CN111952506A - Portable unmanned aerial vehicle battery bin - Google Patents

Portable unmanned aerial vehicle battery bin Download PDF

Info

Publication number
CN111952506A
CN111952506A CN202010858710.3A CN202010858710A CN111952506A CN 111952506 A CN111952506 A CN 111952506A CN 202010858710 A CN202010858710 A CN 202010858710A CN 111952506 A CN111952506 A CN 111952506A
Authority
CN
China
Prior art keywords
box
clamping groove
aerial vehicle
unmanned aerial
storage case
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN202010858710.3A
Other languages
Chinese (zh)
Inventor
丁志敏
李明华
袁一方
唐煊阳
顾光荣
王秀境
方学智
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guizhou Power Grid Co Ltd
Original Assignee
Guizhou Power Grid Co Ltd
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 Guizhou Power Grid Co Ltd filed Critical Guizhou Power Grid Co Ltd
Priority to CN202010858710.3A priority Critical patent/CN111952506A/en
Publication of CN111952506A publication Critical patent/CN111952506A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/42Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/48Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
    • H01M10/486Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte for measuring temperature
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/61Types of temperature control
    • H01M10/613Cooling or keeping cold
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/62Heating or cooling; Temperature control specially adapted for specific applications
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/63Control systems
    • H01M10/635Control systems based on ambient temperature
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/655Solid structures for heat exchange or heat conduction
    • H01M10/6551Surfaces specially adapted for heat dissipation or radiation, e.g. fins or coatings
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/60Heating or cooling; Temperature control
    • H01M10/65Means for temperature control structurally associated with the cells
    • H01M10/656Means for temperature control structurally associated with the cells characterised by the type of heat-exchange fluid
    • H01M10/6561Gases
    • H01M10/6563Gases with forced flow, e.g. by blowers
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Abstract

The invention discloses a portable unmanned aerial vehicle battery storage box which comprises a box body, wherein the box body comprises an inner box and an outer box, a gap is formed between the inner box and the outer box, the inner box is provided with a plurality of placing areas for placing unmanned aerial vehicle batteries, and each placing area is provided with an automatic heat dissipation mechanism and a fixing mechanism. According to the unmanned aerial vehicle battery self-discharging box, the plurality of placing areas are concentrated in the box body, the box body is light and convenient to carry, low in cost, convenient to maintain and manage and convenient to transport, the batteries are completely isolated from each other, the buffer mechanism is arranged, damage can not be caused even if the batteries are extruded, and meanwhile, the automatic heat dissipation mechanism and the grounding wire are arranged, so that potential safety hazards caused by self-discharging of the unmanned aerial vehicle batteries are prevented.

Description

Portable unmanned aerial vehicle battery bin
Technical Field
The invention relates to the field of electric power auxiliary tools, in particular to a portable unmanned aerial vehicle battery storage box.
Background
Along with the development of the power grid, the application amount of the unmanned aerial vehicle in the Xinjiang province to patrol and examine in the power system is larger and larger, and a large amount of use of the unmanned aerial vehicle is brought. The large amount of applications of the unmanned aerial vehicle, along with the battery capacity of the unmanned aerial vehicle is large. General 1 unmanned aerial vehicle of personnel of patrolling and examining, configuration 15 batteries. Go out at ordinary times and patrol and examine, the unmanned aerial vehicle battery is carried with traveling bag commonly used. Due to the fact that the environment of a first-line site is severe, batteries fall off frequently, the batteries collide with each other, foreign matters enter the battery core, and the problem is more prominent in the first-line site; secondly, the carrying to the first-line site is inconvenient. The result is that unmanned aerial vehicle battery damage rate is higher, and electric core trouble often appears, and the battery rises to bulge harm scheduling problem.
Disclosure of Invention
In view of this, the invention aims to provide a portable unmanned aerial vehicle battery storage box, which has the advantages of convenience in storage and no potential safety hazard.
The purpose of the invention is realized by the following technical scheme:
the utility model provides a portable unmanned aerial vehicle battery bin, includes the box, the box includes inner box and outer container, have the clearance between inner box and the outer container, the inner box is equipped with a plurality of areas of placing that are used for placing unmanned aerial vehicle battery, every place the area and all be equipped with automatic heat dissipation mechanism and fixed establishment.
Further, the placing area is constructed in the shape of a clamping groove, the cross section of the clamping groove is rectangular, and a coating made of waterproof materials is arranged on the outer surface of the clamping groove.
Furthermore, the fixing mechanism comprises two corresponding expansion plates arranged in the width direction of the clamping groove and a cover body arranged at the top end of the clamping groove.
Furthermore, two expansion plates are connected with first elastic elements, the extension directions of the two first elastic elements are opposite, and the distance between the two expansion plates in a natural state is smaller than the length of the cross section of the unmanned aerial vehicle battery.
Furthermore, the cover body is hinged with one of the two corresponding fixing plates arranged on the clamping groove, and a thermometer is arranged on the cover body and used for measuring the temperature inside the clamping groove.
Further, the automatic heat dissipation mechanism comprises a fan arranged on one of the two expansion plates and a temperature sensor arranged on the inner wall of the clamping groove.
Further, the fan is provided with a switch which is electrically connected with the temperature sensor,
when the temperature in the clamping groove reaches a threshold value, the temperature sensor controls the switch to turn on the fan to dissipate heat.
Furthermore, a plurality of heat dissipation holes are formed in the side face of the outermost layer connection position of the inner box and the outer box.
Further, be equipped with buffer gear between inner box and the outer container, buffer gear includes the cylinder, the both ends setting of cylinder respectively with two buffering ends that the lateral wall of outer container and the lateral wall of inner box are connected, buffering end includes the second elastic element that circumference set up, second elastic element is close to the one end of cylinder be equipped with the connecting rod that the cylinder is connected, the other end is equipped with soft rubber.
Further, the outer container is made of high-strength foam, and the outer side wall of the outer container is provided with a grounding wire.
The invention has the beneficial effects that:
according to the unmanned aerial vehicle battery self-discharging box, the plurality of placing areas are concentrated in the box body, the box body is light and convenient to carry, low in cost, convenient to maintain and manage and convenient to transport, the batteries are completely isolated from each other, the buffer mechanism is arranged, damage can not be caused even if the batteries are extruded, and meanwhile, the automatic heat dissipation mechanism and the grounding wire are arranged, so that potential safety hazards caused by self-discharging of the unmanned aerial vehicle batteries are prevented.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention. The objectives and other advantages of the invention may be realized and attained by the means of the instrumentalities and combinations particularly pointed out hereinafter.
Drawings
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be further described in detail with reference to the accompanying drawings, in which:
FIG. 1 is a schematic diagram of the appearance structure of the present invention;
FIG. 2 is a schematic view of the internal structure of the present invention;
FIG. 3 is a cross-sectional view of the present invention;
FIG. 4 is a schematic structural view of a buffer mechanism;
FIG. 5 is a schematic view of a card slot structure;
FIG. 6 is a schematic view of the connection between the expansion plate and the bottom plate.
Detailed Description
Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. It should be understood that the preferred embodiments are illustrative of the invention only and are not limiting upon the scope of the invention.
In the description of the present invention, it is to be understood that the terms "longitudinal", "length", "circumferential", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically connected, electrically connected or can communicate with each other; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
This embodiment has proposed an unmanned aerial vehicle battery box, as shown in fig. 1-3, the power distribution box comprises a box body, the box includes inner box 2 and outer container 1, outer container 1 adopts the high strength foam to make, have better compressive capacity, inner box 2 realizes swing joint through buckle 5 with outer container 1, there is the clearance between inner box 2 and the outer container 1, be equipped with buffer gear 4 between the clearance, as shown in fig. 4, buffer gear 4 includes cylinder 41, two buffering ends that the both ends setting of cylinder 41 is connected with the lateral wall of outer container 1 and the lateral wall of inner box 2 respectively, the buffering end includes the second elastic element 43 that circumference set up, the one end that second elastic element 43 is close to cylinder 41 is equipped with the connecting rod 42 of being connected with cylinder 41, the other end is equipped with soft rubber 44. The function of the damper mechanism 4 is to reduce the force acting on the inner case 2 by the second elastic member 43 and the soft rubber 44 when there is a pressure applied from the outer case 1 to the inner case 2.
The inner box 2 is provided with a plurality of placing areas for placing the unmanned aerial vehicle battery, each placing area is provided with an automatic heat dissipation mechanism and a fixing mechanism, the placing areas are constructed into the shape of a clamping groove, as shown in fig. 5 and 6, the cross section of the clamping groove 3 is rectangular, and the outer side wall of the clamping groove 3 is provided with a coating made of waterproof materials. This is to prevent the risk of water droplets penetrating into the card slot 3.
The card slot 3 comprises a bottom plate 36, two corresponding expansion plates 32, two corresponding fixing plates 31 and a cover body 33 (fixing mechanism), wherein a first elastic element 35 is arranged between the expansion plates 32 and the bottom plate 36, the extension directions of the two first elastic elements 35 are opposite, and the two first elastic elements are used for providing elastic force on the expansion plates 32 in the direction close to the bottom plate 36 so as to fix the unmanned aerial vehicle battery, and the distance between the two expansion plates 32 in the natural state is smaller than the length of the cross section of the unmanned aerial vehicle battery. The cover 33 is disposed on the top of the slot 3 and hinged to one of the two fixing plates 31 for fixing the battery of the unmanned aerial vehicle. A thermometer (not shown) is provided on the cover 33, and can measure and display the temperature inside the card slot 3.
The inside automatic heat dissipation mechanism that still is equipped with of draw-in groove 3, automatic heat dissipation mechanism is including setting up fan 34 at one of two expansion plates 32 and establishing the temperature sensor (not shown in the figure) at draw-in groove 3 inner wall, fan 34 is equipped with the switch, the switch is connected with the temperature sensor electricity, when the temperature in draw-in groove 3 reaches the threshold value, temperature sensor control switch opens fan 34 and dispels the heat, be soft materials at the outmost junction of inner box 2 and outer container 1 simultaneously, and set up a plurality of louvres.
Simultaneously, the lateral wall of outer container 1 is provided with the earth connection, and this is because unmanned aerial vehicle battery laying time is too long, and in order to protect the battery inside, the battery can start from discharge system, when the box is idle, with earth connection and ground contact, prevents that the unmanned aerial vehicle battery from producing danger to the people owing to self-discharge. And the handle is made of insulating materials and arranged on the outer surface of the outer box 1. Used for lifting the box body.
Finally, the above embodiments are only intended to illustrate the technical solutions of the present invention and not to limit the present invention, and although the present invention has been described in detail with reference to the preferred embodiments, it will be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions, and all of them should be covered by the claims of the present invention.

