CN208385470U - A kind of unmanned plane cell apparatus - Google Patents
A kind of unmanned plane cell apparatus Download PDFInfo
- Publication number
- CN208385470U CN208385470U CN201820332967.3U CN201820332967U CN208385470U CN 208385470 U CN208385470 U CN 208385470U CN 201820332967 U CN201820332967 U CN 201820332967U CN 208385470 U CN208385470 U CN 208385470U
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- Prior art keywords
- shell
- sliding
- sliding block
- unmanned plane
- cell apparatus
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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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- Battery Mounting, Suspending (AREA)
Abstract
The utility model relates to a kind of unmanned plane cell apparatus.Unmanned plane cell apparatus described in the utility model includes battery case, battery and the guide rail being mounted on unmanned aerial vehicle body, the battery case includes shell, first sliding block and male fastener, first sliding block and the male fastener are set in turn in the same side of the shell, the guide rail includes first sliding groove and mother buckle, one end of the first sliding groove is arranged in the mother buckle, first sliding block is connected by way of opposite sliding with the first sliding groove, the male fastener is connected by way of being mutually interlocked with the mother buckle, the battery is set in the cavity of the shell.Unmanned plane cell apparatus described in the utility model has the advantages that for unmanned machine battery to be mounted on unmanned aerial vehicle body accurate, firm and easy to disassemblely.
Description
Technical field
The utility model relates to unmanned plane fields, more particularly to a kind of unmanned plane cell apparatus.
Background technique
Unmanned plane is taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, is monitoring biography
Catch an illness, survey and draw, news report, electric inspection process, the disaster relief, the fields such as movies-making using very extensive, have a extensive future.Nothing
It is man-machine to be powered by battery to maintain flight operation, it is main because quality is big currently used for the high capacity cell on unmanned plane
If being fixed on unmanned plane by way of band and velcro binding, the on-off of aircraft is realized by plug connector again later
Electricity.
However, existing unmanned plane cell apparatus fixed form has the disadvantage in that
The position of each fixed battery be difficult it is unified, will result in so every time installation battery after aircraft center of gravity occur
Error；
There is aging with the time passage and the corrosion of external environment that use in velcro, is easily broken off, cannot will be electric
Pond is fixed on unmanned aerial vehicle body；
Battery need to consolidate when being mounted on unmanned aerial vehicle body, need to additionally increase a shell, structure is complicated, it has not been convenient to will be electric
Pond disassembles.
Utility model content
Based on this, the purpose of the utility model is to provide a kind of unmanned plane cell apparatus, have unmanned machine battery
Accurately, the advantage being mounted on firmly and easy to disassemble on unmanned aerial vehicle body.
A kind of unmanned plane cell apparatus, including battery case, battery and the guide rail being mounted on unmanned aerial vehicle body, the electricity
Pond shell includes shell, the first sliding block and male fastener, and first sliding block and the male fastener are set in turn in the shell
Side, the guide rail include first sliding groove and mother buckle, and the mother buckle is arranged in one end of the first sliding groove, and described first
Sliding block is connected by way of opposite sliding with the first sliding groove, and the male fastener and the mother buckle are by being mutually interlocked
Mode be connected, the battery is set in the cavity of the shell.
The unmanned plane cell apparatus of the utility model makes the battery case not using the fastening of male fastener and mother buckle
It can be detached from first sliding groove, constrain battery in the freedom degree of horizontal backward directions and left and right directions, accurately, surely by unmanned machine battery
Gu and easy to disassemble being mounted on unmanned aerial vehicle body.
Further, the first sliding groove cross section is L-type, and upper end is fixedly connected with unmanned aerial vehicle body, lower end support institute
The first sliding block is stated, meanwhile, first sliding block slides in the first sliding groove.
The first sliding block is stated in first sliding groove support residence, be ensure that the battery case will not fall, is constrained battery
In the freedom degree of vertical direction.
Further, the first sliding groove includes the guide portion with the first width and the sliding part with the second width,
First width is bigger than second width, guide portion to one transitional region of formation, transitional region between the sliding part
Width be gradually increased from first width to second width, first sliding block enters the cunning from the guide portion
Dynamic portion.
The transitional region formed between the guide portion and the sliding part increases the first sliding groove and the first sliding block
Contact area, facilitate the first sliding block of the battery case to slide into the first sliding groove.
Further, the first sliding groove further includes limiting section, and the limiting section is set to the mother buckle and described draws
It leads between portion, limiting section one end connection mother buckle, the other end to one transitional region of formation between the guide portion,
The width of transitional region is gradually increased.
The transitional region that the limiting section and the sliding part are formed, can prevent the battery case in first sliding groove
Continue slide, constrain battery in freedom degree horizontally forward.
Further, the shell includes first shell and second shell, and the first shell and the second shell can
Dismantling connection, first sliding block are set to the side of the first shell, and the male fastener is set to the second shell
Side.
After the first shell and second shell disassembly separation, the battery can be taken from the shell
Out, facilitate the disassembly of battery.
Further, the first shell is provided with several limited blocks, the second shell in the outer surface of aperture position
Body is provided with several limit holes in the inner surface of aperture position, and the first shell and the second shell pass through the limit
The mode that block and the limit hole match is detachably connected.
The first shell and second shell can be bonded by the mating connection of the limited block and limit hole, and
It is easily disassembled.
It further, further include second sliding slot and the second sliding block, the side of the second shell is arranged in the second sliding slot
Side, second sliding block, which is inlayed, to be mounted in the second sliding slot, and with the second sliding slot by way of opposite sliding phase
Connection, meanwhile, second sliding block connects the male fastener close to one end of second shell aperture position, and drives the pin thread
Part moves between the mother buckle and limiting section.
Second sliding block realizes fastening and the separation of male fastener and mother buckle by sliding, than the side for pressing male fastener
Formula is more laborsaving.
Further, the outer surface of second sliding block is zigzag.
Jagged second sliding block can increase the friction between hand and the second sliding block, only need to it is smaller push it is dynamic
Second sliding block can fasten the male fastener and the mother buckle or separation, saves physical strength.
Further, the guide rail further includes several mounting holes, and the mounting hole is set in the first sliding groove, institute
It states and is provided with screw in mounting hole, the guide rail is mounted on the unmanned aerial vehicle body by the screw.
The mounting hole guide rail-fixing and can will be removably mounted on the unmanned aerial vehicle body.
Further, the battery case is ABS engineering plastics shell, and the guide rail is aluminum alloy guide rail.
The battery case uses ABS engineering plastics, has the effect that using the elasticity of plastics, offsetting battery core is filling
Expansion when electric discharge；It waits when replacing battery and more quickly dismantles battery using flexible buckle；In mass production
When reduce production cost.
The guide rail uses the aluminium alloy of machine add-on type, can not only fix battery, additionally it is possible to increase stiffness of fuselage.
In order to better understand and implement, according to the present invention will be described in detail below with reference to the accompanying drawings.
Detailed description of the invention
Fig. 1 is the guide rail structure schematic diagram of the utility model；
Fig. 2 is the first shell structural schematic diagram of the utility model；
Fig. 3 is the second shell structural schematic diagram of the utility model；
Fig. 4 is the overall structure diagram of the utility model；
Fig. 5 is the overall structure top view of the utility model；
Fig. 6 is office's cross-sectional view of the first sliding block and first sliding groove in the utility model.
Specific embodiment
With reference to the accompanying drawings and examples, clear, complete description is carried out to the utility model.
Embodiment 1
In conjunction with attached drawing 1-5, the unmanned plane cell apparatus of the utility model includes battery 1, battery case 2 and guide rail 3.Battery
Shell 2 includes shell 21, the first sliding block 22 and male fastener 23.First sliding block 22 and male fastener 23 are set in turn in the same of shell 21
A side.Guide rail 3 is mounted on unmanned aerial vehicle body, and including first sliding groove 31 and mother buckle 32.Mother buckle 32 is arranged first
One end of sliding slot 31, the first sliding block 22 are connected by way of opposite sliding with first sliding groove 31, male fastener 23 and mother buckle
32 are connected by way of being mutually interlocked.Battery 1 is set in the cavity of shell 21.
Specifically, the cross section of first sliding groove 31 is L-type, and the upper end is fixedly connected with unmanned aerial vehicle body, lower end support the
One sliding block 22.
Specifically, shell 21 includes first shell 211 and second shell 212.First shell 211 and second shell 212 can
Dismantling connection, the first sliding block 22 are set to the side of first shell 211, and male fastener 23 is set to the side of second shell 212.
Specifically, first shell 211 is provided with several limited blocks 213 in the outer surface of aperture position, and second shell exists
The inner surface of aperture position is provided with several limit holes 214.First shell 211 and second shell 212 pass through 213 He of limited block
The mode that limit hole 214 matches is detachably connected.
Specifically, guide rail 3 further includes several mounting holes 33.Mounting hole 33 is set in first sliding groove 31, mounting hole 33
It is inside provided with screw, guide rail 3 is mounted on unmanned aerial vehicle body by screw.
Specifically, first sliding groove 31 successively includes limiting section 311, guide portion 312 and sliding part according to width from small to large
313.Limiting section 311 is set between mother buckle 32 and guide portion 312, and 311 one end of limiting section connects mother buckle 32, and the other end arrives
A transitional region is formed between guide portion 312, the width of transitional region is gradually increased.Guide portion 312 is between sliding part 313
A transitional region is formed, the width of transitional region is gradually increased, and the first sliding block 22 enters sliding part 313 from guide portion 312.
As shown in Fig. 6, specifically, first sliding groove 31 is set to the lower section of the first sliding block 22, and holds the first sliding block 22,
It ensure that battery case 2 will not fall, constrain battery 1 in the freedom degree of vertical direction.
In the present embodiment, battery case 2 is ABS engineering plastics shell, and guide rail 3 is aluminum alloy guide rail.
Battery case 2 uses ABS engineering plastic materials, has following technical effect that using the elasticity of plastics and offsets electricity
Expansion of the core in charge and discharge；It waits when replacing battery and more quickly dismantles battery using flexible buckle；In batch
Metaplasia reduces production cost when producing.
Guide rail 3 can not only fix battery, additionally it is possible to increase stiffness of fuselage using the aluminum alloy materials of machine add-on type.
The working principle and use process of the unmanned plane cell apparatus of the utility model described further below:
Firstly, the mounting screw in mounting hole 33, it is provided with screw hole on unmanned aerial vehicle body, screw is threadedly coupled with screw hole, will
Guide rail 3 is fixedly mounted on unmanned aerial vehicle body.Wherein, guide rail 3 can be removably mounted on unmanned aerial vehicle body by mounting hole 33,
Guide rail 3 is consolidated can will dismantle while being mounted on unmanned aerial vehicle body with 3 slave of guide rail.
Then, battery 1 is installed to 3 on guide rail.The workflow that battery 1 is installed to guide rail 3 is as follows:
Firstly, battery 1 is loaded into the cavity of first shell 2116, then by first shell 211 and second shell 212
By cooperating together for limited block 213 and limit hole 214, guarantee that battery is fixed in battery case 2.
Then, the beginning of the first sliding block 22 is promoted to the sliding part 213 of first sliding groove 31 along guide portion 312.When first
When sliding block 22 slides into the end of sliding part 213, wherein one side contacts male fastener 23 with mother buckle 32, and movable with mother buckle 32
It snaps connection.The width of guide portion 312 is bigger than limiting section 311, increases the contact area of first sliding groove 31 and the first sliding block 22,
The first sliding block 22 is facilitated to enter first sliding groove 31.
The connection of mother buckle 32 and male fastener 23 prevents battery case 2 from being detached from first sliding groove 31, battery 1 is constrained to exist
The freedom degree of horizontal backward directions.
When the first sliding block 22 has the tendency that moving forward because of external interference, limiting section 311 resists male fastener
23, it prevents male fastener 23 from moving on, so that the first sliding block 22 be prevented to continue to slide on sliding part 213, constrains battery 1
In freedom degree horizontally forward.
When needing to disassemble battery 1 from guide rail 3, male fastener 23 is pressed with hand, by male fastener 23 from mother buckle
It is withdrawn on 32, at this point, male fastener 23 and mother buckle 32 separate.Then, battery case is extracted from sliding part 313,
To realize the technical purpose for disassembling battery from unmanned aerial vehicle body.
Embodiment 2
As shown in Fig. 3, embodiment 2 and the difference of the embodiment 1 are, the unmanned plane cell apparatus also wraps
Include second sliding slot 215 and the second sliding block 216.Second sliding slot sets 215 sides that second shell 212 is arranged in, the second sliding block 216
It inlays and is mounted in second sliding slot 215, and be connected by way of opposite sliding with second sliding slot 215.Meanwhile second sliding block
216 connect male fastener 23 close to one end of second shell 212, and drive male fastener 23 between mother buckle 32 and limiting section 311
Movement.
Specifically, the outer surface of the second sliding block 216 is zigzag.Jagged second sliding block 216 can increase hand and
Friction between two sliding blocks 216, only need to it is smaller push the sliding of dynamic second sliding block 222 can be by male fastener 221 from mother buckle
It is disassembled on 32.
Embodiment 2 presses male fastener 23 with hand compared in embodiment 1, and male fastener 23 is withdrawn from mother buckle 32
Technical solution has the technical effect that battery case 2 is dismantled or installed from guide rail 3 more laborsavingly.
Above embodiments only express the several embodiments of the utility model, and the description thereof is more specific and detailed, but simultaneously
The limitation to utility model patent range therefore cannot be interpreted as.It should be pointed out that for the ordinary skill people of this field
For member, without departing from the concept of the premise utility, various modifications and improvements can be made, these belong to this reality
With novel protection scope.
Claims (10)
1. a kind of unmanned plane cell apparatus, which is characterized in that including battery case, battery and be mounted on leading on unmanned aerial vehicle body
Rail, the battery case include shell, the first sliding block and male fastener, and first sliding block and the male fastener are set in turn in institute
The side of shell is stated, the guide rail includes first sliding groove and mother buckle, and one end of the first sliding groove is arranged in the mother buckle,
First sliding block is connected by way of opposite sliding with the first sliding groove, and the male fastener and the mother buckle pass through
The mode being mutually interlocked is connected, and the battery is set in the cavity of the shell.
2. unmanned plane cell apparatus according to claim 1, which is characterized in that the first sliding groove cross section is L-type, on
End is fixedly connected with unmanned aerial vehicle body, the first sliding block described in the support of lower end, meanwhile, first sliding block is in the first sliding groove
Face sliding.
3. unmanned plane cell apparatus according to claim 2, which is characterized in that the first sliding groove includes wide with first
The guide portion of degree and sliding part with the second width, first width is bigger than second width, guide portion to the cunning
A transitional region is formed between dynamic portion, the width of transitional region is gradually increased from first width to second width,
First sliding block enters the sliding part from the guide portion.
4. unmanned plane cell apparatus according to claim 3, which is characterized in that the first sliding groove further includes limiting section,
The limiting section is set between the mother buckle and the guide portion, and described limiting section one end connects the mother buckle, another
One transitional region of formation, the width of transitional region between the guide portion is held to be gradually increased.
5. unmanned plane cell apparatus according to claim 4, which is characterized in that the shell includes first shell and second
Shell, the first shell and the second shell are detachably connected, and first sliding block is set to the side of the first shell
Side, the male fastener are set to the side of the second shell.
6. unmanned plane cell apparatus according to claim 5, which is characterized in that the first shell is in the outer of aperture position
Surface is provided with several limited blocks, and the second shell is provided with several limit holes in the inner surface of aperture position, described
First shell and the second shell are detachably connected in such a way that the limited block and the limit hole match.
7. unmanned plane cell apparatus according to claim 5, which is characterized in that it further include second sliding slot and the second sliding block,
The side of the second shell is arranged in the second sliding slot, and second sliding block, which is inlayed, to be mounted in the second sliding slot, and
It is connected by way of opposite sliding with the second sliding slot, meanwhile, second sliding block is close to second shell aperture position
One end connect the male fastener, and the male fastener is driven to move between the mother buckle and limiting section.
8. unmanned plane cell apparatus according to claim 7, which is characterized in that the outer surface of second sliding block is sawtooth
Shape.
9. unmanned plane cell apparatus according to claim 1, which is characterized in that the guide rail further includes several installations
Hole, the mounting hole are set in the first sliding groove, and screw is provided in the mounting hole, and the guide rail passes through the screw
It is mounted on the unmanned aerial vehicle body.
10. unmanned plane cell apparatus according to claim 1, which is characterized in that the battery case is ABS engineering plastics
Shell, the guide rail are aluminum alloy guide rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820332967.3U CN208385470U (en) | 2018-03-12 | 2018-03-12 | A kind of unmanned plane cell apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820332967.3U CN208385470U (en) | 2018-03-12 | 2018-03-12 | A kind of unmanned plane cell apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208385470U true CN208385470U (en) | 2019-01-15 |
Family
ID=64974301
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820332967.3U Active CN208385470U (en) | 2018-03-12 | 2018-03-12 | A kind of unmanned plane cell apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208385470U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113348587A (en) * | 2019-02-04 | 2021-09-03 | 曼·胡默尔有限公司 | Active material container, battery case, and method for mounting active material container in battery case |
-
2018
- 2018-03-12 CN CN201820332967.3U patent/CN208385470U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113348587A (en) * | 2019-02-04 | 2021-09-03 | 曼·胡默尔有限公司 | Active material container, battery case, and method for mounting active material container in battery case |
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