CN209200048U - A kind of direct insertion battery for unmanned plane - Google Patents
A kind of direct insertion battery for unmanned plane Download PDFInfo
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- CN209200048U CN209200048U CN201821940914.6U CN201821940914U CN209200048U CN 209200048 U CN209200048 U CN 209200048U CN 201821940914 U CN201821940914 U CN 201821940914U CN 209200048 U CN209200048 U CN 209200048U
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- main body
- unmanned plane
- battery
- battery main
- supply line
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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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Abstract
The utility model discloses a kind of direct insertion batteries for unmanned plane, including battery main body, described battery main body one end is connected with power supply line, the power supply line periphery is fitted with aluminium foil, mesh grid is equipped on the outside of the aluminium foil, the mesh grid periphery is coated with PVC crust, described power supply line one end is equipped with convex power connection, insulating strength plate is provided at the top of the battery main body, insulating strength plate one end is fixedly connected with charging plug, a kind of direct insertion battery for unmanned plane of the utility model, it is charged by power supply line to battery main body, mesh grid, aluminium foil and PVC crust ensure the intensity and toughness of power supply line, battery main body is directly connected with the charging connector inside unmanned plane using the charging plug of insulating strength plate one end, eliminate traditional connection, reduce battery weight bearing, charging plug and charging When mouth is correspondingly connected with, limit clamp is plugged in limit card slot, so that battery main body will not shake when installing.
Description
Technical field
The utility model relates to a kind of battery, in particular to a kind of direct insertion battery for unmanned plane belongs to unmanned plane
Equipment technical field.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.It is on ground, naval vessels or female
Machine remote control station personnel track it, are positioned, are remotely controlled, telemetering and Digital Transmission by the equipment such as radar, can be distant in radio
It takes off as conventional airplane under control or is launched with booster rocket, aerial launch can also be taken to by machine tool and flown.When recycling,
The mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block, it can be anti-
It is multiple to use repeatedly.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
Existing unmanned machine battery needs to be connected by route with aircraft, and the installation of route is there are certain consumption and to winged
Machine is taken certain weight bearing, and the joint of route is easy to fall off, and it is extremely inconvenient to use.Therefore we make this
It improves, proposes a kind of direct insertion battery for unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of direct insertion batteries for unmanned plane, to solve above-mentioned background technique
Traditional unmanned plane battery line weight bearing of middle proposition is big, and the problem of be easy to fall off at battery contact.
To achieve the above object, the utility model provides the following technical solutions: a kind of direct insertion battery for unmanned plane,
Including battery main body, described battery main body one end is connected with power supply line, and the power supply line periphery is fitted with aluminium foil, outside the aluminium foil
Side ring is equipped with mesh grid, and the mesh grid periphery is coated with PVC crust, and described power supply line one end is equipped with convex power connection,
It is provided with insulating strength plate at the top of the battery main body, insulating strength plate one end is fixedly connected with charging plug, described to fill
Plug side is equipped with limit clamp, and the limit clamp is connected with limit card slot, and the limit card slot is arranged in charging connector
One end, the charging connector are mounted on inside unmanned plane, and the charging connector other end is equipped with cable-through hole, the limit card slot side
It is connected with charging interface corresponding with charging plug.
As a kind of optimal technical scheme of the utility model, the battery main body avris is uniformly distributed heat release hole.
As a kind of optimal technical scheme of the utility model, the limit clamp and charging plug and insulating strength plate it
Between be an integral molding structure.
As a kind of optimal technical scheme of the utility model, the battery main body periphery is provided with insulation protection shell, institute
State insulation protection shell outer application corrosion-inhibiting coating.
As a kind of optimal technical scheme of the utility model, it is electrically connected between the charging connector and unmanned plane.
As a kind of optimal technical scheme of the utility model, the battery main body side is offered and convex power connection
Corresponding accommodating groove, described accommodating groove one end are connected with arc groove.
Compared with prior art, the utility model has the beneficial effects that a kind of straight cutting for unmanned plane of the utility model
Formula battery has route weight bearing small, and at battery contact the advantages of stable connection, specific in use, with traditional battery
In comparison, the utility model is charged by power supply line to battery main body, and mesh grid, aluminium foil and PVC crust ensure power supply
The intensity and toughness of line, will not fracture damage easily, battery main body using insulating strength plate one end charging plug directly with nothing
The charging connector of man-machine inside is connected, and eliminates traditional connection, reduces battery weight bearing, charging plug and charging interface pair
When should connect, limit clamp is plugged in limit card slot, so that battery main body will not shake when installing, stable connection uses effect
Fruit is good.
Detailed description of the invention
Fig. 1 is the utility model overall structure diagram；
Fig. 2 is the charging connector structural schematic diagram of the utility model；
Fig. 3 is the storage slot structure schematic diagram of the utility model.
In figure: 1, battery main body；2, insulation protection shell；3, power supply line；4, mesh grid；5, aluminium foil；6, convex power connection；
7, PVC crust；8, insulating strength plate；9, clamp is limited；10, charging plug；11, cable-through hole；12, charging connector；13, charging
Mouthful；14, limit card slot；15, accommodating groove；16, arc groove；17, heat release hole.
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of direct insertion battery for unmanned plane, including battery main body 1,
Described 1 one end of battery main body is connected with power supply line 3, and 3 periphery of power supply line is fitted with aluminium foil 5, is equipped on the outside of the aluminium foil 5
Mesh grid 4,4 periphery of mesh grid are coated with PVC crust 7, and described 3 one end of power supply line is equipped with convex power connection 6, described
Insulating strength plate 8 is provided at the top of battery main body 1, described 8 one end of insulating strength plate is fixedly connected with charging plug 10, described to fill
10 side of plug is equipped with limit clamp 9, and the limit clamp 9 is connected with limit card slot 14, and the setting of limit card slot 14 exists
12 one end of charging connector, the charging connector 12 are mounted on inside unmanned plane, and 12 other end of charging connector is equipped with cable-through hole 11,
14 side of limit card slot is connected with charging interface 13 corresponding with charging plug 10.
Preferably, 1 avris of battery main body is uniformly distributed heat release hole 17, the localized hyperthermia generated when battery being avoided to work
Battery itself is damaged.
Preferably, it is an integral molding structure, is convenient between the limit clamp 9 and charging plug 10 and insulating strength plate 8
Battery main body 1 is connected directly with charging connector 12 in unmanned plane.
Preferably, 1 periphery of battery main body is provided with insulation protection shell 2, the 2 outer application anti-corrosion of insulation protection shell
Coating, highly-safe, long service life.
Preferably, it is electrically connected between the charging connector 12 and unmanned plane, convenient for being powered by battery to body.
Preferably, 1 side of battery main body offers accommodating groove 15 corresponding with convex power connection 6, the storage
15 one end of slot is connected with arc groove 16, the convenient convex power connection 6 fixed when battery does not charge of accommodating groove 15, arc groove
16 stir pick-and-place to convex power connection 6 in accommodating groove 15 convenient for finger.
When specifically used, a kind of direct insertion battery for unmanned plane of the utility model has route weight bearing small, and battery
The advantages of joint stable connection, is charged by power supply line 3 to battery main body 1, and mesh grid 4, aluminium foil 5 and PVC crust 7 ensure
The intensity and toughness of power supply line 3, will not fracture damage easily, convex power connection 6 is connected to storage after battery is fully charged
In slot 15, battery main body 1 using 8 one end of insulating strength plate charging plug 10 directly with 12 phase of charging connector inside unmanned plane
Even, traditional connection is eliminated, battery weight bearing, when charging plug 10 and charging interface 13 are correspondingly connected with, limiting card are reduced
First 9 are plugged in limit card slot 14, so that battery main body 1 will not shake when installing, stable connection is worth being widely popularized.
In the description of the present invention, it should be understood that term " coaxial ", " bottom ", " one end ", " top ", " in
The orientation of the instructions such as portion ", " other end ", "upper", " side ", " top ", "inner", " front ", " center ", " both ends " or position are closed
System is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description, rather than
The device or element of indication or suggestion meaning must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot
It is construed as a limitation of the present invention.
In addition, term " first ", " second ", " third ", " the 4th " are used for description purposes only, and should not be understood as instruction or
It implies relative importance or implicitly indicates the quantity of indicated technical characteristic, define " first ", " second ", " the as a result,
Three ", the feature of " the 4th " can explicitly or implicitly include at least one of the features.
In the present invention unless specifically defined or limited otherwise, term " installation ", " setting ", " connection ", " Gu
Calmly ", the terms such as " being screwed on " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integral；
It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, can also indirectly connected through an intermediary, it can be with
It is the interaction relationship of the connection or two elements inside two elements, unless otherwise restricted clearly, for this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of direct insertion battery for unmanned plane, including battery main body (1), which is characterized in that the battery main body (1) one
End is connected with power supply line (3), and power supply line (3) periphery is fitted with aluminium foil (5), is equipped with mesh grid on the outside of the aluminium foil (5)
(4), mesh grid (4) periphery is coated with PVC crust (7), and described power supply line (3) one end is equipped with convex power connection (6),
It is provided with insulating strength plate (8) at the top of the battery main body (1), described insulating strength plate (8) one end is fixedly connected with charging and inserts
Head (10), charging plug (10) side are equipped with limit clamp (9), and the limit clamp (9) is connected with limit card slot (14),
The limit card slot (14) is arranged in charging connector (12) one end, and the charging connector (12) is mounted on inside unmanned plane, and fills
Electric connection (12) other end is equipped with cable-through hole (11), and limit card slot (14) side is connected with corresponding with charging plug (10)
Charging interface (13).
2. a kind of direct insertion battery for unmanned plane according to claim 1, it is characterised in that: the battery main body
(1) avris is uniformly distributed heat release hole (17).
3. a kind of direct insertion battery for unmanned plane according to claim 1, it is characterised in that: the limit clamp
(9) it is an integral molding structure between charging plug (10) and insulating strength plate (8).
4. a kind of direct insertion battery for unmanned plane according to claim 1, it is characterised in that: the battery main body
(1) periphery is provided with insulation protection shell (2), insulation protection shell (2) the outer application corrosion-inhibiting coating.
5. a kind of direct insertion battery for unmanned plane according to claim 1, it is characterised in that: the charging connector
(12) it is electrically connected between unmanned plane.
6. a kind of direct insertion battery for unmanned plane according to claim 1, it is characterised in that: the battery main body
(1) side offers accommodating groove (15) corresponding with convex power connection (6), and it is recessed that described accommodating groove (15) one end is connected with arc
Slot (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821940914.6U CN209200048U (en) | 2018-11-23 | 2018-11-23 | A kind of direct insertion battery for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821940914.6U CN209200048U (en) | 2018-11-23 | 2018-11-23 | A kind of direct insertion battery for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209200048U true CN209200048U (en) | 2019-08-02 |
Family
ID=67425690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821940914.6U Active CN209200048U (en) | 2018-11-23 | 2018-11-23 | A kind of direct insertion battery for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209200048U (en) |
-
2018
- 2018-11-23 CN CN201821940914.6U patent/CN209200048U/en active Active
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