CN210349905U - Unmanned aerial vehicle battery compartment reinforcing apparatus - Google Patents
Unmanned aerial vehicle battery compartment reinforcing apparatus Download PDFInfo
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- CN210349905U CN210349905U CN201921194815.2U CN201921194815U CN210349905U CN 210349905 U CN210349905 U CN 210349905U CN 201921194815 U CN201921194815 U CN 201921194815U CN 210349905 U CN210349905 U CN 210349905U
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- battery compartment
- fixed
- aerial vehicle
- unmanned aerial
- clamping
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- 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
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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Abstract
The utility model discloses an unmanned aerial vehicle battery compartment reinforcing apparatus, including battery compartment and apron, the trompil has all been seted up at the middle part of battery compartment both sides, and two trompils alternate with two pull rods respectively and are connected, and the clamping plate is all fixedly installed to the one end of two pull rods, and the other end of two pull rods is fixed and is equipped with the pulling handle, and the surface cover of the one end of two pull rods is equipped with clamping spring, and the bottom mounting of battery compartment inside is equipped with a plurality of support bars, and one side of battery compartment top is articulated through hinge and one side of apron, the utility model relates to an unmanned aerial vehicle battery compartment reinforcing apparatus, the clamping plate is convenient for press from both sides tight to the battery through the clamping spring that sets up and clamping plate, and is convenient for pulling clamping plate through the pulling handle that sets up and pull rod; the clamping block arranged on one side of the fixed block is connected with the clamping groove arranged on the back of the battery bin in a clamping mode, and the position of the cover plate is convenient to fix.
Description
Technical Field
The utility model relates to a reinforcing apparatus, in particular to unmanned aerial vehicle battery compartment reinforcing apparatus belongs to unmanned air vehicle technical field.
Background
But current unmanned aerial vehicle adopts plug-in battery more, so that change reserve battery, thereby improve unmanned aerial vehicle's duration, unmanned aerial vehicle's battery is generally installed inside it at present, unmanned aerial vehicle's casing is equipped with the one side open battery and holds the chamber, and the apron through the casing block with unmanned aerial vehicle holds the chamber with the battery and seals, in order to hold the chamber with the battery fastening in the battery, however, when the battery is changed to needs, at first need dismantle the apron from unmanned aerial vehicle's casing, the battery that will treat to change again holds the chamber from the battery and takes out, then install reserve battery in the battery holds the chamber, the change operation of battery is just accomplished in last apron closure and locking, the troublesome poeration and also not very comprehensive to the fixed of battery, also can take place accident and cause economic loss.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle battery compartment reinforcing apparatus to the problem that the change that provides in solving above-mentioned background art is troublesome and difficult for going on fixing.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle battery compartment reinforcing device comprises a battery compartment and a cover plate, wherein the middle parts of two sides of the battery compartment are respectively provided with an opening, the two openings are respectively and alternately connected with two pull rods, one ends of the two pull rods are respectively and fixedly provided with a clamping plate, the other ends of the two pull rods are fixedly provided with a pull handle, the surface of one end of each of the two pull rods is sleeved with a clamping spring, the bottom end inside the battery compartment is fixedly provided with a plurality of supporting strips, one side of the top end of the battery compartment is hinged with one side of the cover plate through a hinge, the other side of the cover plate is hinged with one side of the bottom end of a fixed block through a hinge, the bottom end of one side of the fixed block is fixedly provided with a clamping block, the top part of the back surface of the battery compartment is provided with a clamping groove corresponding to the position of, the both sides of battery compartment all are fixed and are equipped with the heat dissipation fan of establishing ties each other, the middle part at the battery compartment back is fixed and is equipped with the temperature controller, the inner wall at the battery compartment back is arranged in to the test probe of temperature controller.
As a preferred technical scheme of the utility model, two the fixed screw thread post that is equipped with of one end of pull rod, two threaded hole has been seted up at the middle part of clamp plate one side, screw thread post and screw hole threaded connection.
As a preferred technical scheme of the utility model, two clamping spring's both ends are all fixed and are equipped with annular fixed plate, two the fixed orifices, two have all been seted up on annular fixed plate's surface annular fixed plate's one end all through fixing bolt respectively with one side fixed connection of two clamping plates, two annular fixed plate's the other end respectively with the both sides inner wall fixed connection of battery compartment.
As a preferred technical scheme of the utility model, two a plurality of bleeder vent has all been seted up on the surface of pinch-off blades, just a plurality of louvre has been seted up to the bottom in battery compartment.
As a preferred technical scheme of the utility model, the heat dissipation fan passes through temperature controller and battery compartment internally mounted's battery electric connection.
As an optimal technical scheme of the utility model, two the opposite side of pinch-off blades and the bottom of pressure strip all fix and are equipped with rubber buffer.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model relates to an unmanned aerial vehicle battery compartment reinforcing apparatus, the both sides of battery are convenient for press from both sides tightly through clamping spring and the pinch plate that sets up, and be convenient for pull the pinch plate through the pull handle and the pull rod that set up and move clamping spring and contract, thereby be convenient for take out the battery; the clamping block arranged on one side of the fixed block is clamped and connected with the clamping groove arranged on the back of the battery bin, so that the position of the cover plate is convenient to fix, and the top end of the storage battery is convenient to compress and fix through the compression spring and the compression plate; the temperature in the battery compartment can be conveniently detected through the arranged temperature controller, so that the heat dissipation fan is automatically controlled to work, and the heat in the battery compartment can be conveniently and quickly discharged; the supporting strip through setting up is convenient for play the supporting role to the battery to be convenient for discharge the heat that produces in the battery working process through the louvre of battery compartment bottom.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the cover plate of the present invention;
fig. 3 is a schematic side view of the battery compartment of the present invention;
fig. 4 is a schematic structural view of the clamping plate of the present invention;
FIG. 5 is a schematic structural view of the pull rod of the present invention;
fig. 6 is a schematic structural view of the clamping spring of the present invention;
fig. 7 is a schematic diagram of the back structure of the battery compartment of the present invention.
In the figure: 1. a battery compartment; 2. opening a hole; 3. a pull rod; 4. pulling a handle; 5. a threaded post; 6. a clamping plate; 7. a threaded hole; 8. air holes are formed; 9. a clamping spring; 10. an annular fixed plate; 11. a fixing hole; 12. a supporting strip; 13. a cover plate; 14. a fixed block; 15. a clamping block; 16. a temperature controller; 17. a card slot; 18. a compression spring; 19. a compression plate; 20. a heat dissipation fan.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-7, the utility model provides an unmanned aerial vehicle battery compartment reinforcing device, which comprises a battery compartment 1 and a cover plate 13, wherein the middle part of both sides of the battery compartment 1 is provided with an opening 2, the two openings 2 are respectively penetrated and connected with two pull rods 3, one end of each of the two pull rods 3 is fixedly provided with a clamping plate 6, the other end of each of the two pull rods 3 is fixedly provided with a pull handle 4, the surface of one end of each of the two pull rods 3 is sleeved with a clamping spring 9, the bottom end inside the battery compartment 1 is fixedly provided with a plurality of supporting bars 12, one side of the top end of the battery compartment 1 is hinged with one side of the cover plate 13 through a hinge, the other side of the cover plate 13 is hinged with one side of the bottom end of a fixed block 14 through a hinge, the bottom end of one side of the fixed block 14 is fixedly provided with a clamping block 15, the top part of the back surface of the battery compartment 1 is provided with, the both sides of battery compartment 1 all are fixed to be equipped with the heat dissipation fan 20 of establishing ties each other, and the middle part at the battery compartment 1 back is fixed and is equipped with temperature controller 16, and the inner wall at the battery compartment 1 back is arranged in to temperature controller 16's detection probe.
Preferably, the one end of two pull rods 3 is fixed and is equipped with screw thread post 5, and threaded hole 7 is seted up at the middle part of two clamp plates 6 one sides, and screw thread post 5 and threaded hole 7 threaded connection are convenient for install and dismantle.
Preferably, the two ends of the two clamping springs 9 are all fixedly provided with annular fixing plates 10, the fixing holes 11 are formed in the surfaces of the two annular fixing plates 10, one ends of the two annular fixing plates 10 are fixedly connected with one sides of the two clamping plates 6 through fixing bolts respectively, the other ends of the two annular fixing plates 10 are fixedly connected with the inner walls of the two sides of the battery bin 1 respectively, and the clamping springs 9 can be conveniently mounted and dismounted.
Preferably, a plurality of air holes 8 are formed in the surfaces of the two clamping plates 6, and a plurality of heat dissipation holes are formed in the bottom end of the battery compartment 1, so that the heat dissipation performance is improved, and the heat in the battery compartment 1 can be conveniently discharged.
Preferably, the heat dissipation fan 20 is electrically connected to the battery installed inside the battery compartment 1 through the temperature controller 16, and the temperature controller 16 is convenient for automatically controlling the operation of the heat dissipation fan 20, so as to dissipate heat.
Preferably, rubber cushions are fixedly arranged on the other sides of the two clamping plates 6 and the bottom ends of the pressing plates 19, and the rubber cushions protect the surface of the storage battery.
When the device is used in detail, the utility model relates to an unmanned aerial vehicle battery compartment reinforcing device, at first open apron 13, pull clamping plate 6 through pulling handle 4 and drive clamping spring 9 and contract, place the battery into battery compartment 1, support bar 12 plays the supporting role, loosen pulling handle 4, drive two clamping plates 6 under the effect of clamping spring 9 and press from both sides tight to the battery, close apron 13 and drive compression spring 18 and contract, thereby compress tightly the top of battery, block 15 through fixing block 14 one side setting is connected with the draw-in groove 17 block that the back of battery compartment 1 was seted up, thereby fix apron 13; the set type can be the temperature control range of the XMTG-7000 temperature controller 16, when the heat generated by the working of the storage battery is higher than the set value of the temperature controller 16, the temperature controller 16 automatically controls the heat dissipation fan 20 to work, and the heat generated by the working of the storage battery is discharged through the heat dissipation hole at the bottom end of the battery compartment 1.
