CN205891236U - Solar unmanned aerial vehicle - Google Patents
Solar unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205891236U CN205891236U CN201620873777.3U CN201620873777U CN205891236U CN 205891236 U CN205891236 U CN 205891236U CN 201620873777 U CN201620873777 U CN 201620873777U CN 205891236 U CN205891236 U CN 205891236U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- shape
- solar
- slide block
- unmanned plane
- 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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- 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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- Photovoltaic Devices (AREA)
Abstract
The utility model relates to a solar unmanned aerial vehicle, including fuselage, the wing that lies in the fuselage both sides, solar cell panel and fixed bolster, solar cell panel fixes in the fixed bolster, is equipped with the revolving stage on the fuselage, is equipped with the groove of taking in that is used for taking in solar cell panel on the revolving stage, and the middle part of taking in the groove is equipped with elevator motor, should take in groove one side side intermediate position and be equipped with the upset motor, under the fixed bolster bottom surface middle part with the top of elevator motor telescopic link is articulated, and the bottom surface is equipped with T shape spout under the fixed bolster, and T shape spout lies in upset motor below along the pin joint orientation setting of elevator motor with the fixed bolster, the top of upset motor telescopic link be equipped with with T shape spout sliding fit's T shape slider or disk slider, the telescopic link of upset motor with be hinged joint between T shape slider or the disk slider. The utility model discloses the solar energy reception is good, and realization solar panel's that can be nimble lift is receive and release, avoids the solar panel influence that flight caused to unmanned aerial vehicle under the special conditions.
Description
Technical field
This utility model is related to unmanned plane, particularly a kind of solar energy unmanned plane.
Background technology
Unmanned plane is using wireless remotecontrol or the not manned aircraft that manipulates of the presetting apparatus provided for oneself, with scientific and technological
Constantly improve, the development of unmanned air vehicle technique is more and more ripe, with more and more extensive, may not only be applied to complete battle reconnaissance and prison
Depending on, position school and penetrate, injure the military missions such as assessment, electronic warfare, but also oneself as target drone it can also be used to civilian, such as border is patrolled
Patrol, nuclear radiation detection, aeroplane photography, mineral exploration aviation, the condition of a disaster supervision, traffic patrolling, security monitoring etc..
Unmanned plane, due to needing Function Extension, just must improve overall endurance, therefore endurance is to its performance shadow
Ring greatly preferably improve at present unmanned plane endurance mode be by the wing of unmanned plane make solar panel or
Lay solar panel on wing, wing is made solar panel and generally requires very large area, cost is very high, and
On wing, laying solar panel can affect to fly again, and therefore best at present mode is to install solar energy collecting on fuselage additional
Device, but due to being limited by body, the solar panels that can install are limited, therefore in order to improve continuation of the journey effect, just required
Using solar energy tracking device.
There is high cost using solar energy tracking technology in traditional on unmanned plane, installation difficulty is big, and solar energy collecting is imitated
Really undesirable and easily cause solar panel when unmanned plane runs into vile weather damage, and in takeoff and landing
Or when execution special duty, aircraft flight speed be there are certain requirements, now this mode solar panel can affect to fly
OK.
Utility model content
The purpose of this utility model is to solve above-mentioned technical problem, provides a kind of solar energy unmanned plane, makes solar panels
Can be automatically tracked according to the trend of light, follow the movement of solar irradiation and change direction, reach the solar energy of maximum
Reception, require to combine with the concrete flight of unmanned plane simultaneously, can flexibly realize the lifting folding and unfolding of solar panels, it is to avoid
Under specific condition, solar panels cause a certain degree of impact to the flight of unmanned plane.
For solving above-mentioned technical problem, this utility model employs a kind of solar energy unmanned plane and includes fuselage, including fuselage,
Wing positioned at described fuselage both sides, solar panel and fixed support, described solar panel is fixed on described fixation
In support, wherein, described fuselage is provided with turntable, and described turntable is provided with the storage for receiving solar panel
Groove, the middle part of described accommodating groove is provided with lifting motor, and this accommodating groove side side centre position is provided with upset motor, described fixation
Hinged with the top of described lifting motor expansion link in the middle part of support bottom surface, described fixed support bottom surface is provided with t shape chute, t
Shape chute is located at below upset motor along lifting motor and the setting of support bracket fastened pin joint direction, described upset motor expansion link
Top be provided with described t shape slide cooperation t shape slide block or dish type slide block, the expansion link of described upset motor with described
It is chain connection between t shape slide block or dish type slide block.
Further, in technique scheme, in order to realize taking in fixed support to accommodating groove completely, described accommodating groove
Depth be more than described support bracket fastened thickness.
Further, in technique scheme, in order to ensure night normal work, the lower surface of described fuselage scribbles fluorescence
Material.
Further, in technique scheme, in order to ensure the smoothness slided, described t shape slide block or dish type slide block with
The surface of described t shape chute contact is arcwall face.
This utility model is had the advantages that this device can make the solar panels on unmanned plane follow solar irradiation
Movement and change direction, keep the optimal irradiating angle of sunlight, reach the maximum utilization ratio of solar energy；It is provided for receiving
Receive and solar panel can be received in it after the accommodating groove of solar panels, so can further prevent solar panel quilt
Destroy or reduce the impact to flight；The lower surface of fuselage scribbles fluorescent material, is so easy to operator and observes unmanned plane
Particular location is it is ensured that the normal work at unmanned plane night.
Brief description
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation at a in Fig. 1；
Fig. 3 is t shape slide block of the present utility model and t shape chute mating part structural representation.
