CN105501432A - Solar integrated drone aircraft wing - Google Patents
Solar integrated drone aircraft wing Download PDFInfo
- Publication number
- CN105501432A CN105501432A CN201510853267.XA CN201510853267A CN105501432A CN 105501432 A CN105501432 A CN 105501432A CN 201510853267 A CN201510853267 A CN 201510853267A CN 105501432 A CN105501432 A CN 105501432A
- Authority
- CN
- China
- Prior art keywords
- fin
- unmanned plane
- wing panel
- solar
- wing
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/34—In-flight charging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses a solar integrated drone aircraft wing, which comprises a first wing panel, an intermediate wing panel and a second wing panel. The first and second wing panels are hinged to the intermediate wing panel through a pivot. The first wing panel, the intermediate wing panel and the second wing panel are all provided with solar cell panels. The solar cell panels, the first wing panel, the second wing panel and the intermediate wing panel are integrated as a whole. Through the above mode, mass of a drone aircraft can be reduced by the use of the solar integrated drone aircraft wing, flight speed of the drone aircraft is raised, absorption area of solar and light energy is increased, large area of absorbing sunlight is guaranteed, and conversion efficiency of solar energy and light energy is greatly raised.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to a kind of solar power integral type unmanned plane wing.
Background technology
Unmanned plane is the not manned aircraft utilizing radio robot and the process controller provided for oneself to handle, at present taking photo by plane, agricultural plant protection, the field such as mapping have a wide range of applications.
Current unmanned plane during flying needs to consume a large amount of oil equal energy sources, also increases the weight of unmanned plane self on the one hand, also creates the waste of the energy on the other hand.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of solar power integral type unmanned plane wing, the quality of unmanned plane can be alleviated, improve the flying speed of unmanned plane, add the absorption area of solar power luminous energy, ensure that there is the larger area being photographed sunlight, substantially increase the conversion efficiency of solar power luminous energy, decrease the excessive use of the energy.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of solar power integral type unmanned plane wing, comprise the first fin, intermediate fins and the second fin, described first fin and the second fin are by pivot and the hinged setting of intermediate fins, described first fin, the second fin and intermediate fins are all provided with solar panel, and described solar panel and the first fin, the second fin and intermediate fins are formed in one and arrange.
In a preferred embodiment of the present invention, described solar panel covers all surfaces of the first fin, the second fin and intermediate fins.
In a preferred embodiment of the present invention, described solar panel is linked together by serial or parallel connection mode.
In a preferred embodiment of the present invention, described solar panel and the first fin, between the second fin and intermediate fins for be electrically connected.
In a preferred embodiment of the present invention, described first fin, intermediate fins and the second fin adopt light material to make.
The invention has the beneficial effects as follows: solar power integral type unmanned plane wing of the present invention can alleviate the quality of unmanned plane, improve the flying speed of unmanned plane, add the absorption area of solar power luminous energy, ensure that there is the larger area being photographed sunlight, substantially increase the conversion efficiency of solar power luminous energy, decrease the excessive use of the energy.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, 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, wherein:
Fig. 1 is the structural representation of solar power integral type unmanned plane wing one of the present invention preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, the first fin, and 2, intermediate fins, the 3, second fin, 4, pivot, 5, solar panel.
Detailed description of the invention
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1, the embodiment of the present invention comprises:
A kind of solar power integral type unmanned plane wing, comprises the first fin 1, intermediate fins 2 and the second fin 3, and described first fin 1 and the second fin 3 are by pivot 4 and the hinged setting of intermediate fins 2.
Described first fin 1, intermediate fins 2 and the second fin 3 adopt light material to make, and can alleviate the quality of unmanned plane, greatly improve the flying speed of unmanned plane.
Described first fin 1, second fin 2 and intermediate fins 3 are all provided with solar panel 5, and described solar panel 5 is linked together by serial or parallel connection mode.
Described solar panel 5 and the first fin 1, second fin 2 and intermediate fins 3 are formed in one and arrange, and reduce further the quality of unmanned plane on the one hand, too increase the absorption area of solar power luminous energy on the other hand.
Described solar panel 5 covers all surfaces of the first fin 1, second fin 3 and intermediate fins 2, ensures to have the larger area being photographed sunlight, substantially increases the conversion efficiency of solar power luminous energy.
Described solar panel 5 and between the first fin 1, second fin 3 and intermediate fins 2 for be electrically connected, facilitate conversion quality and the conversion efficiency of photoelectricity.
The beneficial effect of solar power integral type unmanned plane wing of the present invention is:
The quality of unmanned plane can be alleviated, improve the flying speed of unmanned plane, add the absorption area of solar power luminous energy, ensure that there is the larger area being photographed sunlight, substantially increase the conversion efficiency of solar power luminous energy, decrease the excessive use of the energy.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.
Claims (5)
1. a solar power integral type unmanned plane wing, comprise the first fin, intermediate fins and the second fin, described first fin and the second fin are by pivot and the hinged setting of intermediate fins, it is characterized in that, described first fin, the second fin and intermediate fins are all provided with solar panel, and described solar panel and the first fin, the second fin and intermediate fins are formed in one and arrange.
2. solar power integral type unmanned plane wing according to claim 1, it is characterized in that, described solar panel covers all surfaces of the first fin, the second fin and intermediate fins.
3. solar power integral type unmanned plane wing according to claim 1, it is characterized in that, described solar panel is linked together by serial or parallel connection mode.
4. solar power integral type unmanned plane wing according to claim 1, is characterized in that, described solar panel and the first fin, between the second fin and intermediate fins for be electrically connected.
5. solar power integral type unmanned plane wing according to claim 1, is characterized in that, described first fin, intermediate fins and the second fin adopt light material to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510853267.XA CN105501432A (en) | 2015-11-30 | 2015-11-30 | Solar integrated drone aircraft wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510853267.XA CN105501432A (en) | 2015-11-30 | 2015-11-30 | Solar integrated drone aircraft wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105501432A true CN105501432A (en) | 2016-04-20 |
Family
ID=55709839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510853267.XA Pending CN105501432A (en) | 2015-11-30 | 2015-11-30 | Solar integrated drone aircraft wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105501432A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1420829A (en) * | 2000-02-14 | 2003-05-28 | 威罗门飞行公司 | Aircraft |
| CN101254753A (en) * | 2007-02-28 | 2008-09-03 | 西北工业大学 | Solar pilotless plane |
| US20120091263A1 (en) * | 2007-09-14 | 2012-04-19 | Aurora Flight Sciences Corporation | Method of operating a solar aircraft |
| CN103332290A (en) * | 2013-05-28 | 2013-10-02 | 北京航空航天大学 | Wing structure-solar cell integrated module and development method thereof |
| WO2015050609A2 (en) * | 2013-07-10 | 2015-04-09 | Google Inc. | High altitude aircraft with integrated solar cells, and associated systems and methods |
-
2015
- 2015-11-30 CN CN201510853267.XA patent/CN105501432A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1420829A (en) * | 2000-02-14 | 2003-05-28 | 威罗门飞行公司 | Aircraft |
| CN101254753A (en) * | 2007-02-28 | 2008-09-03 | 西北工业大学 | Solar pilotless plane |
| US20120091263A1 (en) * | 2007-09-14 | 2012-04-19 | Aurora Flight Sciences Corporation | Method of operating a solar aircraft |
| CN103332290A (en) * | 2013-05-28 | 2013-10-02 | 北京航空航天大学 | Wing structure-solar cell integrated module and development method thereof |
| WO2015050609A2 (en) * | 2013-07-10 | 2015-04-09 | Google Inc. | High altitude aircraft with integrated solar cells, and associated systems and methods |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160420 |
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| WD01 | Invention patent application deemed withdrawn after publication |