CN204956898U - Light and handy type solar energy unmanned aerial vehicle - Google Patents
Light and handy type solar energy unmanned aerial vehicle Download PDFInfo
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- CN204956898U CN204956898U CN201520660467.9U CN201520660467U CN204956898U CN 204956898 U CN204956898 U CN 204956898U CN 201520660467 U CN201520660467 U CN 201520660467U CN 204956898 U CN204956898 U CN 204956898U
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model discloses a light and handy type solar energy unmanned aerial vehicle, including aircraft nose, camera, solar cell panel, first quick -witted wall, fixed connection board and second machine wall, the camera is located one side lower extreme of first quick -witted wall, the front end of first quick -witted wall is equipped with the aircraft nose, the both ends of fixed connection board are connected with first quick -witted wall and second machine wall, solar cell panel is installed to the centre of first quick -witted wall and second machine wall, be equipped with the air jet in the middle of the lower extreme of first quick -witted wall and second machine wall. This unmanned aerial vehicle simple structure just can use through simple equipment, and the fuselage adopts skeleton construction basically, is favorable to light and handy flight, installs solar cell panel on the fuselage, can be effectual improvement unmanned aerial vehicle's duration, solve the short problem of current unmanned aerial vehicle time of endurance to through setting up the effectual materials used of having saved of first quick -witted wall and second machine wall, resources are saved.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, is specially a kind of legerity type solar power unmanned plane.
Background technology
Along with the development of state-of-art, unmanned plane have also been obtained fast development, current unmanned plane has been applied to some aspect of life, city and countryside, all change in the appearance because of unmanned plane, if live in rural area, you can exclaim in unmanned plane in the transport capacity promoting remote districts and the outstanding performance improved in agricultural production efficiency, if as a member in city, you also can be pleasantly surprised see that unmanned plane is solving the effect of non-same common music in tortoise speed logistics and urban planning and development control, the epoch in the world are engulfed in this technology, unmanned plane as air all-pervasive penetrate in daily life, in the big city that the crowd is crowded, and the rural area of the other end, but the unmanned plane efficiency used at present is comparatively low, structure is comparatively complicated, can not well for people use, we devise a kind of legerity type solar power unmanned plane for this reason, be used for solving the problem.
Utility model content
The purpose of this utility model is to provide a kind of legerity type solar power unmanned plane, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme: a kind of legerity type solar power unmanned plane, comprise head, camera, solar panel, first machine wall, fixed connecting plate and the second machine wall, described camera is positioned at the lower end, side of the first machine wall, the front end of described first machine wall is provided with head, the two ends of described fixed connecting plate are connected with the first machine wall and the second machine wall, the centre of described first machine wall and the second machine wall is provided with solar panel, air nozzle is provided with in the middle of the lower end of described first machine wall and the second machine wall, the both sides, lower end of described first machine wall and the second machine wall are equipped with expansion link, the lower end of described expansion link is provided with base, the rear end of described second machine wall is provided with sliding block joint arm, described sliding block joint arm is provided with tail away from the side of the second machine wall, the rear end of described tail is provided with the wind-guiding wing.
Preferably, described solar panel adopts detachable installation.
Preferably, the described wind-guiding wing adopts the rotary type wind wing.
Preferably, the lower end of described base is provided with convex surface.
Compared with prior art, the beneficial effects of the utility model are: this unmanned plane structure is simple, just can use by simply assembling, fuselage adopts skeleton structure substantially, is conducive to light and handy flight, fuselage is provided with solar panel, the flying power of unmanned plane can be improved by actv., solve short problem in existing unmanned plane cruise duration, and by arranging the first machine wall and the second machine wall actv. saves use material, economize on resources.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Fig. 2 is the utility model bottom construction schematic diagram.
In figure: 1 head, 2 cameras, 3 solar panels, 4 first machine walls, 5 fixed connecting plates, 6 second machine walls, 7 sliding block joint arms, 8 tails, the 9 wind-guiding wings, 10 air nozzles, 11 expansion links, 12 bases.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1-2, the utility model provides a kind of technical scheme: a kind of legerity type solar power unmanned plane, comprise head 1, camera 2, solar panel 3, first machine wall 4, fixed connecting plate 5 and the second machine wall 6, camera 2 is positioned at the lower end, side of the first machine wall 4, for shooting, the front end of the first machine wall 4 is provided with head 1, the two ends of fixed connecting plate 5 are connected with the first machine wall 4 and the second machine wall 6, made more firm between the two by the connection of fixed connecting plate 5, the centre of the first machine wall 4 and the second machine wall 6 is provided with solar panel 3, for unmanned plane provides power, solar panel 3 adopts detachable installation, person's operation more convenient to use, air nozzle 10 is provided with in the middle of the lower end of the first machine wall 4 and the second machine wall 6, for promoting unmanned plane during flying, the both sides, lower end of the first machine wall 4 and the second machine wall 6 are equipped with expansion link 11, the lower end of expansion link 11 is provided with base 12, the lower end of base 12 is provided with convex surface, increasing friction force, the rear end of the second machine wall 6 is provided with sliding block joint arm 7, can conditioner body structure by sliding block joint arm 7 transform length, sliding block joint arm 7 is provided with tail 8 away from the side of the second machine wall 6, the rear end of tail 8 is provided with the wind-guiding wing 9, the wind-guiding wing 9 adopts the rotary type wind wing, for guiding wind direction.
The above; be only the utility model preferably detailed description of the invention; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; be equal to according to the technical solution of the utility model and improvement design thereof and replace or change, all should be encompassed in protection domain of the present utility model.
Claims (4)
1. a legerity type solar power unmanned plane, comprise head (1), camera (2), solar panel (3), first machine wall (4), fixed connecting plate (5) and the second machine wall (6), described camera (2) is positioned at the lower end, side of the first machine wall (4), it is characterized in that: the front end of described first machine wall (4) is provided with head (1), the two ends of described fixed connecting plate (5) are connected with the first machine wall (4) and the second machine wall (6), the centre of described first machine wall (4) and the second machine wall (6) is provided with solar panel (3), air nozzle (10) is provided with in the middle of the lower end of described first machine wall (4) and the second machine wall (6), the both sides, lower end of described first machine wall (4) and the second machine wall (6) are equipped with expansion link (11), the lower end of described expansion link (11) is provided with base (12), the rear end of described second machine wall (6) is provided with sliding block joint arm (7), described sliding block joint arm (7) is provided with tail (8) away from the side of the second machine wall (6), the rear end of described tail (8) is provided with the wind-guiding wing (9).
2. a kind of legerity type solar power unmanned plane according to claim 1, is characterized in that: described solar panel (3) adopts screw threads for fastening.
3. a kind of legerity type solar power unmanned plane according to claim 1, is characterized in that: the described wind-guiding wing (9) adopts the rotation type wind wing.
4. a kind of legerity type solar power unmanned plane according to claim 1, is characterized in that: the lower end of described base (12) is provided with convex surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520660467.9U CN204956898U (en) | 2015-08-30 | 2015-08-30 | Light and handy type solar energy unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520660467.9U CN204956898U (en) | 2015-08-30 | 2015-08-30 | Light and handy type solar energy unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204956898U true CN204956898U (en) | 2016-01-13 |
Family
ID=55051979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520660467.9U Active CN204956898U (en) | 2015-08-30 | 2015-08-30 | Light and handy type solar energy unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204956898U (en) |
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2015
- 2015-08-30 CN CN201520660467.9U patent/CN204956898U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wei Yichao Inventor before: Xu Yuemiao |
|
| COR | Change of bibliographic data | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160406 Address after: 310052 Binjiang District, Hangzhou, Xincheng Road, No. 307, room 2, building 33 Patentee after: HANGZHOU PINNET TECHNOLOGIES CO., LTD. Address before: 311815 Zhuji City, Zhejiang Province, the second town, No., No. 182 Patentee before: Xu Yuemiao |