CN206857013U - A kind of rotor wing unmanned aerial vehicle charging device and replacing battery system - Google Patents
A kind of rotor wing unmanned aerial vehicle charging device and replacing battery system Download PDFInfo
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- CN206857013U CN206857013U CN201720449604.3U CN201720449604U CN206857013U CN 206857013 U CN206857013 U CN 206857013U CN 201720449604 U CN201720449604 U CN 201720449604U CN 206857013 U CN206857013 U CN 206857013U
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- battery
- aerial vehicle
- unmanned aerial
- wing unmanned
- rotor wing
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Abstract
It the utility model is related to unmanned plane applied technical field; more particularly to a kind of rotor wing unmanned aerial vehicle charging device and replacing battery system; rotor wing unmanned aerial vehicle charging device includes battery stake; the top surface of the battery stake is airplane parking area; the airplane parking area is provided with empty battery case and the reserve cell groove equipped with fully charged battery; the empty battery case is used for accepting the battery fallen from rotor wing unmanned aerial vehicle; the both sides of the airplane parking area are equipped with the mechanical push rods of W types, and the distance of two points of dashing forward of the W types of the mechanical push rods is equal with the spacing of the landing gear of the rotor wing unmanned aerial vehicle.The utility model sets the mechanical push rods of W types in the both sides of battery stake, rotor wing unmanned aerial vehicle can be realized and positioned, the registration, reliable, and positioning method is simple.
Description
Technical field
It the utility model is related to unmanned plane applied technical field, more particularly to a kind of rotor wing unmanned aerial vehicle charging device and replacing
Battery system.
Background technology
The not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself is referred to as unmanned
Aircraft, referred to as " unmanned plane ", from technical standpoint, unmanned plane can be divided into：Unmanned fixed-wing aircraft, unmanned VTOL machine, nobody
Dirigible, depopulated helicopter, rotor wing unmanned aerial vehicle and umbrella wing unmanned plane etc..In recent years, as earthquake, flood, nuclear pollution etc. are large-scale
Natural calamity takes place frequently, and due to the rotor wing unmanned aerial vehicle risk that has that cost is low, efficiency-cost ratio is high, no one was injured and can set foot in someone
The advantages that region (core, chemistry, bacterium infection region) that machine can not reach, the research of rotor wing unmanned aerial vehicle is increasingly becoming unmanned plane and ground
The focus studied carefully.In addition, also it is with a wide range of applications in dual-use field, as low-altitude reconnaissance, meteorological exploration, aviation are taken the photograph
Shadow, traffic patrolling etc..But due to being confined to the body size of rotor wing unmanned aerial vehicle, the flight time is very in the air for rotor wing unmanned aerial vehicle
It is short, it is necessary to change battery and battery is charged, at present, conventional charging device is when rotor wing unmanned aerial vehicle stops falling, to rotor
The positioning method of unmanned plane is excessively complicated, and positioning form is unreliable, and certain timeliness sex chromosome mosaicism be present.
Utility model content
(1) technical problems to be solved
The utility model provides a kind of rotor wing unmanned aerial vehicle charging device and changes battery system, for solving existing rotor
Unmanned plane positions complicated, insecure problem when charging.
(2) technical scheme
In order to solve the above-mentioned technical problem, the utility model provides a kind of rotor wing unmanned aerial vehicle charging device, including battery stake,
The top surface of the battery stake is airplane parking area, and the airplane parking area is provided with empty battery case and the reserve cell equipped with fully charged battery
Groove, the empty battery case are used for accepting the battery fallen from rotor wing unmanned aerial vehicle, and the both sides of the airplane parking area are equipped with the machinery of W types
Push rod, the distance of two points of dashing forward of the W types of the mechanical push rods are equal with the spacing of the landing gear of the rotor wing unmanned aerial vehicle.
Wherein, the mechanical push rods connect motor by rack linkage.
Wherein, the batter-charghing system to be charged to the battery is provided with inside the battery stake.
Wherein, the both sides of the battery stake are equipped with solar panel.
Wherein, the solar panel is spindle rotationally arranged in the both sides of the battery stake.
Wherein, the surfacing of the airplane parking area is acrylic.
Wherein, the battery includes battery container, and the upper and lower surface of the battery container is equipped with as power interface
Groove.
Wherein, the material of the shell is insulated high-strength plastics.
Wherein, the groove is conductor recesses.
The utility model additionally provides a kind of rotor wing unmanned aerial vehicle and changes battery system, including rotor wing unmanned aerial vehicle and above-mentioned rotation
Wing unmanned plane charging device, it is characterised in that the rotor wing unmanned aerial vehicle includes battery carry plate, and the battery carry plate is provided with
Dead electricity type electromagnet, the dead electricity type electromagnet includes shell, in the shell and the coil that sets gradually up and down and forever
The magnetic of magnet, magnetic caused by the coil electricity and the permanent magnet is on the contrary, to offset the magnetic of the permanent magnet.
(3) beneficial effect
Rotor wing unmanned aerial vehicle charging device provided by the utility model, has the characteristics that compared to prior art：
1st, rotor wing unmanned aerial vehicle charging device provided by the utility model, by the machinery that W types are set in the both sides of battery stake
Push rod, rotor wing unmanned aerial vehicle can be realized and be accurately positioned, and the movement to rotor wing unmanned aerial vehicle can be realized, so that dead electricity type is electric
The different groove locations in magnet alignment battery stake top portion；
2nd, rotor wing unmanned aerial vehicle provided by the utility model changes battery system, by setting the rotation with dead electricity type electromagnet
Wing unmanned plane and the cooperation of battery stake, the quick-replaceable of rotor wing unmanned aerial vehicle battery is realized, automation can be realized, improve efficiency,
Reduce labor intensity.
Brief description of the drawings
Fig. 1 is the structure chart of rotor wing unmanned aerial vehicle charging device provided by the utility model；
Fig. 2 is the structure chart of mechanical push rods provided by the utility model；
Fig. 3 is the structure chart that rotor wing unmanned aerial vehicle provided by the utility model changes battery system；
Fig. 4 is the structure chart of rotor wing unmanned aerial vehicle provided by the utility model；
Fig. 5 is the structure chart of battery carry plate provided by the utility model；
Fig. 6 is the structure chart of dead electricity type electromagnet provided by the utility model；
Fig. 7 is the structure chart of battery provided by the utility model；
In figure, 1：Battery carry plate；2：Dead electricity type electromagnet；201：Shell；202：Coil；203：Permanent magnet；3：Battery
Stake；301：Empty battery case；302：Energy-storage battery groove；4：Mechanical push rods；5：Landing gear；6：Rack linkage；7：Motor；
8：Solar panel；9：Battery；901：Battery container；902：Conductor recesses.
Embodiment
For the ease of understanding the utility model, the utility model is more fully retouched below with reference to relevant drawings
State.Better embodiment of the present utility model is given in accompanying drawing.It these are only preferred embodiment of the present utility model, and unprovoked
This limits the scope of the claims of the present utility model, every equivalent structure made using the utility model specification and accompanying drawing content or
Equivalent flow conversion, or other related technical areas are directly or indirectly used in, similarly it is included in of the present utility model special
In sharp protection domain.
Unless otherwise defined, all of technologies and scientific terms used here by the article is led with belonging to technology of the present utility model
The implication that the technical staff in domain is generally understood that is identical.It is simply in term used in the description of the present utility model herein
The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term as used herein " and/or " bag
Include the arbitrary and all combination of the Listed Items of one or more correlations.
The utility model provides a kind of rotor wing unmanned aerial vehicle charging device and changes battery system, for solving existing rotor
Unmanned plane positions complicated, insecure problem when charging.
As shown in Figure 1, 2, a kind of rotor wing unmanned aerial vehicle charging device, including battery stake 3 are provided in the utility model embodiment,
The top surface of battery stake 3 is airplane parking area, and airplane parking area is provided with empty battery case 301 and the reserve cell groove 302 equipped with fully charged battery,
Empty battery case 301 is used for accepting the battery 9 that is fallen from rotor wing unmanned aerial vehicle, the size of empty battery case 301 and reserve cell groove 302 and
The size of battery 9 is suitable, so as to which the battery 9 of rotor wing unmanned aerial vehicle is fallen into hole battery case 301, and empty battery case 301 and deposit
About 1cm is spaced between battery case 302.The both sides of airplane parking area are equipped with the mechanical push rods 4 of W types, the W types of each mechanical push rods 4
The distance of two points of dashing forward is equal with the spacing of the landing gear 5 of rotor wing unmanned aerial vehicle.The mechanical push rods 4 of W types can be in rotor wing unmanned aerial vehicle
When dropping on airplane parking area, the positioning to rotor wing unmanned aerial vehicle is realized.Wherein, undercarriage 5 is that four stripe pitch are equal into matrix distribution
Thin column, due to two of W types points of dashing forward of each mechanical push rods 4 distances and rotor wing unmanned aerial vehicle landing gear 5 spacing
It is equal, the thin column of the landing gear 5 of rotor wing unmanned aerial vehicle can be stuck in two prominent points of the W types of two W types mechanical push rods 4
In, it is high so as to which rotor wing unmanned aerial vehicle to be respectively positioned to different positions, the accurate positioning of the positioning method, and operating efficiency.
When rotor wing unmanned aerial vehicle needs charging, rotor wing unmanned aerial vehicle can be dropped on the airplane parking area of battery stake 3, first by rotor
The battery 9 without electricity of unmanned plane is directed at empty battery case 301, will fall into sky battery case 301 without battery 9 on rotor wing unmanned aerial vehicle
It is interior, then rotor wing unmanned aerial vehicle is directed at reserve cell groove 302, the battery 9 that will be filled with electricity is arranged on rotor wing unmanned aerial vehicle, realizes battery
Replacing and charging.
In the present embodiment, in order to realize the movement of mechanical push rods, in order to position rotor wing unmanned aerial vehicle, mechanical push rods 4 pass through
Rack linkage 6 connects motor 7, under the dynamic action of motor 7, the driving mechanical push rod 4 of rack linkage 6
It is mobile, so as to realize the clamping to landing gear 5, and the movement to rotor wing unmanned aerial vehicle, to be respectively aligned to the He of sky battery case 301
Reserve cell groove 302.
The utility model provides a kind of rotor wing unmanned aerial vehicle charging device, by the machinery that W types are set in the both sides of battery stake 3
Push rod 4, rotor wing unmanned aerial vehicle can be realized and be accurately positioned, and the movement to rotor wing unmanned aerial vehicle can be realized, so that dead electricity type
Electromagnet 2 is directed at the empty battery case 301 and reserve cell groove 302 at the top of battery stake 3.
In the present embodiment, the inside of battery stake 3 is provided with the batter-charghing system to be charged to battery.For the ease of to no electric
Charged in battery 9, the inside of battery stake 3 is provided with the battery with master control neutral circuit, total battery and battery charger and filled
Electric system, after no electric battery 9 is fallen into sky battery case 301 from rotor wing unmanned aerial vehicle, the charging inlet connection at the back side of battery 9
Batter-charghing system, realize the charging to battery 9.
In the present embodiment, the both sides of battery stake 3 are equipped with solar panel 8, rotor provided by the utility model nobody
Machine charging device, can be by solar panel to battery by being respectively provided with solar panel 8 in the both sides of battery stake 3
Power supply, solves the problems, such as that field does not have power supply.Further, solar panel 8 is spindle rotationally arranged in battery stake 3,
In the case of power free in the wild, the solar panel 8 of both sides is pulled open and propped up, is powered using solar energy.
In the present embodiment, the surfacing of airplane parking area is acrylic, and the surface of airplane parking area is smooth acrylic material, can
To reduce friction during rotor wing unmanned aerial vehicle landing.
As seen in figures 3-6, the utility model also provides a kind of rotor wing unmanned aerial vehicle and changes battery system, including rotor wing unmanned aerial vehicle
With rotor wing unmanned aerial vehicle charging device, rotor wing unmanned aerial vehicle includes battery carry plate 1, and battery carry plate 1 is provided with dead electricity type electromagnet
2, it is to be understood that dead electricity type electromagnet 2 can be set up in parallel to be multiple, to there is multiple batteries to be adsorbed, to rotor without
The enough power of man-machine offer, in the present embodiment, dead electricity type electromagnet 2 is provided with two, wherein, dead electricity type electromagnet 2 includes outer
Shell 201, located at the interior loop 202 of shell 201 and permanent magnet 203, and coil 202 and permanent magnet 203 in shell 201 from top to bottom
Set gradually, coil 202 be powered caused by magnetic and permanent magnet 203 magnetic on the contrary, to offset the magnetic of permanent magnet 203；Rotation
Wing unmanned plane charging device includes battery stake 3, and the top surface of battery stake 3 is airplane parking area, and rotor wing unmanned aerial vehicle is provided with control system, should
Control system can control rotor wing unmanned aerial vehicle to drop on airplane parking area, and airplane parking area is provided with empty battery case 301 and equipped with fully charged
The reserve cell groove 302 of battery, empty battery case 301 are used for accepting the battery fallen from rotor wing unmanned aerial vehicle, empty battery case 301 and storage
The size of standby battery case 302 and the size of battery are suitable, so as to which the battery of rotor wing unmanned aerial vehicle is fallen into hole battery case 301, and
About 1cm is spaced between empty battery case 301 and reserve cell groove 302.The both sides of airplane parking area are equipped with the mechanical push rods 4 of W types, each
The distance of the prominent point of two of the W types of mechanical push rods 4 is equal with the spacing of the landing gear 5 of rotor wing unmanned aerial vehicle.The mechanical push rods 4 of W types
The positioning to rotor wing unmanned aerial vehicle can be realized when rotor wing unmanned aerial vehicle is dropped on airplane parking area.Wherein, between undercarriage 5 is four
Away from the equal thin column into matrix distribution, due to the distance and rotor wing unmanned aerial vehicle of two points of dashing forward of the W types of each mechanical push rods 4
Landing gear 5 spacing it is equal, the thin column of the landing gear 5 of rotor wing unmanned aerial vehicle can be stuck in two W types mechanical push rods 4
In the prominent point of two of W types, so that rotor wing unmanned aerial vehicle is respectively positioned to different positions, the accurate positioning of the positioning method, and
Operating efficiency is high.When rotor wing unmanned aerial vehicle needs charging, rotor wing unmanned aerial vehicle can be dropped on the airplane parking area of battery stake 3, first will
Rotor wing unmanned aerial vehicle is directed at empty battery case 301 without battery, and coil 202 is powered, and adsorbs electric without electricity on rotor wing unmanned aerial vehicle
Pond is fallen into sky battery case 301, then the dead electricity type electromagnet 2 of rotor wing unmanned aerial vehicle is aligned into reserve cell groove 302, disconnects coil
202 power supply, fully charged battery are attracted in the presence of permanent magnet 203 on dead electricity type electromagnet 2, realize battery oneself
It is dynamic to change.
Rotor wing unmanned aerial vehicle provided by the utility model changes battery system, by using the rotation with dead electricity type electromagnet 2
Wing unmanned plane and the cooperation of battery stake 3, the quick-replaceable of rotor wing unmanned aerial vehicle battery is realized, automation can be realized, improve efficiency,
Reduce labor intensity.
In the present embodiment, for the ease of needing to fall on no electric battery, battery carry plate 1 is provided with electric supply installation
(not shown).The electric supply installation to dead electricity type electromagnet 2 power when, coil 202 produces magnetic, offsets permanent magnet 203
Magnetic so that without electricity battery fall, in addition, the electric supply installation can also when there is no battery powered, the short time to
Rotor wing unmanned aerial vehicle provides a small amount of electric energy, ensures that rotor wing unmanned aerial vehicle does not shut down.
In the present embodiment, in order to facilitate the setting of coil 202 and permanent magnet 203, the shell 201 of dead electricity type electromagnet 2 is
Cylindrical shell.In addition, the shell 201 of dead electricity type electromagnet 2 is conductor material, the shell 201 and rotor of conductor material nobody
Power supply interface inside machine is connected, and when dead electricity type electromagnet 2 adsorbs battery, electric energy in battery is by conductor casing to rotor
Unmanned plane is powered.
As shown in fig. 7, in the present embodiment, battery 9 includes battery container 901, and the battery is rectangle combined battery, electricity
The material of pond housing 901 is insulated high-strength plastics, and the upper and lower surface of battery container 901 is equipped with conductor recesses 11, and conductor is recessed
The material of groove 902 is 1mm thickness alloy iron plates, should be with the rectangle combined battery 9 of conductor recesses 902, can be by permanent magnet
203 absorption, and electric energy is provided.It is understood that the top surface of battery 9 has two conductor guide grooves for connecing positive pole and negative pole respectively
902, there are four conductor recesses 902 for connecing a positive pole and three negative poles the bottom surface of battery 9, the top surface of battery 9 be provided with to rotor without
The power supply interface of man-machine power supply, the bottom surface of battery 9 are provided with the charging inlet to be charged to battery 9, the power supply interface of battery 9 and charging
Interface uses weak magnetic suction, in that context it may be convenient to is dismantled, weak magnetic property enough ensures the abundant contact of interface, is unlikely to again very
Hardly possible separation., can be with the power supply interface adhesive of rotor wing unmanned aerial vehicle, so as to rotation after the top surface of battery is adsorbed by dead electricity type electromagnet 2
Wing unmanned plane is powered；, can be with the charging in battery stake 3 when the bottom surface of battery is absorbed in the empty battery case 301 of airplane parking area
Mouth adhesive, so as to be charged.
The course of work that rotor wing unmanned aerial vehicle changes battery system is as described below：
Under the control of the control system with GPS positioning technology, when the top of battery stake 3 is arrived in rotor wing unmanned aerial vehicle flight,
Signal is sent to battery stake 3, and battery stake 3 is worked well preparation.Mechanical push rods 4 are opened, and rotor wing unmanned aerial vehicle is according to fixed direction
Drop to the random place of airplane parking area, now, mechanical push rods 4 are released, the undercarriage 5 of rotor wing unmanned aerial vehicle for four stripe pitch it is equal into
The thin column of matrix distribution, during mechanical push rods 4 contact undercarriage 5 and move, four thin columns of undercarriage 5
The groove of W two points of dashing forward is respectively embedded in, positioning is realized by moving left and right.Now, the energy-storage battery groove on airplane parking area
Interior 302 are embedded with fully charged battery, do not have battery in empty battery case 301.After completing precise positioning, rotor wing unmanned aerial vehicle is pushed away first
To at the empty battery case 301 of airplane parking area, then, the electric supply installation of battery carry plate 1 is powered to the coil 202 of dead electricity type magnet 2,
Dead electricity type electromagnet 2 loses magnetism, by battery of the magnetic absorption of permanent magnet 203 on dead electricity type magnet 2 because gravity falls
Fall in the empty battery case 301 of lower section, empty battery case 301 is automatic right in the presence of the batter-charghing system inside battery stake 3
This dead battery is charged.After battery stake 3 detects that rotor wing unmanned aerial vehicle does not have battery, be moved into has battery in addition
Energy-storage battery groove 302 at, now stop powering to the coil 202 of dead electricity type electromagnet 2, dead electricity type electromagnet 2 show magnetic,
Again the fully charged battery in absorption lower section, is adsorbed with battery when rotor wing unmanned aerial vehicle detects, takes off again.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc., the utility model should be included in
Protection domain within.
Claims (10)
- A kind of 1. rotor wing unmanned aerial vehicle charging device, it is characterised in that including battery stake, the top surface of the battery stake is airplane parking area, The airplane parking area is provided with empty battery case and the reserve cell groove equipped with fully charged battery, and the empty battery case is used for accepting from rotation The battery that wing unmanned plane is fallen, the both sides of the airplane parking area are equipped with the mechanical push rods of W types, and the two of the W types of the mechanical push rods Individual prominent sharp distance is equal with the spacing of the landing gear of the rotor wing unmanned aerial vehicle.
- 2. rotor wing unmanned aerial vehicle charging device according to claim 1, it is characterised in that the mechanical push rods are joined by rack Dynamic device connection motor.
- 3. rotor wing unmanned aerial vehicle charging device according to claim 1, it is characterised in that be provided with inside the battery stake to institute State the batter-charghing system of battery charging.
- 4. rotor wing unmanned aerial vehicle charging device according to claim 1, it is characterised in that the both sides of the battery stake are equipped with Solar panel.
- 5. rotor wing unmanned aerial vehicle charging device according to claim 4, it is characterised in that the solar panel is rotatable The both sides for being arranged on the battery stake.
- 6. the rotor wing unmanned aerial vehicle charging device according to any one of claim 1-5, it is characterised in that the airplane parking area Surfacing is acrylic.
- 7. the rotor wing unmanned aerial vehicle charging device according to any one of claim 1-5, it is characterised in that the battery includes Battery container, the upper and lower surface of the battery container are equipped with the groove as power interface.
- 8. rotor wing unmanned aerial vehicle charging device according to claim 7, it is characterised in that the material of the battery container is exhausted Edge highstrenghtpiston.
- 9. rotor wing unmanned aerial vehicle charging device according to claim 7, it is characterised in that the groove is conductor recesses.
- 10. a kind of rotor wing unmanned aerial vehicle changes battery system, it is characterised in that any including rotor wing unmanned aerial vehicle and claim 1-9 Rotor wing unmanned aerial vehicle charging device described in, the rotor wing unmanned aerial vehicle include battery carry plate, and the battery carry plate is provided with Dead electricity type electromagnet, the dead electricity type electromagnet includes shell, in the shell and the coil that sets gradually up and down and forever The magnetic of magnet, magnetic caused by the coil electricity and the permanent magnet is on the contrary, to offset the magnetic of the permanent magnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720449604.3U CN206857013U (en) | 2017-04-26 | 2017-04-26 | A kind of rotor wing unmanned aerial vehicle charging device and replacing battery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720449604.3U CN206857013U (en) | 2017-04-26 | 2017-04-26 | A kind of rotor wing unmanned aerial vehicle charging device and replacing battery system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206857013U true CN206857013U (en) | 2018-01-09 |
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ID=60822943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720449604.3U Expired - Fee Related CN206857013U (en) | 2017-04-26 | 2017-04-26 | A kind of rotor wing unmanned aerial vehicle charging device and replacing battery system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206857013U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161343A (en) * | 2017-04-26 | 2017-09-15 | 海南大学 | A kind of rotor wing unmanned aerial vehicle and its replacing battery system |
| CN108177790A (en) * | 2018-02-07 | 2018-06-19 | 西安工业大学 | A kind of unmanned plane relay station and its method |
| CN108928479A (en) * | 2018-06-28 | 2018-12-04 | 山东浩坤安全技术咨询有限公司 | A kind of rotor wing unmanned aerial vehicle with solar recharging |
-
2017
- 2017-04-26 CN CN201720449604.3U patent/CN206857013U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161343A (en) * | 2017-04-26 | 2017-09-15 | 海南大学 | A kind of rotor wing unmanned aerial vehicle and its replacing battery system |
| CN107161343B (en) * | 2017-04-26 | 2020-08-21 | 海南大学 | Rotor unmanned aerial vehicle and change battery system thereof |
| CN108177790A (en) * | 2018-02-07 | 2018-06-19 | 西安工业大学 | A kind of unmanned plane relay station and its method |
| CN108177790B (en) * | 2018-02-07 | 2023-05-12 | 西安工业大学 | Unmanned aerial vehicle relay station and method thereof |
| CN108928479A (en) * | 2018-06-28 | 2018-12-04 | 山东浩坤安全技术咨询有限公司 | A kind of rotor wing unmanned aerial vehicle with solar recharging |
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| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180109 Termination date: 20210426 |
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| CF01 | Termination of patent right due to non-payment of annual fee |