CN110155346B - A solar cell adds holds device for unmanned aerial vehicle - Google Patents
A solar cell adds holds device for unmanned aerial vehicle Download PDFInfo
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- CN110155346B CN110155346B CN201910409695.1A CN201910409695A CN110155346B CN 110155346 B CN110155346 B CN 110155346B CN 201910409695 A CN201910409695 A CN 201910409695A CN 110155346 B CN110155346 B CN 110155346B
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- unmanned aerial
- aerial vehicle
- solar cell
- frame
- clamping device
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- 229920000915 polyvinyl chloride Polymers 0.000 claims description 3
- 239000004800 polyvinyl chloride Substances 0.000 claims description 3
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 abstract description 9
- 230000005611 electricity Effects 0.000 description 5
- 230000005389 magnetism Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
-
- 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
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention provides a solar cell adding and holding device for an unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises a cell frame for placing a solar cell and a splicing frame connected with the cell frame, wherein a fixed rod for connecting with an unmanned aerial vehicle body is arranged on the splicing frame, the upper surface of the splicing frame protrudes upwards, the cell frame is connected with an annular ring, a protruding part is arranged on the side surface of the splicing frame, an annular sliding groove for rotating the protruding part is formed in the inner wall of the annular ring, a magnetic part is arranged on the annular ring, an electromagnetic part, a power supply electrically connected with the electromagnetic part and a lead wire groove electrically connected with an engine of the unmanned aerial vehicle are arranged on the splicing frame, a first joint is arranged below the lead wire groove, and a second joint for connecting with the first joint is arranged on the solar. The solar cell clamping device for the unmanned aerial vehicle is simple in structure, can be directly installed on the existing unmanned aerial vehicle, is convenient to install and maintain, and greatly improves the cruising ability of the unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles,
in particular, the present invention relates to a solar cell holding device for an unmanned aerial vehicle.
Background
Along with the rapid development of civil unmanned aerial vehicles, unmanned aerial vehicle shadows are increasingly appearing on advertisements, movies, wedding video records and the like. Present civilian unmanned aerial vehicle charges for the battery, then provides the electric energy for the inside electrical components of unmanned aerial vehicle, but owing to use needs longer time such as some unmanned aerial vehicles take photo by plane, the battery can not provide sufficient electric energy, so has taken solar cell panel's unmanned aerial vehicle, sets up solar cell panel tiling on unmanned aerial vehicle, absorbs external light energy to supply unmanned aerial vehicle to continue a journey.
But the unmanned aerial vehicle of many models does not load solar cell panel now, and the unmanned aerial vehicle's after having loaded solar cell panel weight can increase moreover, and the ability of continuing endurance receives great influence.
Therefore, in order to solve the above problems, it is necessary to design a reasonable solar cell holding device for the unmanned aerial vehicle.
Disclosure of Invention
The invention aims to provide a solar cell holding device for an unmanned aerial vehicle, which has a simple structure, can be directly installed on the existing unmanned aerial vehicle, is convenient to install and maintain, and greatly improves the cruising ability of the unmanned aerial vehicle.
In order to achieve the purpose, the invention is realized by adopting the following technical scheme:
the utility model provides a solar cell adds holds device for unmanned aerial vehicle, including be used for placing solar cell's battery rack and with the concatenation frame that the battery rack is connected, be provided with the dead lever that is used for with the unmanned aerial vehicle body coupling on the concatenation frame, the upper surface of concatenation frame is upwards protruding, the battery rack is connected with annular ring, concatenation frame side is provided with the bellying, annular ring inner wall is provided with and is used for bellying pivoted ring type spout, be provided with the magnetic part on the annular ring, be provided with the electromagnetic part on the concatenation frame, with the power of electromagnetic part electricity connection and be used for the lead wire groove of being connected with unmanned aerial vehicle engine electricity, lead wire groove below is provided with first joint, solar cell last be provided with be used for with first articulate second connects.
Preferably, a voltage inductor electrically connected with the primary battery of the unmanned aerial vehicle is arranged between the power supply and the electromagnetic piece.
Preferably, the magnetic member includes a first magnetic member and a second magnetic member, and the first magnetic member and the second magnetic member have opposite magnetic poles.
Preferably, the first magnetic member and the second magnetic member are respectively disposed at two ends of the annular ring.
Preferably, the lead slot comprises a first lead slot electrically connected with the positive pole of the engine of the unmanned aerial vehicle and a second lead slot electrically connected with the negative pole of the engine of the unmanned aerial vehicle.
Preferably, the lead slot is connected with the unmanned aerial vehicle engine through a lead, and a lead through hole for facilitating the lead to pass through is formed in the fixing rod.
Preferably, the battery rack and the splicing rack are both made of polyvinyl chloride.
Preferably, the number of the first joint and the second joint is at least two.
Preferably, at least a portion of the battery holder is arc-shaped.
Preferably, a waterproof layer is provided on the outer side of the battery holder.
The solar cell clamping device for the unmanned aerial vehicle has the beneficial effects that:
simple structure can the direct mount on current unmanned aerial vehicle, is convenient for install and maintain, has greatly improved unmanned aerial vehicle's duration.
Drawings
FIG. 1 is a schematic structural diagram of one embodiment of the present invention;
FIG. 2 is a schematic top view of an embodiment of the present invention;
FIG. 3 is a schematic illustration of the magnetic field in one embodiment of the present invention;
FIG. 4 is a schematic illustration of magnetic fields in another embodiment of the present invention;
in the figure: 1. the solar cell module comprises a cell frame 11, a solar cell 12, an annular ring 121, an annular sliding groove 13, a magnetic part 131, a first magnetic part 132, a second magnetic part 2, a splicing frame 21, a fixing rod 22, a protruding part 23, an electromagnetic part 24, a power supply 25, a lead slot 251, a first lead slot 252 and a second lead slot.
Detailed Description
The invention is further described below with reference to the accompanying drawings and examples.
Along with the rapid development of civil unmanned aerial vehicles, unmanned aerial vehicle shadows are increasingly appearing on advertisements, movies, wedding video records and the like. Present civilian unmanned aerial vehicle charges for the battery, then provides the electric energy for the inside electrical components of unmanned aerial vehicle, but owing to use needs longer time such as some unmanned aerial vehicles take photo by plane, the battery can not provide sufficient electric energy, so has taken solar cell panel's unmanned aerial vehicle, sets up solar cell panel tiling on unmanned aerial vehicle, absorbs external light energy to supply unmanned aerial vehicle to continue a journey.
But the unmanned aerial vehicle of many models does not load solar cell panel now, and the unmanned aerial vehicle's after having loaded solar cell panel weight can increase moreover, and the ability of continuing endurance receives great influence.
The first embodiment is as follows: as shown in fig. 1 to 3, which are only one embodiment of the present invention, a solar cell clamping device for an unmanned aerial vehicle comprises a cell holder 1 for holding a solar cell 11 and a splicing holder 2 connected to the cell holder 1, the splicing frame 2 is provided with a fixed rod 21 used for being connected with the unmanned aerial vehicle body, the upper surface of the splicing frame 2 is upwards convex, the battery frame 1 is connected with an annular ring 12, the side surface of the splicing frame 2 is provided with a convex part 22, the inner wall of the annular ring 12 is provided with an annular sliding groove 121 for the rotation of the boss 22, the annular ring 12 is provided with a magnetic part 13, the splicing frame 2 is provided with an electromagnetic part 23, a power supply 24 electrically connected with the electromagnetic part 23 and a lead groove 25 for electrically connecting with an unmanned aerial vehicle engine, a first connector is arranged below the lead groove 25, and a second connector used for being connected with the first connector is arranged on the solar cell.
In the invention, in order to enhance the cruising ability of the unmanned aerial vehicle, a solar cell holding device can be directly installed on the existing unmanned aerial vehicle, the cell frame 1 is used for placing the solar cell 11, the splicing frame 2 is connected with the cell frame 1, then the cell frame 1 is connected to the unmanned aerial vehicle body through the fixing rod 21, and finally the solar cell 11 can supply power to the unmanned aerial vehicle.
Firstly, the structure of the splicing frame 2 is adopted, the upper surface of the splicing frame 2 protrudes upwards, so that after the solar cell holding device for the unmanned aerial vehicle is loaded on the unmanned aerial vehicle of the existing model, the upper surface of the splicing frame 2 protrudes during the flight of the unmanned aerial vehicle, the air flowing through the upper surface of the splicing frame 2 moves fast, the air flowing below the splicing frame 2 moves slow, an upward lifting force is generated under the pressure difference, the load of the splicing frame 2 and the cell frame 1 on the unmanned aerial vehicle is reduced, and the cruising ability is ensured not to be influenced.
And, the upper surface of splicing frame 2 upwards protrudes, can increase the receiving area of the upper surface of splicing frame 2 for receiving solar energy, and can better collect solar energy.
Then be the connection of battery frame 1 and splice frame 2, battery frame 1 is connected with annular circle 12, 2 sides of splice frame are provided with bellying 22, the 12 inner walls of annular circle are provided with and are used for bellying 22 pivoted ring type spout 121, and splice frame 2 has at least partly to be located annular circle 12, and the bellying 22 card in the 2 outsides of splice frame in the ring type spout 121 of annular circle 12 inner wall, and the quantity of bellying 22 is one at least, and bellying 22 can freely rotate in ring type spout 121 like this, so after splice frame 2 and unmanned aerial vehicle support body fixed connection, and battery frame 1 can wind splice frame 2 free rotation.
Last is the combination of battery frame 1 and concatenation frame 2, be provided with magnetic part 13 on the annular ring 12, be provided with electromagnetic part 23 on the concatenation frame 2, with the power 24 that electromagnetic part 23 electricity is connected and be used for the lead wire groove 25 of being connected with unmanned aerial vehicle engine electricity, lead wire groove 25 below is provided with first joint, solar cell is last be provided with be used for with first articulate's second joint, power 24 supplies power to electromagnetic part 23, and electromagnetic part 23 produces magnetic field, and under the effect of the magnetic field power of magnetic part 13 (like poles repel each other opposite poles attract), the position of the relative concatenation frame 2 of battery frame 1 rotates, and the second joint on the last solar cell 11 and the first articulate that lead wire groove 25 below set up, last solar cell 11 is connected with unmanned aerial vehicle engine electricity through lead wire groove 25, supplies power to unmanned aerial vehicle.
The electromagnetic member 23 is an object that generates magnetism when energized.
In fact, in the installation of battery frame 1 and splice frame 2, with battery frame 1 and the installation of splice frame 2 dislocation, solar cell 11 can not supply power to unmanned aerial vehicle like this, when needs solar cell 11 to supply power to unmanned aerial vehicle, only need power 24 start-up work can.
The power supply 24 only needs a small capacity, and can complete the work of supplying power to the electromagnetic piece 23, and when the solar cell 11 supplies power to the unmanned aerial vehicle, the power supply 24 can be charged by the way.
It should be noted here that at least a part of the battery holder 1 is arc-shaped, and the battery holder 1 is preferably disc-shaped, so that in the process of the unmanned aerial vehicle performing a flight mission, the battery holder 1 is not blown to rotate in the gas flowing process, which results in the disconnection of the second connector on the solar cell 11 and the first connector arranged below the lead slot 25, and avoids the occurrence of the situation that the unmanned aerial vehicle loses power.
The solar cell clamping device for the unmanned aerial vehicle is simple in structure, can be directly installed on the existing unmanned aerial vehicle, is convenient to install and maintain, and greatly improves the cruising ability of the unmanned aerial vehicle.
The second embodiment is also shown in fig. 1 to 2, which is only one embodiment of the present invention, and in order to make the connection effect of the solar cell clamping device for the unmanned aerial vehicle of the present invention better and make the stability higher, the present invention further has the following design:
firstly, a voltage inductor electrically connected with the primary battery of the unmanned aerial vehicle is arranged between the power supply 24 and the electromagnetic piece 23. In case the unmanned aerial vehicle primary cell electric quantity is not enough like this, voltage drop to appointed threshold value, then starting power supply 24 supplies power to electromagnetic part 23, and solar cell 11 supplies power to unmanned aerial vehicle at last, guarantees unmanned aerial vehicle's continuation of the journey.
Then, the magnetic member 13 includes a first magnetic member 131 and a second magnetic member 132, and the first magnetic member 131 and the second magnetic member 132 have opposite magnetic poles. Because electromagnetism piece 23 is a whole, electromagnetism piece 23 has two magnetic poles, also set up first magnetism piece 131 and second magnetism piece 132 that two magnetic poles are opposite respectively so and carry out the magnetic field interaction to electromagnetism piece 23 simultaneously, the magnetic field atress is more stable, can effectively reduce 24 the power supply pressure to electromagnetism piece 23 of power, the relative splice frame 2's of cell holder 1 position rotates more sensitively, solar cell 11 supplies power more stably to unmanned aerial vehicle.
Moreover, the first magnetic member 131 and the second magnetic member 132 are respectively disposed at two ends of the annular ring 12. So that the two poles just opposite the electromagnet 23 generate magnetic forces.
Then, the lead groove 25 includes a first lead groove 251 electrically connected to the positive pole of the drone engine and a second lead groove 252 electrically connected to the negative pole of the drone engine.
And, lead wire groove 25 passes through the wire with the unmanned aerial vehicle engine and is connected, be provided with in the dead lever 21 and be used for making things convenient for the wire through-hole that the wire passes through.
Correspondingly, the quantity that first joint and second connect all is two at least, and first joint and second connect the connection that can be better like this, and solar cell 1 is better supplies power to unmanned aerial vehicle.
And finally, the battery frame 1 and the splicing frame 2 are both polyvinyl chloride pieces. The battery rack 1 and the splicing rack 2 are lighter, better in strength and better in corrosion resistance. The waterproof layer is arranged on the outer side of the battery frame 1, and water cannot enter the joint of the battery frame 1 and the splicing frame 2.
The solar cell clamping device for the unmanned aerial vehicle is simple in structure, can be directly installed on the existing unmanned aerial vehicle, is convenient to install and maintain, and greatly improves the cruising ability of the unmanned aerial vehicle.
The present invention is not limited to the above-described specific embodiments, and various modifications and variations are possible. Any modifications, equivalents, improvements and the like made to the above embodiments in accordance with the technical spirit of the present invention should be included in the scope of the present invention.
Claims (10)
1. The utility model provides a solar cell adds holds device for unmanned aerial vehicle which characterized in that: comprises a battery frame (1) used for placing a solar battery (11) and a splicing frame (2) connected with the battery frame (1), wherein a fixing rod (21) used for being connected with an unmanned aerial vehicle body is arranged on the splicing frame (2), the upper surface of the splicing frame (2) is upwards convex, a solar receiving plate is arranged on the upper surface of the splicing frame (2), the battery frame (1) is connected with an annular ring (12), a bulge part (22) is arranged on the side surface of the splicing frame (2), an annular sliding groove (121) used for rotating the bulge part (22) is arranged on the inner wall of the annular ring (12), a magnetic part (13) is arranged on the annular ring (12), an electromagnetic part (23), a power supply (24) electrically connected with the electromagnetic part (23) and a lead slot (25) electrically connected with an engine of the unmanned aerial vehicle are arranged on the splicing frame (2), a first connector is arranged below the lead groove (25), and a second connector used for being connected with the first connector is arranged on the solar cell (11).
2. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: and a voltage inductor electrically connected with the primary battery of the unmanned aerial vehicle is arranged between the power supply (24) and the electromagnetic piece (23).
3. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the magnetic part (13) comprises a first magnetic part (131) and a second magnetic part (132), and the first magnetic part (131) and the second magnetic part (132) have opposite magnetic poles.
4. The solar cell clamping device for the unmanned aerial vehicle according to claim 3, wherein: the first magnetic part (131) and the second magnetic part (132) are respectively arranged at two ends of the annular ring (12).
5. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the lead groove (25) comprises a first lead groove (251) electrically connected with the positive pole of the unmanned aerial vehicle engine and a second lead groove (252) electrically connected with the negative pole of the unmanned aerial vehicle engine.
6. The solar cell clamping device for the unmanned aerial vehicle according to claim 5, wherein: the lead groove (25) is connected with the unmanned aerial vehicle engine through a lead, and a lead through hole for allowing the lead to pass through is formed in the fixing rod (21).
7. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the battery rack (1) and the splicing rack (2) are both polyvinyl chloride pieces.
8. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the number of the first joints and the second joints is at least two.
9. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the battery rack (1) is disc-shaped.
10. The solar cell clamping device for the unmanned aerial vehicle according to claim 1, wherein: the number of the convex parts (22) is at least one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910409695.1A CN110155346B (en) | 2019-05-17 | 2019-05-17 | A solar cell adds holds device for unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910409695.1A CN110155346B (en) | 2019-05-17 | 2019-05-17 | A solar cell adds holds device for unmanned aerial vehicle |
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| CN110155346A CN110155346A (en) | 2019-08-23 |
| CN110155346B true CN110155346B (en) | 2021-04-02 |
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| CN114261292A (en) * | 2021-12-02 | 2022-04-01 | 歌尔科技有限公司 | Unmanned aerial vehicle system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN206983759U (en) * | 2017-07-04 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Unmanned plane charging device and vehicle-mounted unmanned aerial vehicle |
| CN108482687A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of unmanned plane photovoltaic panel mounting mechanism |
| CN109532543A (en) * | 2017-08-08 | 2019-03-29 | 梅汝爱 | A kind of New-energy electric vehicle emergency power supply charging pile |
| CN109546940A (en) * | 2018-12-07 | 2019-03-29 | 天津鑫福祥科技发展有限公司 | Solar photovoltaic assembly mounting bracket |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL260259B2 (en) * | 2016-05-13 | 2023-11-01 | Aurora Flight Sciences Corp | Solar power system and method thereof |
| US10239613B2 (en) * | 2017-01-23 | 2019-03-26 | Ameristar Solar, LLC | Solar power tethered drone |
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2019
- 2019-05-17 CN CN201910409695.1A patent/CN110155346B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206983759U (en) * | 2017-07-04 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Unmanned plane charging device and vehicle-mounted unmanned aerial vehicle |
| CN109532543A (en) * | 2017-08-08 | 2019-03-29 | 梅汝爱 | A kind of New-energy electric vehicle emergency power supply charging pile |
| CN108482687A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of unmanned plane photovoltaic panel mounting mechanism |
| CN109546940A (en) * | 2018-12-07 | 2019-03-29 | 天津鑫福祥科技发展有限公司 | Solar photovoltaic assembly mounting bracket |
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| CN110155346A (en) | 2019-08-23 |
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Address after: 231300 Gaotang village, Chengguan Town, Shucheng County, Lu'an City, Anhui Province Patentee after: Anhui Shuzhou Ecological Agriculture Technology Co.,Ltd. Address before: 231300 Gaotang village, Chengguan Town, Shucheng County, Lu'an City, Anhui Province Patentee before: ANHUI SHUZHOU AGRICULTURAL TECHNOLOGY Co.,Ltd. |
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Denomination of invention: A solar cell holding device for UAV Effective date of registration: 20210930 Granted publication date: 20210402 Pledgee: Anhui Shucheng Rural Commercial Bank Co., Ltd. Meihe road sub branch Pledgor: Anhui Shuzhou Ecological Agriculture Technology Co., Ltd Registration number: Y2021980010151 |
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