CN209581910U - A kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device - Google Patents
A kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device Download PDFInfo
- Publication number
- CN209581910U CN209581910U CN201822167932.1U CN201822167932U CN209581910U CN 209581910 U CN209581910 U CN 209581910U CN 201822167932 U CN201822167932 U CN 201822167932U CN 209581910 U CN209581910 U CN 209581910U
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- Prior art keywords
- block
- battery
- limited block
- quick
- detach
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Links
- 230000001681 protective effect Effects 0.000 title claims abstract description 10
- 239000011521 glass Substances 0.000 claims abstract description 12
- 238000012216 screening Methods 0.000 claims abstract description 12
- 239000003822 epoxy resin Substances 0.000 claims description 4
- 239000003292 glue Substances 0.000 claims description 4
- 229920000647 polyepoxide Polymers 0.000 claims description 4
- 230000006378 damage Effects 0.000 abstract description 4
- 238000004880 explosion Methods 0.000 abstract description 4
- 208000027418 Wounds and injury Diseases 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 230000004224 protection Effects 0.000 description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 3
- 229910052744 lithium Inorganic materials 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective devices, including screening glass is arranged, fixed plate, left fixed block and right fixed block, the left fixed block is equipped with Quick-disassembling mechanism, the Quick-disassembling mechanism includes limited block, shifting block, guide rod and reset spring, the limited block is slidably disposed in the groove on left fixed block, the shifting block is arranged above limited block, the guide rod is arranged on the inside of limited block and is slidably disposed in the slideway of recess sidewall, the reset spring is set on guide rod, and both ends are connect with limited block and recess sidewall respectively.The fast assembling-disassembling that battery is realized by Quick-disassembling mechanism, improves work efficiency；And battery firmly installs, and is not in the phenomenon that battery loosens, improves the safety of unmanned plane；Battery is protected by screening glass, reduces a possibility that battery is by explosion on fire is hit, and then reduce economic loss and injury to personnel problem.
Description
Technical field
The utility model relates to unmanned plane spare and accessory parts technical field, in particular to a kind of multi-rotor unmanned aerial vehicle battery is quickly torn open
It unloads and protective device.
Background technique
Currently, multi-rotor unmanned aerial vehicle battery mostly uses one piece or two pieces common lithium battery as power supply, magic is then used
Patch is banded on unmanned aerial vehicle rack plate.But due to velcro to tie up effect bad, loosening is easy to produce, especially at nobody
When machine unstable flight or aircraft bombing, battery is easy to fall off.Since common lithium battery appearance is without special safeguard procedures, lithium battery holds
It is subject to be impacted and damage, it is on fire to may cause battery explosion when serious, generates serious economic loss and threateningly dough figurine
The safety of member.
Utility model content
In order to solve the above technical problems, the utility model discloses a kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protections
Device, including the screening glass of four sides of battery, the fixed plate being arranged on two sides of battery is arranged in and respectively with two
The left fixed block and right fixed block of a fixed plate connection, the left fixed block are equipped with Quick-disassembling mechanism, and the Quick-disassembling mechanism includes
Limited block, shifting block, guide rod and reset spring, the limited block is slidably disposed in the groove on left fixed block, described
Shifting block is arranged above limited block, and the slideway on the inside of limited block and being slidably disposed on recess sidewall is arranged in the guide rod
Interior, the reset spring is set on guide rod, and both ends are connect with limited block and recess sidewall respectively.
As a further improvement of the above technical scheme, intilted first wedge surface is equipped on the outside of the limited block.
As a further improvement of the above technical scheme, intilted second wedge surface is equipped on the outside of the right fixed block.
As a further improvement of the above technical scheme, the screening glass is the strip structure that cross sectional shape is rectangular in shape.
As a further improvement of the above technical scheme, the screening glass and fixed plate pass through epoxide-resin glue and battery
It is fixedly connected.
The beneficial effects of the utility model are:
1, the fast assembling-disassembling that battery is realized by Quick-disassembling mechanism, improves work efficiency；And battery firmly installs, no
It will appear the phenomenon that battery loosens, increase the stability of unmanned plane, reduce the generation of unstable phenomenon, improve the peace of unmanned plane
Quan Xing；
2, battery is protected by screening glass, reduces a possibility that battery is by explosion on fire is hit, and then subtract
Few economic loss and injury to personnel problem.
Detailed description of the invention
In order to illustrate more clearly of the technical scheme in the embodiment of the utility model, will make below to required in embodiment
Attached drawing is briefly described, it should be apparent that, the drawings in the following description are merely some embodiments of the present invention,
For those of ordinary skill in the art, without any creative labor, it can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the overlooking structure diagram of the utility model；
Fig. 3 is the partial enlarged view in Fig. 1 at A.
Appended drawing reference:
1- screening glass；2- fixed plate；The left fixed block of 3-；31- groove；32- slideway；The right fixed block of 4-；The second wedge surface of 41-；
5- Quick-disassembling mechanism；51- limited block；52- shifting block；53- guide rod；54- reset spring；The first wedge surface of 55-；6- battery；7- left frame
Plate；71- card slot；The right frame plate of 8-.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
It is to be appreciated that the directional instruction (such as up, down, left, right, before and after ...) of institute in the utility model embodiment
It is only used for explaining in relative positional relationship, the motion conditions etc. under a certain particular pose (as shown in the picture) between each component, such as
When the fruit particular pose changes, then directionality instruction also correspondingly changes correspondingly.
In addition, the description for being related to " first ", " second " etc. in the present invention is used for description purposes only, and cannot understand
For its relative importance of indication or suggestion or implicitly indicate the quantity of indicated technical characteristic.Define as a result, " first ",
The feature of " second " can explicitly or implicitly include at least one of the features.
As shown in Figs. 1-2, the fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device of the present embodiment, including be arranged in electricity
It the screening glass 1 of 6 four sides in pond, the fixed plate 2 being arranged on 6 two sides of battery and is connect respectively with two fixed plates 2
Left fixed block 3 and right fixed block 4, left fixed block 3 be equipped with Quick-disassembling mechanism 5.
Screening glass 1 and fixed plate 2 are bonded on battery 6 by epoxide-resin glue, and epoxide-resin glue has good stripping
From intensity, impact strength and weatherability, resistance to ag(e)ing, it can guarantee the bonding strength of screening glass 1 and fixed plate 2, it will not be light
Easily fall off.
Screening glass 1 is the strip structure that cross sectional shape is rectangular in shape, and can just be matched with four sides of battery 6.It is logical
Overprotection piece 1 carries out effective protection to battery 6, reduces a possibility that battery 6 is by explosion on fire is hit, and then reduces economical
Loss and injury to personnel problem.
Left fixed block 3 and right fixed block 4 are connect by bolt with fixed plate 2 respectively.
As shown in figure 3, Quick-disassembling mechanism 5 includes limited block 51, shifting block 52, guide rod 53 and reset spring 54；Limited block 51
It is slidably disposed in the groove 31 on left fixed block 3, shifting block 52 is arranged above limited block 51, and the setting of guide rod 53 is limiting
51 inside of block, and be slidably disposed in the slideway 32 of 31 side wall of groove；Reset spring 54 is set on guide rod 53, and
Both ends are connect with the side wall of limited block 51 and groove 31 respectively；Intilted first wedge surface 55 is equipped on the outside of limited block 51, it is right
Intilted second wedge surface 41 is equipped on the outside of fixed block 4.
When installation, the second wedge surface 41 of the first wedge surface 55 of limited block 51 and right fixed block 4 respectively with the left machine of unmanned plane
Frame plate 7 and right frame plate 8 contact.With the insertion of battery, the continuous compression reseting spring 54 of limited block 51 finally makes limited block 51
Into in the card slot 71 of left frame plate 7, the position locking of battery 6 is realized.
When disassembly, shifting block 52 is stirred inwardly with hand, separate limited block 51 with card slot 71, then to above mentioning battery 6
Out.
The fast assembling-disassembling that battery 6 is realized by Quick-disassembling mechanism 5, improves work efficiency；And battery 6 firmly installs,
Be not in the phenomenon that battery 6 loosens, increase the stability of unmanned plane, reduce the generation of unstable phenomenon, improve unmanned plane
Safety.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.It in addition, the technical solution between each embodiment can be combined with each other, but must be general with this field
Based on logical technical staff can be realized；It will be understood that when the combination of technical solution appearance is conflicting or cannot achieve this
The combination of technical solution is not present, also not within the protection scope of the requires of the utility model.
Claims (5)
1. a kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device, it is characterised in that: including being arranged in four sides of battery
The screening glass on side, the fixed plate being arranged on two sides of battery and the left fixed block being connect respectively with two fixed plates and the right side
Fixed block, the left fixed block are equipped with Quick-disassembling mechanism, and the Quick-disassembling mechanism includes limited block, shifting block, guide rod and resets bullet
Spring, the limited block are slidably disposed in the groove on left fixed block, and the shifting block is arranged above limited block, described to lead
Bar is arranged on the inside of limited block and is slidably disposed in the slideway of recess sidewall, and the reset spring is set on guide rod,
And both ends are connect with limited block and recess sidewall respectively.
2. the fast quick-detach of multi-rotor unmanned aerial vehicle battery according to claim 1 and protective device, it is characterised in that: the limit
Intilted first wedge surface is equipped on the outside of the block of position.
3. the fast quick-detach of multi-rotor unmanned aerial vehicle battery according to claim 2 and protective device, it is characterised in that: the right side
Intilted second wedge surface is equipped on the outside of fixed block.
4. the fast quick-detach of multi-rotor unmanned aerial vehicle battery according to claim 1 and protective device, it is characterised in that: the guarantor
Bluff piece is the strip structure that cross sectional shape is rectangular in shape.
5. the fast quick-detach of multi-rotor unmanned aerial vehicle battery according to claim 1 and protective device, it is characterised in that: the guarantor
Bluff piece and fixed plate pass through epoxide-resin glue and are fixedly connected with battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822167932.1U CN209581910U (en) | 2018-12-21 | 2018-12-21 | A kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822167932.1U CN209581910U (en) | 2018-12-21 | 2018-12-21 | A kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209581910U true CN209581910U (en) | 2019-11-05 |
Family
ID=68378423
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822167932.1U Active CN209581910U (en) | 2018-12-21 | 2018-12-21 | A kind of fast quick-detach of multi-rotor unmanned aerial vehicle battery and protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209581910U (en) |
-
2018
- 2018-12-21 CN CN201822167932.1U patent/CN209581910U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |