CN205203398U - Single rotor unmanned aerial vehicle solar charging device - Google Patents
Single rotor unmanned aerial vehicle solar charging device Download PDFInfo
- Publication number
- CN205203398U CN205203398U CN201520643735.6U CN201520643735U CN205203398U CN 205203398 U CN205203398 U CN 205203398U CN 201520643735 U CN201520643735 U CN 201520643735U CN 205203398 U CN205203398 U CN 205203398U
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- CN
- China
- Prior art keywords
- fuselage
- solar cell
- balance adjustment
- adjustment frame
- aerial vehicle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a single rotor unmanned aerial vehicle solar charging device, the device installs on the fuselage, both ends are equipped with equipment respectively and carry on frame and fin around the fuselage, its inside fuselage battery that is equipped with, the device includes a balance adjustment frame, solar cell and carriage, the top at the fin is fixed to balance adjustment frame horizontally, its one end and fuselage fixed connection, its other end is connected with the fin through a connecting plate, solar cell installs on the carriage, the carriage cover is established on the balance adjustment frame, and with balance adjustment frame sliding connection, wherein, solar cell includes panel and bottom plate, the panel is connected with the carriage, the bottom plate is connected with the fuselage battery through a lead wire. The utility model discloses a solar cell has played the effect that quick adjustment is balanced, and simultaneously, solar cell charges to the fuselage battery under no external power supply's the circumstances, has lengthened the time of endurance of fuselage battery.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, particularly relates to a kind of single rotor wing unmanned aerial vehicle solar charging device.
Background technology
At present, general single rotor monitoring unmanned plane is all use storage battery to provide electric energy for unmanned plane, quite waste energy, before use storage battery is charged, because the electricity of storage battery is limited, can not long-time continuous carry out policer operation, otherwise it is not enough just may to appear in flight course electricity, causes the situations such as unmanned plane crash to occur.And the digital camera that single rotor wing unmanned aerial vehicle carries when performing monitor task or pick up camera, all can affect the center-of-gravity position of single rotor wing unmanned aerial vehicle, thus balance when can affect unmanned plane during flying.
Utility model content
The utility model mainly solves technical matters existing in prior art, thus provides a kind of charging convenience, battery durable ability high and the simple single rotor wing unmanned aerial vehicle solar charging device of adjustment.
Above-mentioned technical matters of the present utility model is mainly solved by following technical proposals:
Single rotor wing unmanned aerial vehicle solar charging device that the utility model provides, this device is arranged on fuselage, the rear and front end of described fuselage is respectively equipped with equipment and carries frame and empennage, its inside is provided with fuselage battery, this device comprises a balance adjustment frame, solar cell and sliding rack, the top being fixed on described empennage of described balance adjustment frame level, its one end is fixedly connected with described fuselage, its other end is connected with described empennage by a plate, described solar cell is arranged on described sliding rack, described sliding rack is set on described balance adjustment frame, and with described balance adjustment frame sliding block joint, wherein, described solar cell comprises panel and base plate, described panel is connected with described sliding rack, described base plate is connected with described fuselage battery by a lead-in wire.
Further, also comprise a penetration pipe, described penetration pipe is positioned at the below of solar cell, and is fixedly connected with described fuselage, and described lead-in wire is located in described penetration pipe.
Further, the outside of described penetration pipe is also provided with spring protecting jacket.
Further, the top of described balance adjustment frame is gone up along its length and is also provided with graduation apparatus.
Further, described sliding rack is also provided with a lock bolt, described lock bolt is for locking described sliding rack.
The beneficial effects of the utility model are: be fixed on balance adjustment frame by being slided by solar cell, change the position of solar cell on balance adjustment frame, change the moment of back body empennage, the equipment hold torque that itself and forebody carry is balanced, make solar cell serve the effect of quick adjustment balance, meanwhile, solar cell is when without external source, fuselage battery is charged, extends the cruise duration of fuselage battery.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of single rotor wing unmanned aerial vehicle solar charging device of the present utility model.
Fig. 2 is the partial enlarged drawing of Fig. 1.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Consult shown in Fig. 1, single rotor wing unmanned aerial vehicle solar charging device of the present utility model, this device is installed on the fuselage 1, the rear and front end of fuselage 1 is respectively equipped with equipment and carries frame 2 and empennage 3, its inside is provided with fuselage battery 13, this device comprises a balance adjustment frame 4, solar cell 5 and sliding rack 6, the top being fixed on empennage 3 of balance adjustment frame 4 level, its one end is fixedly connected with fuselage 1, its other end is connected with empennage 3 by a plate 7, solar cell 5 is arranged on sliding rack 6, sliding rack 6 is set on balance adjustment frame 4, and with balance adjustment frame 4 sliding block joint, wherein, solar cell 5 comprises panel 8 and base plate 9, panel is connected with sliding rack 6, base plate 9 is connected with fuselage battery 13 by a lead-in wire 14.The utility model is fixed on balance adjustment frame 4 by being slided by solar cell 5, change the position of solar cell 5 on balance adjustment frame 4, change the moment of back body empennage, the equipment hold torque that itself and forebody carry is balanced, make solar cell 5 serve the effect of quick adjustment balance, meanwhile, solar cell 5 is when without external source, fuselage battery 13 is charged, extends the cruise duration of fuselage battery 13.
Concrete, also comprise a penetration pipe 15, penetration pipe 15 is positioned at the below of solar cell 5, and is fixedly connected with fuselage 1, and lead-in wire 14 is located in penetration pipe 15.Protected by penetration pipe 15 and guide lead-in wire 14, avoiding lead-in wire 14 discretionary wiring (method) to cause being wound around with fuselage 1.Preferably, the outside of penetration pipe 15 is being regulated also to be provided with spring protecting jacket 11.When solar cell 5 slides along balance adjustment frame 4, spring protecting jacket 11, for the protection of lead-in wire 14, is avoided breaking lead-in wire 14.
Concrete, conveniently theory calculate and quick adjusting regulate the position of counterweight 5, and the top of balance adjustment frame 4 is gone up along its length and is also provided with graduation apparatus 10.Sliding rack 6 is also provided with a lock bolt 12, lock bolt 12 is for locking sliding rack 6.
Above, be only detailed description of the invention of the present utility model, but protection domain of the present utility model is not limited thereto, any change of expecting without creative work or replacement, all should be encompassed within protection domain of the present utility model.Therefore, the protection domain that protection domain of the present utility model should limit with claims is as the criterion.
Claims (5)
1. a single rotor wing unmanned aerial vehicle solar charging device, this device is arranged on fuselage (1), the rear and front end of described fuselage (1) is respectively equipped with equipment and carries frame (2) and empennage (3), its inside is provided with fuselage battery (13), it is characterized in that: this device comprises a balance adjustment frame (4), solar cell (5) and sliding rack (6), the top being fixed on described empennage (3) of described balance adjustment frame (4) level, its one end is fixedly connected with described fuselage (1), its other end is connected with described empennage (3) by a plate (7), described solar cell (5) is arranged on described sliding rack (6), described sliding rack (6) is set on described balance adjustment frame (4), and with described balance adjustment frame (4) sliding block joint, wherein, described solar cell (5) comprises panel (8) and base plate (9), described panel is connected with described sliding rack (6), described base plate (9) is connected with described fuselage battery (13) by a lead-in wire (14).
2. single rotor wing unmanned aerial vehicle solar charging device as claimed in claim 1, it is characterized in that: also comprise a penetration pipe (15), described penetration pipe (15) is positioned at the below of solar cell (5), and be fixedly connected with described fuselage (1), described lead-in wire (14) is located in described penetration pipe (15).
3. single rotor wing unmanned aerial vehicle solar charging device as claimed in claim 2, is characterized in that: the outside of described penetration pipe (15) is also provided with spring protecting jacket (11).
4. single rotor wing unmanned aerial vehicle solar charging device as claimed in claim 3, is characterized in that: the top of described balance adjustment frame (4) is gone up along its length and is also provided with graduation apparatus (10).
5. single rotor wing unmanned aerial vehicle solar charging device as claimed in claim 1, it is characterized in that: described sliding rack (6) is also provided with a lock bolt (12), described lock bolt (12) is for locking described sliding rack (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520643735.6U CN205203398U (en) | 2015-08-24 | 2015-08-24 | Single rotor unmanned aerial vehicle solar charging device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520643735.6U CN205203398U (en) | 2015-08-24 | 2015-08-24 | Single rotor unmanned aerial vehicle solar charging device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205203398U true CN205203398U (en) | 2016-05-04 |
Family
ID=55841130
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520643735.6U Expired - Fee Related CN205203398U (en) | 2015-08-24 | 2015-08-24 | Single rotor unmanned aerial vehicle solar charging device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205203398U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106314793A (en) * | 2016-08-31 | 2017-01-11 | 甘勍 | Multifunctional UAV (unmanned aerial vehicle) |
| CN106452556A (en) * | 2016-09-14 | 2017-02-22 | 芜湖扬展新材料科技服务有限公司 | Data transmission system for aircraft based on 4G network |
-
2015
- 2015-08-24 CN CN201520643735.6U patent/CN205203398U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106314793A (en) * | 2016-08-31 | 2017-01-11 | 甘勍 | Multifunctional UAV (unmanned aerial vehicle) |
| CN106452556A (en) * | 2016-09-14 | 2017-02-22 | 芜湖扬展新材料科技服务有限公司 | Data transmission system for aircraft based on 4G network |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160504 Termination date: 20160824 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |