CN205882819U - On -vehicle solar charging system of wired electronic unmanned aerial vehicle - Google Patents
On -vehicle solar charging system of wired electronic unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205882819U CN205882819U CN201620640262.9U CN201620640262U CN205882819U CN 205882819 U CN205882819 U CN 205882819U CN 201620640262 U CN201620640262 U CN 201620640262U CN 205882819 U CN205882819 U CN 205882819U
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- China
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- charging system
- unmanned plane
- service cable
- unmanned aerial
- aerial vehicle
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Abstract
The utility model relates to an unmanned aerial vehicle field. On -vehicle solar charging system of wired electronic unmanned aerial vehicle, its characterized in that, including the charging system of setting on the car, charging system includes a solar cell panel, solar cell panel connects the module of charging, a battery that is used for storing the electric energy is connected to the module of charging, the battery is connected with unmanned aerial vehicle through a supply cable. The utility model discloses a set up charging system on the car, can pass through the supply cable continually and for unmanned aerial vehicle provides power, effectively prolong unmanned aerial vehicle's hang time, satisfy unmanned aerial vehicle carried out aircraft mission for a long time in among a small circle demand. Simultaneously, use solar cell panel as storage battery charging energy saving not only, can also satisfy the needs of user in the long -time operation in open air.
Description
Technical field
This utility model relates to unmanned plane field, is specifically related to unmanned plane charging system.
Background technology
Unmanned plane is exactly unpiloted aircraft.Unmanned plane during flying process by ground staff by remote control equipment command into
OK, or by the route automatic lifting stick implanted in advance fly and perform predetermined airflight plan.The most common unmanned plane
It mostly is electronic unmanned plane, and electronic unmanned plane many employings lithium battery provides energy, although alleviate unmanned plane quality, but still deposit
Long in the charging interval, that the flight time is short problem.Therefore, a flying power always the most thorny difficult problem is solved.
Utility model content
The purpose of this utility model is, it is provided that wire control electric unmanned plane Vehicular solar charging system, to solve at least
One above-mentioned technical problem.
This utility model is solved the technical problem that to realize by the following technical solutions:
Wire control electric unmanned plane Vehicular solar charging system, it is characterised in that include the Charging being arranged on automobile
System, described charging system includes that a solar panel, described solar panel connect a charging module, described charging module
Connecting an accumulator being used for storing electric energy, described accumulator is connected with unmanned plane by a service cable.
This utility model is by arranging charging system on automobile, it is possible to be unmanned plane by service cable endlessly
Power is provided, effectively extends the hang time of unmanned plane, meet unmanned plane long-time execution aerial mission in little scope
Demand.Meanwhile, using solar panel is that the energy is not only saved in accumulator charging, moreover it is possible to meet user the most long-time
The needs of operation.
Described solar panel uses flexible crystalline silicon solar cell plate.Flexible crystalline silicon solar cell plate can be with
The arc perfection laminating of car roof, and flexible crystalline silicon solar cell plate light weight, significantly reduce the weight of vehicle body.
The thickness of described flexible crystalline silicon solar cell plate is 2mm to 10mm, preferably 5mm.To alleviate vehicle body
Quality.
The back side of described flexible crystalline silicon solar cell plate is provided with one layer of adhesive-layer, described flexible crystalline silicon solar electricity
Pond plate is bonded in automobile top by described adhesive-layer.Fixing to realize.
Described unmanned plane includes that a control circuit plate, described control circuit plate connect the control end of a motor, described electricity
The power output shaft of motivation connects propeller, and described control circuit plate connects an attitude transducer.Described attitude transducer is monitored
The attitude information of unmanned plane is also sent to control circuit plate by UAV Attitude situation, and control circuit plate controls motor-driven spiral shell
Rotation oar, and then realize the attitude stabilization in flight course.
Described service cable includes the first service cable, the second service cable；
The outfan of described accumulator and one end of the first service cable are connected, and the other end of described first service cable is solid
Being scheduled on a reel, described reel is provided with a rotating shaft, and described rotating shaft is arranged with the second service cable, described second service cable
One end connect described unmanned plane, it is electric that the other end of described second service cable connects described first power supply by swivel
Cable；
Described rotating shaft connects a frequency conversion motor by drive disk assembly.Will pass through the forward and reverse realization power supply electricity of motor
The folding and unfolding of cable.
Described swivel is a rotating Elecrical connector.Facilitate implementation rotating shaft in rotation process, service cable
With being connected of the power output end of accumulator.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
For the technological means making this utility model realize, creation characteristic, reach purpose and be easy to understand with effect, under
Face combines to be specifically illustrating and this utility model is expanded on further.
See Fig. 1, wire control electric unmanned plane Vehicular solar charging system, including the charging system being arranged on automobile 2,
Charging system includes a solar panel, and solar panel connects a charging module, and charging module connects one and is used for storing
The accumulator of electric energy, accumulator is connected with unmanned plane 1 by a service cable.This utility model is by arranging charging on automobile
System, it is possible to provide power by service cable for unmanned plane endlessly, effectively extends the hang time of unmanned plane, full
Foot unmanned plane is the long-time demand performing aerial mission in little scope.Meanwhile, using solar panel is accumulator charging
Not only save the energy, moreover it is possible to meet the needs of user long working out of doors.
Solar panel uses flexible crystalline silicon solar cell plate.Flexible crystalline silicon solar cell plate energy and automobile
The arc perfection laminating of roof, and flexible crystalline silicon solar cell plate light weight, significantly reduce the weight of vehicle body.Flexible brilliant
The thickness of body silicon solar cell plate is 2mm to 10mm, preferably 5mm.To alleviate the quality of vehicle body.The flexible crystalline silicon sun
The back side of energy cell panel is provided with one layer of adhesive-layer, and flexible crystalline silicon solar cell plate is bonded in automobile top by adhesive-layer.
Fixing to realize.
Unmanned plane 1 includes a control circuit plate, and control circuit plate connects the control end of a motor, and the power of motor is defeated
Shaft connects propeller, and control circuit plate connects an attitude transducer.Described attitude transducer monitoring UAV Attitude situation is also
The attitude information of unmanned plane is sent to control circuit plate, and control circuit plate controls motor-driven propeller, and then realizes flying
Attitude stabilization during row.
Service cable includes the first service cable, the second service cable；The outfan of accumulator and the first service cable
One end is connected, and the other end of the first service cable is fixed on a reel, and reel is provided with a rotating shaft, and rotating shaft is arranged with the second confession
Electrical cables, one end of the second service cable connects described unmanned plane, and the other end of the second service cable is connected by swivel
First service cable；Rotating shaft connects a frequency conversion motor by drive disk assembly.Facilitate implementation rotating shaft in rotation process, service cable
With being connected of the power output end of accumulator.
Of the present utility model ultimate principle and principal character and of the present utility model advantage have more than been shown and described.One's own profession
Skilled person will appreciate that of industry, this utility model is not restricted to the described embodiments, described in above-described embodiment and description
Principle of the present utility model is simply described, on the premise of without departing from this utility model spirit and scope, this utility model is also
Have various changes and modifications, in the range of these changes and improvements both fall within claimed this utility model.This utility model
Claimed scope is defined by appending claims and equivalent thereof.
Claims (8)
1. wire control electric unmanned plane Vehicular solar charging system, it is characterised in that include the charging system being arranged on automobile,
Described charging system includes that a solar panel, described solar panel connect a charging module, and described charging module is even
Connecing one for storing the accumulator of electric energy, described accumulator is connected with unmanned plane by a service cable.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 1, it is characterised in that the described sun
Flexible crystalline silicon solar cell plate can be used by cell panel.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 2, it is characterised in that described flexibility
The thickness of crystal silicon solar energy battery plate is 2mm to 10mm.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 3, it is characterised in that described flexibility
The thickness of crystal silicon solar energy battery plate is 5mm.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 2, it is characterised in that described flexibility
The back side of crystal silicon solar energy battery plate is provided with one layer of adhesive-layer, and described flexible crystalline silicon solar cell plate passes through described viscose glue
Layer is bonded in automobile top.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 1, it is characterised in that described unmanned
Machine includes that a control circuit plate, described control circuit plate connect the control end of a motor, the power output shaft of described motor
Connecting propeller, described control circuit plate connects an attitude transducer.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 1, it is characterised in that described power supply
Cable includes the first service cable, the second service cable；
The outfan of described accumulator and one end of the first service cable are connected, and the other end of described first service cable is fixed on
On one reel, described reel is provided with a rotating shaft, and described rotating shaft is arranged with the second service cable, the one of described second service cable
End connects described unmanned plane, and the other end of described second service cable connects described first service cable by swivel；
Described rotating shaft connects a frequency conversion motor by drive disk assembly.
Wire control electric unmanned plane Vehicular solar charging system the most according to claim 7, it is characterised in that described rotation
Joint is a rotating Elecrical connector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620640262.9U CN205882819U (en) | 2016-06-24 | 2016-06-24 | On -vehicle solar charging system of wired electronic unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620640262.9U CN205882819U (en) | 2016-06-24 | 2016-06-24 | On -vehicle solar charging system of wired electronic unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205882819U true CN205882819U (en) | 2017-01-11 |
Family
ID=57692026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620640262.9U Expired - Fee Related CN205882819U (en) | 2016-06-24 | 2016-06-24 | On -vehicle solar charging system of wired electronic unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205882819U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107117301A (en) * | 2017-06-23 | 2017-09-01 | 杭州力谱科技有限公司 | Charging system for electric automobile |
| CN107225990A (en) * | 2017-06-14 | 2017-10-03 | 田进 | A kind of unmanned plane and its solar recharging system |
| CN108312868A (en) * | 2017-06-23 | 2018-07-24 | 杭州力谱科技有限公司 | A kind of electric car electric energy shared system |
-
2016
- 2016-06-24 CN CN201620640262.9U patent/CN205882819U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107225990A (en) * | 2017-06-14 | 2017-10-03 | 田进 | A kind of unmanned plane and its solar recharging system |
| CN107225990B (en) * | 2017-06-14 | 2019-08-16 | 广东亿航白鹭传媒科技有限公司 | A kind of unmanned plane and its solar recharging system |
| CN107117301A (en) * | 2017-06-23 | 2017-09-01 | 杭州力谱科技有限公司 | Charging system for electric automobile |
| CN108312868A (en) * | 2017-06-23 | 2018-07-24 | 杭州力谱科技有限公司 | A kind of electric car electric energy shared system |
| CN108312869A (en) * | 2017-06-23 | 2018-07-24 | 杭州力谱科技有限公司 | A kind of electric car electric energy sharing method |
| CN108312869B (en) * | 2017-06-23 | 2020-07-03 | 杭州力谱科技有限公司 | Electric vehicle electric energy sharing method |
| CN108312868B (en) * | 2017-06-23 | 2020-09-22 | 扬州港信光电科技有限公司 | Electric automobile electric energy sharing system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20190624 |