is under the elastic action
  • the cover plate 2 and the mounting plate 1 are clamped and held by the battery for fixing, and then fixed by the first mounting screw hole 11 and the second mounting screw hole 21, the fixing effect is good, the disassembly and assembly is convenient, and the overall weight is small; the overall structure Simple and low cost.
  • the hinge 32 is provided with an opening groove (not shown) that engages both end portions of a torsion spring (not shown) to improve overall stability and is not easily displaced.
  • the bottom of the first cavity 10 and the second cavity 20 are provided with a buffer pad 4 , and the buffering effect is good and the battery surface is not easily deformed by external force after being fixed.
  • the side walls of the first cavity 10 and the second cavity 20 are provided with a shock absorbing strip 5 to reduce the influence of the battery when a side impact occurs.

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

An unmanned aerial vehicle battery mounting structure, comprising a mounting plate (1) and a cover plate (2). A first concave cavity (10) for mounting a battery is arranged on the mounting plate (1), and a second concave cavity (20) corresponding to the first concave cavity (10) is arranged on the cover plate (2). The structure also comprises a connection structure (3) connecting the mounting plate (1) and the cover plate (2), the connection structure (3) comprising a first connection plate (30) fixed to the mounting plate (1), a second connection plate (31) fixed to the cover plate (2) and a hinge (32) connecting the first connection plate (30) and the second connection plate (31), the inside of the hinge (32) being provided with a torsion spring. A tail end of the mounting plate (1) is provided with a first mounting screw hole (11), and a tail end of the cover plate (2) is provided with a second mounting screw hole (21). When the battery is mounted, the cover plate (2) is opened upwards, the battery is loaded in correspondence with the position of the first concave cavity (10), the torsion spring causes the cover plate (2) and the mounting plate (1) to clamp the battery from the top and bottom via a spring action for fixing, and screw fixing is performed via the first mounting screw hole (11) and the second mounting screw hole (21). The fixing effect is good, disassembly is convenient, the overall weight is small, the whole structure is simple and costs are low.

Description

一种无人机电池安装结构  UAV battery installation structure 技术领域Technical field
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结构。The present invention relates to the field of drone technology, and more particularly to a drone battery mounting structure.
背景技术Background technique
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；目前使用的无人机电池安装时大都直接安装或用扎带等与机身固定，安装与拆卸均较为不便。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 of them are directly installed or fixed with a cable tie, etc. It is inconvenient to install and disassemble.
技术问题technical problem
本发明要解决的技术问题在于，针对现有技术的上述缺陷，提供一种安装拆卸方便的无人机电池安装结构。The technical problem to be solved by the present invention is to provide a UAV battery mounting structure that is convenient to install and disassemble, in view of the above-mentioned drawbacks of the prior art.
技术解决方案Technical solution
本发明解决其技术问题所采用的技术方案是：The technical solution adopted by the present invention to solve the technical problem thereof is:
构造一种无人机电池安装结构，包括安装板和盖板；其中，所述安装板上设置有安装电池的第一凹腔；所述盖板上设置有与所述第一凹腔对应的第二凹腔；还包括连接所述安装板和所述盖板的连接结构，所述连接结构包括与所述安装板固定的第一连接板、与所述盖板固定的第二连接板和连接所述第一连接板和所述第二连接板的合页，所述合页内设置有扭力弹簧；所述安装板尾端设置有第一安装螺孔；所述盖板尾端设置有第二安装螺孔。Constructing a drone battery mounting structure, comprising a mounting plate and a cover plate; wherein the mounting plate is provided with a first cavity for mounting a battery; and the cover plate is provided with a corresponding corresponding to the first cavity a second cavity; further comprising a connection structure connecting the mounting plate and the cover plate, the connection structure comprising a first connection plate fixed to the mounting plate, a second connection plate fixed to the cover plate, and a hinge connecting the first connecting plate and the second connecting plate, wherein the hinge is provided with a torsion spring; the rear end of the mounting plate is provided with a first mounting screw hole; Second, install the screw holes.
本发明所述的无人机电池安装结构，其中，所述合页上设置有与所述扭力弹簧两端部配合的开口槽。In the unmanned battery installation structure of the present invention, the hinge is provided with an opening groove that cooperates with both end portions of the torsion spring.
本发明所述的无人机电池安装结构，其中，所述第一凹腔和所述第二凹腔底部均设置有缓冲垫片。The UAV battery mounting structure of the present invention, wherein the first cavity and the bottom of the second cavity are provided with a buffer pad.
本发明所述的无人机电池安装结构，其中，所述第一凹腔和所述第二凹腔侧壁设置有减震条。The unmanned battery installation structure of the present invention, wherein the first cavity and the second cavity sidewall are provided with a shock absorbing strip.
有益效果Beneficial effect
本发明的有益效果在于：电池安装时，向上掀开盖板，第一凹腔位置对应装入电池，扭力弹簧在弹性作用下使得盖板与安装板上下包夹住电池进行固定，而后通过第一安装螺孔和第二安装螺孔进行螺丝固定，固定效果好且拆装方便，同时整体重量小；整体结构简单，成本低。 The utility model has the beneficial effects that: when the battery is installed, the cover plate is opened upward, and the position of the first cavity is correspondingly inserted into the battery, and the torsion spring elastically acts to fix the cover plate and the lower package on the mounting plate for fixing, and then pass the first A mounting screw hole and a second mounting screw hole are used for screw fixing, the fixing effect is good, the disassembly and assembly is convenient, and the overall weight is small; the overall structure is simple and the cost is low.
附图说明DRAWINGS
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：In order to more clearly illustrate the embodiments of the present invention or the prior art, the present invention will be further described in conjunction with the accompanying drawings and embodiments. For ordinary technicians, other drawings can be obtained based on these drawings without any creative work:
图1是本发明较佳实施例的无人机电池安装结构结构示意图。1 is a schematic view showing the structure of a battery installation structure of a drone according to a preferred embodiment of the present invention.
本发明的实施方式Embodiments of the invention
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。The present invention will be described in detail with reference to the embodiments of the present invention. Not all embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without any inventive effort are within the scope of the present invention.
本发明较佳实施例的无人机电池安装结构如图1所示，包括安装板1和盖板2；安装板1上设置有安装电池的第一凹腔10；盖板2上设置有与第一凹腔10对应的第二凹腔20；还包括连接安装板1和盖板2的连接结构3，连接结构3包括与安装板1固定的第一连接板30、与盖板2固定的第二连接板31和连接第一连接板30和第二连接板31的合页32，合页32内设置有扭力弹簧（图中未显示）；安装板1尾端设置有第一安装螺孔11；盖板2尾端设置有第二安装螺孔21；电池安装时，向上掀开盖板2，第一凹腔10位置对应装入电池，扭力弹簧（图中未显示）在弹性作用下使得盖板2与安装板1上下包夹住电池进行固定，而后通过第一安装螺孔11和第二安装螺孔21进行螺丝固定，固定效果好且拆装方便，同时整体重量小；整体结构简单，成本低。As shown in FIG. 1 , the unmanned battery installation structure of the preferred embodiment of the present invention includes a mounting plate 1 and a cover plate 2; the mounting plate 1 is provided with a first cavity 10 for mounting a battery; and the cover plate 2 is provided with a second cavity 20 corresponding to the first cavity 10; further comprising a connecting structure 3 connecting the mounting plate 1 and the cover plate 2, the connecting structure 3 comprising a first connecting plate 30 fixed to the mounting plate 1 and fixed to the cover plate 2 a second connecting plate 31 and a hinge 32 connecting the first connecting plate 30 and the second connecting plate 31. The hinge 32 is provided with a torsion spring (not shown); the rear end of the mounting plate 1 is provided with a first mounting screw hole 11; the rear end of the cover plate 2 is provided with a second mounting screw hole 21; when the battery is installed, the cover plate 2 is opened upward, the position of the first cavity 10 is correspondingly inserted into the battery, and the torsion spring (not shown) is under the elastic action The cover plate 2 and the mounting plate 1 are clamped and held by the battery for fixing, and then fixed by the first mounting screw hole 11 and the second mounting screw hole 21, the fixing effect is good, the disassembly and assembly is convenient, and the overall weight is small; the overall structure Simple and low cost.
如图1所示，合页32上设置有与扭力弹簧（图中未显示）两端部配合的开口槽（图中未显示），提高整体稳定性且不易移位。As shown in Fig. 1, the hinge 32 is provided with an opening groove (not shown) that engages both end portions of a torsion spring (not shown) to improve overall stability and is not easily displaced.
如图1所示，第一凹腔10和第二凹腔20底部均设置有缓冲垫片4，缓冲效果好且固定后不易因外力导致电池表面变形。As shown in FIG. 1 , the bottom of the first cavity 10 and the second cavity 20 are provided with a buffer pad 4 , and the buffering effect is good and the battery surface is not easily deformed by external force after being fixed.
如图1所示，第一凹腔10和第二凹腔20侧壁设置有减震条5，减少发生侧面撞击时对电池影响。As shown in FIG. 1, the side walls of the first cavity 10 and the second cavity 20 are provided with a shock absorbing strip 5 to reduce the influence of the battery when a side impact occurs.
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。 It is to be understood that those skilled in the art will be able to make modifications and changes in accordance with the above description, and all such modifications and variations are intended to be included within the scope of the appended claims.

Claims (4)

  1. 一种无人机电池安装结构，包括安装板和盖板；其特征在于，所述安装板上设置有安装电池的第一凹腔；所述盖板上设置有与所述第一凹腔对应的第二凹腔；还包括连接所述安装板和所述盖板的连接结构，所述连接结构包括与所述安装板固定的第一连接板、与所述盖板固定的第二连接板和连接所述第一连接板和所述第二连接板的合页，所述合页内设置有扭力弹簧；所述安装板尾端设置有第一安装螺孔；所述盖板尾端设置有第二安装螺孔。 A UAV battery mounting structure includes a mounting plate and a cover plate; wherein the mounting plate is provided with a first cavity for mounting a battery; and the cover plate is provided with a corresponding corresponding to the first cavity a second cavity; further comprising a connection structure connecting the mounting plate and the cover plate, the connection structure comprising a first connection plate fixed to the mounting plate, and a second connection plate fixed to the cover plate And a hinge connecting the first connecting plate and the second connecting plate, wherein the hinge is provided with a torsion spring; the rear end of the mounting plate is provided with a first mounting screw hole; Second mounting screw hole.
  2. 根据权利要求1所述的无人机电池安装结构，其特征在于，所述合页上设置有与所述扭力弹簧两端部配合的开口槽。The drone battery mounting structure according to claim 1, wherein the hinge is provided with an opening groove that engages with both end portions of the torsion spring.
  3. 根据权利要求1所述的无人机电池安装结构，其特征在于，所述第一凹腔和所述第二凹腔底部均设置有缓冲垫片。The UAV battery mounting structure according to claim 1, wherein the first cavity and the bottom of the second cavity are each provided with a buffer pad.
  4. 根据权利要求1所述的无人机电池安装结构，其特征在于，所述第一凹腔和所述第二凹腔侧壁设置有减震条。 The UAV battery mounting structure according to claim 1, wherein the first cavity and the second cavity side wall are provided with a shock absorbing strip.
PCT/CN2016/095321 2016-08-15 2016-08-15 Unmanned aerial vehicle battery mounting structure WO2018032267A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/095321 WO2018032267A1 (en) 2016-08-15 2016-08-15 Unmanned aerial vehicle battery mounting structure

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Application Number Priority Date Filing Date Title
PCT/CN2016/095321 WO2018032267A1 (en) 2016-08-15 2016-08-15 Unmanned aerial vehicle battery mounting structure

Publications (1)

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WO2018032267A1 true WO2018032267A1 (en) 2018-02-22

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB417060A (en) * 1933-03-27 1934-09-27 Noel William Sands North An improved carrier or holder for supporting a battery on a motor cycle or for like purposes
US3088992A (en) * 1960-11-01 1963-05-07 Cambridge Thermionic Corp Holder for electrical components, such as batteries
US3830663A (en) * 1973-03-05 1974-08-20 Us Navy Battery holder for satellite and method
US5222711A (en) * 1992-01-27 1993-06-29 Bell Stuart D Battery hold-down
CN201549558U (en) * 2009-05-15 2010-08-11 深圳市鸿德电池有限公司 Integrated clamp for lithium ion battery liquid injection and formation
CN102569684A (en) * 2010-12-08 2012-07-11 鸿富锦精密工业（深圳）有限公司 Battery fixing device
CN106275460A (en) * 2016-08-15 2017-01-04 张琬彬 A kind of unmanned plane battery fastening structure

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB417060A (en) * 1933-03-27 1934-09-27 Noel William Sands North An improved carrier or holder for supporting a battery on a motor cycle or for like purposes
US3088992A (en) * 1960-11-01 1963-05-07 Cambridge Thermionic Corp Holder for electrical components, such as batteries
US3830663A (en) * 1973-03-05 1974-08-20 Us Navy Battery holder for satellite and method
US5222711A (en) * 1992-01-27 1993-06-29 Bell Stuart D Battery hold-down
CN201549558U (en) * 2009-05-15 2010-08-11 深圳市鸿德电池有限公司 Integrated clamp for lithium ion battery liquid injection and formation
CN102569684A (en) * 2010-12-08 2012-07-11 鸿富锦精密工业（深圳）有限公司 Battery fixing device
CN106275460A (en) * 2016-08-15 2017-01-04 张琬彬 A kind of unmanned plane battery fastening structure

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