CN103803085A - Solar cell rotorcraft based on Fresnel lens - Google Patents
Solar cell rotorcraft based on Fresnel lens Download PDFInfo
- Publication number
- CN103803085A CN103803085A CN201210462501.2A CN201210462501A CN103803085A CN 103803085 A CN103803085 A CN 103803085A CN 201210462501 A CN201210462501 A CN 201210462501A CN 103803085 A CN103803085 A CN 103803085A
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- CN
- China
- Prior art keywords
- cyclogyro
- fresnel lenses
- solar cell
- fresnel lens
- rotorcraft
- 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.)
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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
- Y02E10/52—PV systems with concentrators
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- Photovoltaic Devices (AREA)
Abstract
The invention relates to a solar cell rotorcraft based on a Fresnel lens, comprising a rotorcraft and a Fresnel lens solar system arranged on the upper part of the rotorcraft. The efficient flight of the rotorcraft is realized by means of high efficiency of the Fresnel lens solar system.
Description
Technical field
The invention belongs to cyclogyro field.
Background technology
Cyclogyro adopts oil moving or electronic mostly, also has employing solar powered, but all adopts flat-plate type solar cell, under efficiency, can not meet cyclogyro and use.
Summary of the invention
Shortcoming while utilizing solar power for solving existing cyclogyro under efficiency, the invention provides a kind of solar cell cyclogyro based on Fresnel Lenses, has advantages of that conversion efficiency is high.
Technical solution of the present invention is as follows:
A kind of solar cell cyclogyro based on Fresnel Lenses, comprise cyclogyro, its special character is, also comprise the Fresnel Lenses solar energy system that is arranged on cyclogyro waist, described Fresnel Lenses solar energy system comprises Fresnel Lenses and is positioned at the solar cell of Fresnel Lenses below; The two ends of described Fresnel Lenses are no more than cyclogyro frame.
Beneficial effect of the present invention:
1, the present invention adopts Fresnel Lenses solar energy system, and conversion efficiency is high, can meet cyclogyro and use.
2, the two ends of Fresnel Lenses of the present invention are no more than cyclogyro frame, can guarantee the balance of fuselage.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is Fresnel Lenses solar energy system structural representation;
Wherein: 11-cyclogyro, 12-rotor, 31-solar cell, 32-Fresnel Lenses.
The specific embodiment
As depicted in figs. 1 and 2, the present invention is based on the solar cell cyclogyro of Fresnel Lenses, comprise cyclogyro, be arranged on the Fresnel Lenses solar energy system of cyclogyro waist, Fresnel Lenses solar energy system comprises Fresnel Lenses and is positioned at the solar cell of Fresnel Lenses below; The two ends of described Fresnel Lenses are no more than cyclogyro frame.Continue, to electric engine power supply, can meet cyclogyro long-distance flight requirement by solar cell.
Claims (1)
1. the solar cell cyclogyro based on Fresnel Lenses, comprise cyclogyro, it is characterized in that, also comprise the Fresnel Lenses solar energy system that is arranged on cyclogyro waist, described Fresnel Lenses solar energy system comprises Fresnel Lenses and is positioned at the solar cell of Fresnel Lenses below; The two ends of described Fresnel Lenses are no more than cyclogyro frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210462501.2A CN103803085A (en) | 2012-11-15 | 2012-11-15 | Solar cell rotorcraft based on Fresnel lens |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210462501.2A CN103803085A (en) | 2012-11-15 | 2012-11-15 | Solar cell rotorcraft based on Fresnel lens |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103803085A true CN103803085A (en) | 2014-05-21 |
Family
ID=50700576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210462501.2A Withdrawn CN103803085A (en) | 2012-11-15 | 2012-11-15 | Solar cell rotorcraft based on Fresnel lens |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103803085A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104309801A (en) * | 2014-09-26 | 2015-01-28 | 金陵科技学院 | Rotary wing type unmanned plane with spherical solar collector at central section and landing seat thereof |
| CN113788136A (en) * | 2021-11-10 | 2021-12-14 | 中国空气动力研究与发展中心低速空气动力研究所 | Center shaft ventilation and light condensation airship |
-
2012
- 2012-11-15 CN CN201210462501.2A patent/CN103803085A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104309801A (en) * | 2014-09-26 | 2015-01-28 | 金陵科技学院 | Rotary wing type unmanned plane with spherical solar collector at central section and landing seat thereof |
| CN104309801B (en) * | 2014-09-26 | 2016-02-03 | 金陵科技学院 | A kind of middle part is rotary wind type unmanned plane and the landing seat thereof of spherical solar catcher |
| CN113788136A (en) * | 2021-11-10 | 2021-12-14 | 中国空气动力研究与发展中心低速空气动力研究所 | Center shaft ventilation and light condensation airship |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20140521 |