In the description of the present invention, it should be understood that the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the indicated device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention.
In the present invention, unless otherwise explicitly specified or limited, for example, it may be fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle battery compartment reinforcing apparatus, includes battery compartment (1) and apron (13), its characterized in that, trompil (2) have all been seted up at the middle part of battery compartment (1) both sides, two trompil (2) alternate with two pull rods (3) respectively and are connected, two the equal fixed mounting in one end of pull rod (3) has clamp plate (6), two the other end of pull rod (3) is fixed to be equipped with draws handle (4), two the surface cover of pull rod (3) one end is equipped with clamping spring (9), the bottom mounting of battery compartment (1) inside is equipped with a plurality of support bar (12), one side of battery compartment (1) top is articulated with one side of apron (13) through the hinge, the opposite side of apron (13) is articulated with one side of fixed block (14) bottom through the hinge, the bottom mounting of fixed block (15) one side of fixed block (14), draw-in groove (17) corresponding with fixture block (15) position are seted up at the top at the battery compartment (1) back, fixture block (15) are connected with draw-in groove (17) block, the top fixed connection of a plurality of pressure spring (18) and pressure strip (19) is passed through to the bottom of apron (13), the both sides of battery compartment (1) are all fixed and are equipped with heat dissipation fan (20) of establishing ties each other, the middle part at the battery compartment (1) back is fixed and is equipped with temperature controller (16), the inner wall at the battery compartment (1) back is arranged in to the test probe of temperature controller (16).
2. The unmanned aerial vehicle battery compartment reinforcing apparatus of claim 1, characterized in that: one end of each pull rod (3) is fixedly provided with a threaded column (5), the middle part of one side of each clamping plate (6) is provided with a threaded hole (7), and the threaded columns (5) are in threaded connection with the threaded holes (7).
3. The unmanned aerial vehicle battery compartment reinforcing apparatus of claim 1, characterized in that: two the both ends of clamp spring (9) are all fixed and are equipped with annular fixed plate (10), two fixed orifices (11), two have all been seted up on the surface of annular fixed plate (10) the one end of annular fixed plate (10) all pass through fixing bolt respectively with one side fixed connection of two clamp plates (6), two the other end of annular fixed plate (10) respectively with the both sides inner wall fixed connection of battery compartment (1).
4. The unmanned aerial vehicle battery compartment reinforcing apparatus of claim 1, characterized in that: a plurality of air holes (8) are formed in the surfaces of the two clamping plates (6), and a plurality of heat dissipation holes are formed in the bottom end of the battery bin (1).
5. The unmanned aerial vehicle battery compartment reinforcing apparatus of claim 1, characterized in that: the heat dissipation fan (20) is electrically connected with a storage battery arranged inside the battery bin (1) through the temperature controller (16).
6. The unmanned aerial vehicle battery compartment reinforcing apparatus of claim 1, characterized in that: rubber cushions are fixedly arranged on the other sides of the two clamping plates (6) and the bottom ends of the pressing plates (19).
Priority Applications (1)
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CN201921194815.2U CN210349905U (en) | 2019-07-27 | 2019-07-27 | Unmanned aerial vehicle battery compartment reinforcing apparatus |
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CN201921194815.2U CN210349905U (en) | 2019-07-27 | 2019-07-27 | Unmanned aerial vehicle battery compartment reinforcing apparatus |
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CN210349905U true CN210349905U (en) | 2020-04-17 |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112357104A (en) * | 2021-01-14 | 2021-02-12 | 南京弘伍软件技术有限公司 | High-performance temperature sensor for unmanned aerial vehicle |
CN112864507A (en) * | 2020-12-09 | 2021-05-28 | 国网宁夏电力有限公司检修公司 | Unmanned aerial vehicle battery capacity increasing device |
CN113029205A (en) * | 2021-03-09 | 2021-06-25 | 长沙市日业电气有限公司 | Electromagnetic absolute value multi-ring encoder never losing position |
-
2019
- 2019-07-27 CN CN201921194815.2U patent/CN210349905U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112864507A (en) * | 2020-12-09 | 2021-05-28 | 国网宁夏电力有限公司检修公司 | Unmanned aerial vehicle battery capacity increasing device |
CN112357104A (en) * | 2021-01-14 | 2021-02-12 | 南京弘伍软件技术有限公司 | High-performance temperature sensor for unmanned aerial vehicle |
CN113029205A (en) * | 2021-03-09 | 2021-06-25 | 长沙市日业电气有限公司 | Electromagnetic absolute value multi-ring encoder never losing position |
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