CN207233839U - Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery - Google Patents
Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery Download PDFInfo
- Publication number
- CN207233839U CN207233839U CN201721347369.5U CN201721347369U CN207233839U CN 207233839 U CN207233839 U CN 207233839U CN 201721347369 U CN201721347369 U CN 201721347369U CN 207233839 U CN207233839 U CN 207233839U
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- China
- Prior art keywords
- battery
- shell
- aerial vehicle
- unmanned aerial
- quick release
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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 discloses a kind of unmanned aerial vehicle onboard integral and intelligent Quick Release power battery, include the shell of inner cavity installation battery, several introducing mechanisms for being used to be matched with battery mounting base are provided with the side wall of the shell, is realized by introducing mechanism and is moved along battery mounting base or fixed with battery mounting base.The utility model is using integrated integral installation, it is fixed conveniently, and can quickly be assembled and disassembled, and improves efficiency, and this structure is to be used first on unmanned plane fixed structure；By setting limit switch, the protection to operating personnel is realized；The management to battery status and feedback are realized, realizes automatic alarm, consequently facilitating accurate judgement of the operating personnel to battery status；By communicating in time, the output of data is realized, especially for aircraft, ground handling operator can accurately grasp battery status in real time, and then more rational planning uses.
Description
Technical field
It the utility model is related to a kind of unmanned machine battery, and in particular to a kind of unmanned aerial vehicle onboard integral and intelligent Quick Release power
Battery.
Background technology
With the increasingly maturation, and the popularization of modern agriculture theory of unmanned air vehicle technique so that unmanned plane is in modern agriculture
Substantial amounts of popularization has been obtained in production, such as：Pesticide spraying, fertilising, crop pollination etc. are carried out using unmanned plane.With traditional work
Mode is compared, and drastically increases operating efficiency.However, in the UAV system used now, power battery is used as nobody
One of core component of machine system, but there is many deficiencies, there is many improved directions of needs.
First, the simple battery pack that most of agricultural unmanned plane all uses adds the power scheme being mechanically fixed, Ji Jiang electricity
After core simply packaging, it is connected by straight cutting plug with unmanned plane, the battery core simply packed is by mechanical method, such as bolt, card
The fixing piece such as button or binding strap is fixed, or even some unmanned planes directly load naked battery core to get up to use, more than
Scheme, battery fix/detaching structure complexity, not only expend time and manpower, but also during careless manipulation, easily battery core is caused to damage
Wound, causes to leak electricity, or even jeopardize the safety of operating personnel；
Secondly, the battery core that most of agricultural unmanned plane uses does not have battery-mounted management system, can not be to the state of battery
Fed back in real time, also battery can not be managed and be protected in battery charging process, it is even more impossible to make on unmanned plane
Used time, earthward sends battery status information in real time, so that, when in use, battery is in black box state, can only be by external
Formula equipment or the experience of operating personnel judge battery status, this is very unreasonable even dangerous.There is part to have
The battery of battery management system, also simply simple battery capacity is shown or the service life shows, does not detect battery real-time status
Function；
Finally, battery core belongs to high-risk component, it is necessary to could be worked normally under suitable use condition, therefore, battery must
Must can in time, reasonably protect itself, but existing product can accomplish the fewer and fewer of this function.
Utility model content
Technical problem to be solved in the utility model is that existing battery and unmanned plane fixed structure are complicated, time and effort consuming,
Easily electric leakage, its purpose is to provide a kind of unmanned aerial vehicle onboard integral and intelligent Quick Release power battery, which realizes integration
Integral installation, it is fixed conveniently, and can quickly be assembled and disassembled, improve efficiency.
The utility model is achieved through the following technical solutions：
Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery, includes the shell of inner cavity installation battery, the shell
Several introducing mechanisms for being used to be matched with battery mounting base are provided with side wall, are realized by introducing mechanism along battery
Mounting base is mobile or is fixed with battery mounting base.Current unmanned machine battery is fixed using mechanical, it dismounts not side
Just, for carrying out agricultural operation as the unmanned plane of power supply using lithium battery, it is most commonly seen and frequent to replace battery
Operation, but existing machinery formula fixed form, such as bolt, buckle or binding mode are all extremely inconvenient, it is fixed too tightly or too
Problem all easily occurs for pine, it is fixed can tightly cause very much battery into and out difficulty, it is fixed too loose and connection can be caused to loosen,
Trigger vibration, even result in battery packages fracture failure.Unmanned machine battery current at the same time is all simply to pack, not dust-proof anti-
Water, easily cause danger, and agricultural plant protection unmanned plane will adapt to severe working environment, harsh operating condition, while to ensure
Each component has higher stability, durability and anti-interference.But most battery has all simply carried out letter to battery core
Single packing, or even naked battery core is directly used, once dust and liquid intrusion inside battery, are very easy to cause battery corrosion, leakage
Situations such as electric, damage user.And this programme is then to use integral battery, battery is used into integrated design, is used
The full packaging type structure of shell, by structures such as all circuit components, control chip group, battery core, plugs all by aluminium alloy outside
Shell+carbon fiber board+elastic cotton liner parcel, can shatter-resistant, waterproof and dustproof；Its fixed form is then to use several introducing mechanisms
Realized by introducing mechanism and move along battery mounting base or fixed with battery mounting base, the quantity of introducing mechanism is according to reality
Demand is set, and this structure has extremely strong importing property and adaptivity certainly, and it is accurate when battery quickly loads to meet at the same time
Positioning and the convenient requirement quickly split out.
Actually introducing mechanism is bead introducing mechanism, and this mechanism is oriented to by the scrolling realization of bead, is similar to
Bearing ball can carry out 360 ° and rotate the same, be not easy clamping stagnation, and at this time whether battery wall is that inclined-plane is all inessential, can only can
Guide battery to be inserted into fixed seat realization by bead introducing mechanism to be oriented to and fix, prove by actual use, bead is led
When to enter mechanism be preferably wedge-shaped bead introducing mechanism, play the role of positioning, fixation, from importing etc. using wedge-shaped bead introducing mechanism
Most preferably, when being inserted into battery, it is only necessary to rough alignment direction, by battery quick set-down, or even directly lets go on reasonable altitudes,
Battery can slip into mounting structure automatically under the effect of gravity, while complete to position, easy to operate and quick, and when extraction directly promotes
, it is not necessary to any extra operation.
In order to increase the stability of structure and be easily installed, frame, frame roof protrusion are also provided with below shell
Some framework pillars are formed, shell is arranged in the region of framework pillar formation, and shell wall is pasted with framework branch column wall
Closing, wedge-shaped bead introducing mechanism is installed on corresponding framework branch column outer wall, can realize that multiple spot imports at the same time when so importing,
Battery held stationary falls, and base of frame is provided with shock callus, impact during slowing down insertion.
The top surface of shell is also provided with upper cover, and upper cover is fixed with shell, battery is arranged on upper cover and shell is formed
Seal cavity in, quick plug and handle are provided with upper lid, and quick plug is connected with battery.Handle is easy for operating
Personnel with portable battery, hold with a firm grip place by when insertion.
Existing battery is that power connector is directly drawn inside battery core, powered always, direct with unmanned plane load
During connection, plug can be triggered to strike sparks, plant protection unmanned plane needs frequently to replace battery in addition, adds the possibility of sparking in turn
Property, risk factor is high.And the quick plug of this programme includes quick plug shell, quick plug shell is fixed with upper cover, quick to insert
Accessory power outlet and limit switch are provided with head shell, and limit switch is arranged on below accessory power outlet, accessory power outlet and spacing
Switch is connected through upper cover with battery.It reliably can easily reflect whether battery is normal by the limit switch of setting
Access, is not accessed normally such as, and battery can send alarm and reminding automatically, while according to different access devices, such as aircraft or
Charger etc., carries out subsequent operation automatically, moreover, can also so avoid battery plug powered always, during access device
The situation of sparking.
According to relevant regulations and requirement, the charging and discharging of battery must be in rational scope, and it is tight to overcharge and cross and put
What lattice were forbidden, the use and service life that both of these case all can be to battery have a huge impact, but general battery does not all have
Corresponding management module, can not carry out discharge and recharge self-management.Only have simple light prompt, display on most of battery products
The information about power of battery, and can not be under all use states of battery, there is provided the status information prompting of battery, it is even more impossible in electricity
During the abnormal state of pond, there is provided warning, is carried out at the same time self-protection.Most of batteries can not all be communicated with load or charger,
When completion status exports or the function of command reception, especially unmanned plane carry battery operation, ground staff can not learn electricity
The use state in pond.The problem of many due to more than, constrain the operating efficiency of agricultural plant protection unmanned plane.And this programme be then
Battery management module is provided with upper cover, and battery management module is connected with battery, accessory power outlet and limit switch at the same time, on
Cover the control panel for being provided with and being connected with battery management module, cell switch is provided with control panel, LED lamplight is shown and
Buzzer, is provided with communication module in battery management module, is connected by battery delivery outlet with the external world.Wherein battery management mould
Block, control panel and communication module are all existing components, it can directly buy on the market, and this programme utilizes battery management
Module realizes the functions such as management of charging and discharging, battery status detection, battery status feedback and alarm, and during electric discharge, battery can be shown in real time
Show current state and electricity, when there is abnormality, if battery core overtension, temperature be not in section allowable or monolithic battery core voltage
Imbalance when situations such as occur when, can automatic alarm and according to different access devices, make corresponding reaction, low battery is protected
Shield is one kind the most basic in all functions；During charging, battery can display real-time current state and electricity, while lasting inspection
Oneself state is surveyed, when there is abnormality, such as charging current is excessive, voltage is excessive, battery core temperature is not the section allowable situations such as
During appearance, battery can stop charging immediately, protect itself, be simultaneously emitted by alarm, and over-charging of battery protection is also in all functions
The most basic one kind；Battery can continue detection oneself state using in overall process, while provide condition prompting, when having
After abnormality produces, it can act and alarm immediately.In the present solution, battery-mounting data communication system, passes through same height
Reliability plug completes the electricity output and data output of battery, and when in use, battery can export its data in real time, no longer be
One black box, especially for aircraft, ground handling operator can accurately grasp battery status in real time, and then more reasonable
Planning use.
The utility model compared with prior art, has the following advantages and advantages：
1st, using integrated integral installation, it is fixed conveniently the utility model, can quickly be assembled and disassembled, and improves effect
Rate, this structure are to be used first on unmanned plane fixed structure；
2nd, the utility model realizes the protection to operating personnel by setting limit switch；
3rd, the utility model realizes the management to battery status and feedback, realizes automatic alarm, consequently facilitating operator
Accurate judgement of the member to battery status；
4th, the utility model realizes the output of data, especially for aircraft, ground handling operator by communicating in time
Battery status can be accurately grasped in real time, and then more rational planning uses.
Brief description of the drawings
Attached drawing described herein is used for providing further understanding the utility model embodiment, forms the one of the application
Part, does not form the restriction to the utility model embodiment.In the accompanying drawings：
Fig. 1 is the utility model structure diagram；
Fig. 2 is the structure diagram inside quick plug；
Fig. 3 is the schematic diagram of the arrangement one of bead introducing mechanism；
Fig. 4 is the schematic diagram of the arrangement two of bead introducing mechanism；
Fig. 5 is the schematic diagram of the arrangement three of bead introducing mechanism；
Fig. 6 is the schematic diagram of the arrangement four of bead introducing mechanism；
Fig. 7 is the schematic diagram of the arrangement five of bead introducing mechanism；
Fig. 8 is the schematic diagram of the arrangement six of bead introducing mechanism.
Mark and corresponding parts title in attached drawing：
1- handles, 2- upper covers, 3- wedge shape bead introducing mechanisms, 4- framework pillars, 5- shock callus, 6- shells, 7- are quick
Plug, 8- control panels, 9- accessory power outlets, 10- limit switches.
Embodiment
For the purpose of this utility model, technical solution and advantage is more clearly understood, with reference to embodiment and attached drawing,
The utility model is described in further detail, and the exemplary embodiment and its explanation of the utility model are only used for explaining this
Utility model, is not intended to limit the scope of the present invention.
Embodiment 1：
As shown in Figure 1, unmanned aerial vehicle onboard integral and intelligent Quick Release power battery, including shell 6, the inner cavity installation of shell 6
The structures such as battery, circuit components, control chip group, plug, it uses full packaging type structure, and shell 6 is by carbon fiber board system
Into in conjunction with elastic cotton liner parcel, energy shatter-resistant, waterproof and dustproof, in order to increase the fastness of structure, set below shell 6
Frame made of aluminium alloy is equipped with, frame roof is protruded to form framework pillar 4 made of some aluminium alloys, and shell 6 is arranged on
In the region that framework pillar 4 is formed, and 6 wall of shell is bonded with 4 inner wall of framework pillar, and bead introducing mechanism is installed on corresponding
On 4 outer wall of framework pillar, base of frame is provided with shock callus 5, and mounting base inner cavity surface is vertical plane at this time, bead introducing mechanism
Mounting surface be also plane, i.e., the lateral wall of framework pillar 4 is vertical plane, and bead introducing mechanism moves along vertical plane and arrives peace
Fixed after filling seat setting position, realize rapid-assembling/disassembling.
Embodiment 2：
As shown in Figure 1, the present embodiment and the structure of embodiment 1 are essentially identical, difference is：Mounting base inner cavity surface is
Inclined-plane, introducing mechanism are wedge-shaped bead introducing mechanism 3, and matching is set using wedge-shaped bead introducing mechanism 3 and in unmanned plane one end
Bead seat, play the role of positioning, fixation, from import, adapt to installation position and damping etc., avoid traditional connection structure, such as
The use of bolt and bandage etc..User is when being inserted into battery, it is only necessary to rough alignment direction, by battery quick set-down, even
Directly let go on reasonable altitudes, battery can slip into mounting structure automatically under the effect of gravity, while complete to position, easy to operate
And it is quick, directly promote during extraction, it is not necessary to any extra operation.
Embodiment 3：
As shown in Fig. 2, on the basis of above-described embodiment, upper cover 2 and shell 6 are screwed, battery and its
In the seal cavity that its electrical part is arranged on upper cover 2 and shell 6 is formed, quick plug 7 and handle 1, handle are provided with upper cover 2
1, which is easy for operating personnel, holds and takes, and quick plug 7 includes quick plug shell 11, and quick plug shell 11 is fixed with upper cover 2, soon
Accessory power outlet 9 and limit switch 10 are provided with fast plug body 11, and limit switch 10 is arranged on the lower section of accessory power outlet 9, it is defeated
Go out socket 9 and limit switch 10 is connected through upper cover 2 with battery.By increasing limit switch 10, limit at quick plug 7
Bit switch 10 is a flexible member, it disappears automatic when being squeezed to inside battery retraction and cell communication, extruding force
Rebound departs from the connection with battery, and when normally insertion equipment, the protrusion on relevant device can physical trigger limit switch
10, at this time could normally-open battery, realize powered operation, otherwise battery not supplying power for outside, so avoids to plug
Sparking, moreover, when battery is by improper operation, situations such as extracted by force during supplying power for outside, limit switch 10 is automatic
Pop-up forms power-off, and battery can be detected by the break-make of limit switch immediately, so that automatic alarm and subsequent operation is carried out,
Operating personnel are protected, prevent from getting an electric shock.
Embodiment 4：
As shown in Fig. 2, on the basis of above-described embodiment, the intelligentized control method to battery is realized, realize to battery shape
The management of state and feedback, realize automatic alarm, and communication, realizes the output of data in time.So it is provided with cell tube in upper cover 2
Module is managed, and battery management module is connected with battery, accessory power outlet 9 and limit switch 10 at the same time, battery management module uses
Existing control mainboard, is positioned over inside battery cover, and full packaging type structure not only physically protects mainboard, but also whole battery
Lid can form a potent radiator, and the heat that battery mainboard produces is dispersed, ensures the safety of circuit.It is provided with upper cover 2
The control panel 8 being connected with battery management module, this control panel 8 also can directly bought on the market, control panel 8
On be provided with cell switch, LED lamplight is shown and buzzer, battery can be combined by different light status and buzzer, with
Complete different condition prompting or warning function.The communication mould for carrying out real-time communication is provided with battery management module
Block, communication module are also existing and can directly buy on the market, be connected by battery delivery outlet with the external world, in time by number
According to output, especially for aircraft, ground handling operator can accurately grasp battery status, and then more rational rule in real time
Draw and use.
Embodiment 5：
As shown in Figures 3 to 8, used first when unmanned machine battery is fixed during bead introducing mechanism, not only in battery
In fixation, while it can be used for the Quick-dismantling structures such as Quick Release medicine-chest, and the bead introducing mechanism of the utility model is on battery
Installation site and quantity are unlimited, its number can be 1~n, and position can be any rational fixed bit, can be according to fixation
Bit quantity and section form reasonable layout, the either plane of symmetry are set or symmetric angle is set, and are found by many experiments,
Its optimal arrangement is structure shown in Fig. 7, and bead introducing mechanism is arranged at the seamed edge of battery, and this mode is by glass
Pearl introducing mechanism protrudes and maximum contact surface, the wedge-like engagement mode of recycling bead introducing mechanism, when greatly increasing importing
Stationarity, when battery is tetrahedron, bead introducing mechanism is separately mounted on four seamed edges, when being other polyhedrons, its
It is corresponding to be installed on other seamed edges.
Above-described embodiment, the purpose of this utility model, technical solution and beneficial effect have been carried out into
One step describes in detail, it should be understood that the foregoing is merely specific embodiment of the present utility model, is not used to limit
Determine the scope of protection of the utility model, where within the spirit and principles of the present invention, any modification for being made, equally replace
Change, improve, should be included within the scope of protection of this utility model.
Claims (10)
1. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery, it is characterised in that include the shell of inner cavity installation battery
(6), several introducing mechanisms for being used to be matched with battery mounting base are provided with the side wall of the shell (6), by leading
Enter mechanism realization to move along battery mounting base or fix with battery mounting base.
2. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 1, it is characterised in that the importing
Mechanism is bead introducing mechanism.
3. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 2, it is characterised in that the bead
Introducing mechanism is wedge-shaped bead introducing mechanism (3).
4. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 3, it is characterised in that the shell
(6) lower section is provided with frame, and frame roof is protruded to form some framework pillars (4), and shell (6) is arranged on framework pillar (4)
In the region of formation, and shell (6) wall is bonded with framework pillar (4) inner wall, and wedge-shaped bead introducing mechanism (3), which is installed on, to be corresponded to
Framework pillar (4) outer wall on.
5. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 4, it is characterised in that the frame
Bottom is provided with shock callus (5).
6. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 1, it is characterised in that the shell
(6) top surface is provided with upper cover (2), and upper cover (2) is fixed with shell (6), and battery is arranged on upper cover (2) and shell (6) shape
Into seal cavity in.
7. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 6, it is characterised in that the upper cover
(2) quick plug (7) and handle (1) are provided with, and quick plug (7) is connected with battery.
8. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 7, it is characterised in that described quick
Plug (7) includes quick plug shell (11), and quick plug shell (11) is fixed with upper cover (2), in quick plug shell (11)
Accessory power outlet (9) and limit switch (10) are provided with, and limit switch (10) is arranged on below accessory power outlet (9), accessory power outlet
(9) it is connected with limit switch (10) through upper cover (2) with battery.
9. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 8, it is characterised in that the upper cover
(2) be provided with battery management module in, and battery management module at the same time with battery, accessory power outlet (9) and limit switch (10)
Connection.
10. unmanned aerial vehicle onboard integral and intelligent Quick Release power battery according to claim 9, it is characterised in that on described
The control panel (8) being connected with battery management module is installed on lid (2), control panel is provided with cell switch, LED on (8)
Light is shown and buzzer, and communication module is provided with battery management module, is connected by battery delivery outlet with the external world.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721347369.5U CN207233839U (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721347369.5U CN207233839U (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207233839U true CN207233839U (en) | 2018-04-13 |
Family
ID=61851726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721347369.5U Expired - Fee Related CN207233839U (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard integral and intelligent Quick Release power battery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207233839U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112290153A (en) * | 2020-09-28 | 2021-01-29 | 东风汽车集团有限公司 | Power battery's installing support assembly |
-
2017
- 2017-10-19 CN CN201721347369.5U patent/CN207233839U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112290153A (en) * | 2020-09-28 | 2021-01-29 | 东风汽车集团有限公司 | Power battery's installing support assembly |
| CN112290153B (en) * | 2020-09-28 | 2021-09-17 | 东风汽车集团有限公司 | Power battery's installing support assembly |
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Effective date of registration: 20180516 Granted publication date: 20180413 |
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Date of cancellation: 20190109 Granted publication date: 20180413 |
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| TR01 | Transfer of patent right |
Effective date of registration: 20190131 Address after: Room 211-17, 2nd floor, Building C, Nangang Industrial Zone Office Building, Binhai New District, Tianjin, 300457 Patentee after: Longxiang Hi-Tech (Tianjin) Technology Co., Ltd. Address before: 610000 No. 115 Xingguang West Road, Chengdu Economic and Technological Development Zone (Longquanyi District), Sichuan Province Patentee before: Sichuan Raytheon Aerospace Technology Co., Ltd. |
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