Claims (10)

1. The utility model provides a portable unmanned aerial vehicle battery bin, its characterized in that: the novel battery box comprises a box body, the box includes inner box and outer container, have the clearance between inner box and the outer container, the inner box is equipped with a plurality of regions of placing that are used for placing unmanned aerial vehicle battery, every place the region and all be equipped with automatic heat dissipation mechanism and fixed establishment.
2. The portable drone battery storage case of claim 1, wherein: the placing area is constructed in the shape of a clamping groove, the cross section of the clamping groove is rectangular, and a coating made of waterproof materials is arranged on the outer surface of the clamping groove.
3. The portable drone battery storage case of claim 2, wherein: the fixing mechanism comprises two corresponding expansion plates arranged in the width direction of the clamping groove and a cover body arranged at the top end of the clamping groove.
4. The portable drone battery storage case of claim 3, wherein: the two expansion plates are connected with first elastic elements, the extension directions of the two first elastic elements are opposite, and the distance between the two expansion plates in a natural state is smaller than the length of the cross section of the unmanned aerial vehicle battery.
5. The portable drone battery storage case of claim 3, wherein: the cover body is hinged with one of two corresponding fixing plates arranged on the clamping groove, and a thermometer is arranged on the cover body and used for measuring the temperature inside the clamping groove.
6. The portable drone battery storage case of claim 5, wherein: the automatic heat dissipation mechanism comprises a fan arranged on one of the two expansion plates and a temperature sensor arranged on the inner wall of the clamping groove.
7. The portable drone battery storage case of claim 6, wherein: the fan is provided with a switch which is electrically connected with the temperature sensor,
when the temperature in the clamping groove reaches a threshold value, the temperature sensor controls the switch to turn on the fan to dissipate heat.
8. The portable drone battery storage case of claim 7, wherein: and a plurality of heat dissipation holes are formed in the side surface of the outermost layer joint of the inner box and the outer box.
9. The portable drone battery storage case of claim 1, wherein: be equipped with buffer gear between inner box and the outer container, buffer gear includes the cylinder, the both ends setting of cylinder respectively with two buffering ends that the lateral wall of outer container and the lateral wall of inner box are connected, buffering end includes the second elastic element that circumference set up, second elastic element is close to the one end of cylinder be equipped with the connecting rod that the cylinder is connected, the other end is equipped with soft rubber.
10. The portable drone battery storage case of claim 1, wherein: the outer container is made of high-strength materials, and the outer side wall of the outer container is provided with a grounding wire.
CN202010858710.3A 2020-08-24 2020-08-24 Portable unmanned aerial vehicle battery bin Pending CN111952506A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010858710.3A CN111952506A (en) 2020-08-24 2020-08-24 Portable unmanned aerial vehicle battery bin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010858710.3A CN111952506A (en) 2020-08-24 2020-08-24 Portable unmanned aerial vehicle battery bin

Publications (1)

Publication Number Publication Date
CN111952506A true CN111952506A (en) 2020-11-17

Family

ID=73360209

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010858710.3A Pending CN111952506A (en) 2020-08-24 2020-08-24 Portable unmanned aerial vehicle battery bin

Country Status (1)

Country Link
CN (1) CN111952506A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112993461A (en) * 2021-02-19 2021-06-18 山东水发智慧能源有限公司 Lithium battery convenient for heat dissipation and installation method thereof
CN113844774A (en) * 2021-09-24 2021-12-28 广东电网有限责任公司 Outdoor storage device of unmanned aerial vehicle battery

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206022461U (en) * 2016-08-17 2017-03-15 陈丙彦 A kind of battery for electric automobile case of easy access
CN106992276A (en) * 2017-06-14 2017-07-28 滨州学院 A kind of unmanned plane battery charging management cabinet
CN107293667A (en) * 2017-06-08 2017-10-24 深圳市奈士迪技术研发有限公司 A kind of new energy car battery case
CN107768576A (en) * 2017-11-26 2018-03-06 惠州市海诚润滑油有限公司 Elasticity installation buffer structure
CN210296435U (en) * 2019-07-05 2020-04-10 上海能辉科技股份有限公司 Energy storage battery container

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN206022461U (en) * 2016-08-17 2017-03-15 陈丙彦 A kind of battery for electric automobile case of easy access
CN107293667A (en) * 2017-06-08 2017-10-24 深圳市奈士迪技术研发有限公司 A kind of new energy car battery case
CN106992276A (en) * 2017-06-14 2017-07-28 滨州学院 A kind of unmanned plane battery charging management cabinet
CN107768576A (en) * 2017-11-26 2018-03-06 惠州市海诚润滑油有限公司 Elasticity installation buffer structure
CN210296435U (en) * 2019-07-05 2020-04-10 上海能辉科技股份有限公司 Energy storage battery container

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112993461A (en) * 2021-02-19 2021-06-18 山东水发智慧能源有限公司 Lithium battery convenient for heat dissipation and installation method thereof
CN113844774A (en) * 2021-09-24 2021-12-28 广东电网有限责任公司 Outdoor storage device of unmanned aerial vehicle battery

Similar Documents

Publication Publication Date Title
CN111952506A (en) Portable unmanned aerial vehicle battery bin
CN207529980U (en) A kind of power battery pack and new-energy automobile
CN201387911Y (en) Storage battery module
CN210775242U (en) Novel transmission line ice observation device
CA2109754A1 (en) Lead-acid battery of the absorptive mat type with improved heat transfer
CN101651192A (en) Lithium-ion power battery box
CN112151893A (en) Storage battery with USB output electric energy controllable
CN209526185U (en) Electrokinetic cell system for automobile
CN209738995U (en) Sensor combination device for unmanned vehicle
CN210430017U (en) Battery box
CN218448254U (en) Small lithium battery for offshore operation equipment
CN215793222U (en) All-directional mobile intelligent energy-saving new energy charging station
CN212648311U (en) Lithium titanate battery pack
CN213905541U (en) Protective cover for battery module of wall-climbing robot
KR102045707B1 (en) Case for battery pack
CN213457971U (en) Power supply management device of distributed server
CN219180662U (en) Domestic energy storage multi-string lithium battery pack protection board
CN219067032U (en) Novel model aeroplane and model ship battery structure
CN217009279U (en) Submersible lithium battery system
CN220106713U (en) Lithium battery module and electric equipment
CN216161850U (en) Waterproof moped battery
CN212927157U (en) Protector for municipal works
CN220068078U (en) Multichannel heat dissipation type motor controller
CN217824870U (en) Solar cell panel with splicing structure
CN214099686U (en) Lithium battery module based on high in clouds communication

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20201117

RJ01 Rejection of invention patent application after publication