Wherein: fuselage 1；Wing 2；Solar panel 3；Fixed support 4；Turntable 5；Accommodating groove 6；Lifting motor 7；Turn over
Rotating motor 8；T shape chute 9；T shape slide block 10；Arcwall face 11.
Specific embodiment
Below in conjunction with the accompanying drawings this utility model is further described.
As shown in Figures 1 to 3, this utility model provides a kind of solar energy unmanned plane, includes fuselage 1, positioned at 1 liang of described fuselage
The wing 2 of side, solar panel 3 and fixed support 4, described solar panel 3 is fixed in described fixed support 4, its
In, described fuselage 1 is provided with turntable 5, and turntable 5 can be rotated around its axis on the fuselage 1 by Motor drive, described
Turntable 5 is provided with the accommodating groove 6 for receiving solar panel 3, in order to realize taking in fixed support 4 to storage completely
Groove 6, the depth of described accommodating groove 6 is more than the thickness of described fixed support 4, and the middle part of described accommodating groove 6 is provided with lifting motor 7,
The side side centre position of this accommodating groove 6 is provided with upset motor 8, with described lifting electricity in the middle part of described fixed support 4 bottom surface
The top of machine 7 expansion link is hinged, and described fixed support 4 bottom surface is provided with t shape chute 9, and t shape chute 9 is located at below upset motor 8
Along the pin joint direction setting of lifting motor 7 and fixed support 4, the top of described upset motor 8 expansion link is provided with and described t shape
The t shape slide block 10 that chute 9 is slidably matched.In order to ensure the smoothness slided, described t shape slide block 10 is contacted with described t shape chute 9
Surface be arcwall face 11, between the expansion link of described upset motor 8 and described t shape slide block 10 be chain connection.
By upset motor 8 and lifting motor 7, adjust solar panel 6 direction and angle, keep sunlight
Good irradiating angle, reaches the maximum utilization ratio of solar energy；Require to combine with the concrete flight of unmanned plane simultaneously, Neng Gouling
The lifting folding and unfolding realizing solar panels cell panel 3 lived, it is to avoid the flight to unmanned plane for the solar panel 3 under specific condition
The impact causing；Night can send light to the fluorescent material that fuselage 1 lower surface applies again, so that operator observe the tool of unmanned plane
Body position, improves the safety of unmanned plane during flying.
Specification and drawings of the present utility model are considered as illustrative and not restrictive, on this utility model basis
On, those skilled in the art are according to disclosed technology contents it is not necessary to performing creative labour just can be to some of them technology
Feature is made some and is replaced and deform, all in protection domain of the present utility model.
Claims (4)
1. solar energy unmanned plane, the wing including fuselage, being located at described fuselage both sides, solar panel and fixed support, institute
State solar panel be fixed in described fixed support it is characterised in that: described fuselage is provided with turntable, described turntable
It is provided with the accommodating groove for receiving solar panel, the middle part of described accommodating groove is provided with lifting motor, this accommodating groove side
Side centre position is provided with upset motor, cuts with scissors with the top of described lifting motor expansion link in the middle part of described fixed support bottom surface
Connect, described fixed support bottom surface is provided with t shape chute, t shape chute is located at below upset motor along lifting motor and fixed support
The setting of pin joint direction, the top of described upset motor expansion link be provided with t shape slide block with the cooperation of described t shape slide or
Dish type slide block, is chain connection between the expansion link of described upset motor and described t shape slide block or dish type slide block.
2. solar energy unmanned plane according to claim 1 it is characterised in that: the depth of described accommodating groove be more than described fixation
The thickness of support.
3. solar energy unmanned plane according to claim 1 it is characterised in that: the lower surface of described fuselage scribbles phosphor
Material.
4. solar energy unmanned plane according to claim 1 it is characterised in that: described t shape slide block or dish type slide block and described t
The surface of shape chute contact is arcwall face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620873777.3U CN205891236U (en) | 2016-08-09 | 2016-08-09 | Solar unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620873777.3U CN205891236U (en) | 2016-08-09 | 2016-08-09 | Solar unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205891236U true CN205891236U (en) | 2017-01-18 |
Family
ID=57780886
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620873777.3U Expired - Fee Related CN205891236U (en) | 2016-08-09 | 2016-08-09 | Solar unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205891236U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107253528A (en) * | 2017-06-21 | 2017-10-17 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane with function of energy reclaiming |
| CN107963224A (en) * | 2017-11-22 | 2018-04-27 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of solar energy bird repellent unmanned plane |
| CN107972875A (en) * | 2017-11-22 | 2018-05-01 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of angle of solar cell panel regulating device of unmanned plane |
| CN118074616A (en) * | 2024-04-22 | 2024-05-24 | 陕西引汉济渭科技发展有限公司 | Photovoltaic increases journey unmanned aerial vehicle |
-
2016
- 2016-08-09 CN CN201620873777.3U patent/CN205891236U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107253528A (en) * | 2017-06-21 | 2017-10-17 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane with function of energy reclaiming |
| CN107963224A (en) * | 2017-11-22 | 2018-04-27 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of solar energy bird repellent unmanned plane |
| CN107972875A (en) * | 2017-11-22 | 2018-05-01 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of angle of solar cell panel regulating device of unmanned plane |
| CN118074616A (en) * | 2024-04-22 | 2024-05-24 | 陕西引汉济渭科技发展有限公司 | Photovoltaic increases journey unmanned aerial vehicle |
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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: 20170118 Termination date: 20210809 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |