CN203491953U - Solar energy system for unmanned plane - Google Patents
Solar energy system for unmanned plane Download PDFInfo
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- CN203491953U CN203491953U CN201320570163.4U CN201320570163U CN203491953U CN 203491953 U CN203491953 U CN 203491953U CN 201320570163 U CN201320570163 U CN 201320570163U CN 203491953 U CN203491953 U CN 203491953U
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- unmanned plane
- solar
- solar energy
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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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Abstract
The utility model provides a solar energy system for an unmanned plane; the energy system comprises a solar cell module, a power management system, a storage battery and a data converting interface; the solar cell module is formed by packaging flexible high efficiency film solar energy cell sheets, is characterized in that the solar cell module can suit flexible requirements of surface material by fuselage streamline design, and is high efficient and stable in output; the power management system is formed by an unidirectional diode, a solar energy maximum power tracking system, and a voltage stabilization chip, so the cell module can be automatically charged and controlled under low illumination; the storage battery is a high capacity lithium battery set; the independent energy system is integrated on the solar unmanned plane so as to greatly improve endurance of the unmanned plane and reduce the size of the solar unmanned plane, and can simultaneously provide long time power guarantee for other auxiliary functions of the unmanned plane, so the solar unmanned plane can be applied in many application fields.
Description
Technical field
The utility model patent relates to a kind of solar energy system for unmanned plane, the design of a kind of energy resource system of specific design, material and Research on processing technology.
Background technology
After Iraq and Afghan War, unmanned plane is familiar with by people gradually.Especially unmanned plane is through fast-developing, and after being popularized for multiple civil area, people start to pay close attention to power consumption and the flying power of unmanned plane gradually.For now, traditional unmanned plane adopts aero oil to drive, short, expensive while having boat, the defects such as M R expense height, the fields such as the investigation of having relatively high expectations in the time of cannot being applicable to boat, patrol.
The utility model patent will solve this difficult problem, new type solar energy dynamical system and type design will break through the efficiency bottle neck of unmanned plane motor 7g/w, can be when improving solar energy unmanned plane aerodynamic performance, for unmanned plane provides nexhaustible without " source " power, make the hours underway of solar energy unmanned plane extend 4-5 doubly.Believe in the situation that heliotechnics improves constantly, during the boat of solar energy unmanned plane, also will further expand.
Summary of the invention
The utility model patent provides a kind of designing technique of the solar energy system for unmanned plane;
The utility model patented technology scheme, it is characterized in that it be by thickness between 0.3mm-5mm, energy density is at the solar module between 0.1g/w-30g/w, the power-supply management system being connected with solar cell chip module, the energy storage battery being connected with power-supply management system and be integrated in change-over terminal on power-supply management system and form;
Preferably, described solar battery sheet can be the materials such as amorphous silicon (a-Si), Copper Indium Gallium Selenide (CIGS), GaAs (GaAs), and photoelectric conversion efficiency is 20%-50%, and thickness is 0.05-1mm, unit specific energy is 0.1w/g-5w/g, and bending diameter is 10mm-22mm;
Preferably, the thickness of described solar cell chip module is 0.3mm-5mm, and energy density is 0.1g/w-30g/w, and bending diameter is 10mm-22mm;
Preferably, described solar battery sheet, is characterized in that it is to carry out bending according to the airflow design structure of unmanned plane type, folding grade for operation;
Preferably, described solar battery sheet, is characterized in that it is according to model structure, cell piece array to be arranged, arrangement mode can be series connection, can be in parallel, also can connection in series-parallel and deposit, during its effect, can reach specific voltage, electric current and power requirement;
Preferably, described solar module, is characterized in that its counterdie is comprised of carbon fiber counterdie, has ability of anti-deformation, can adapt to high altitude environment;
Preferably, described carbon fiber counterdie, is characterized in that in membrane material, mixing epoxy resin is composited, have high temperature resistant, shock-resistant, the feature such as toughness is strong;
Preferably, described solar module, is characterized in that its skin covering of the surface, for high Obstruct membrane thoroughly, has increase light transmittance, intercepts hydrone, delays the functions such as assembly decay, for example etfe film;
Described power-supply management system, is comprised of unilateral diode, solar maximum power tracking system, voltage stabilizing chip etc.; It is characterized in that can low light according under charging controller to battery, can guarantee electricity generation system at any time in optimum state;
Preferably, described energy storage battery, its optimal selection is a kind of lithium battery, can be circular lithium battery, can be also flexible package lithium cell;
Preferably, described energy storage battery, is characterized in that energy density is 200wh/kg-400wh/kg, reduces it to airborne load;
Preferably, described energy storage battery connected mode can be in parallel, can be series connection, can be also connection in series-parallel and deposits;
Described change-over terminal, the port that it is characterized in that it can be the port of fixing certain model, can be also standard port, is applicable to various electronic products on UAS and the charging of energy storage battery;
The design technology project of a kind of separate energy source system for solar energy unmanned plane of the present utility model adopts innovative technology, highly effective, simple to operate, can break through the system energy technology bottleneck of current solar energy unmanned plane, extended the hours underway of solar energy unmanned plane, and promoted its range of application, there is higher social benefit, economic benefit.
Accompanying drawing explanation
The utility model provides a kind of solar energy system for unmanned plane.
Fig. 1 is the principle schematic of the solar energy system for unmanned plane.
Fig. 2 is the structural representation of the sky sun energy energy resource system for unmanned plane, wherein: 1, fuselage head solar module region; 2, wing solar module region; 3, empennage solar module region; 4, fuselage solar module region;
Fig. 3 is the schematic cross-section of the sky sun energy energy resource system for unmanned plane, wherein: 5, power-supply management system and change-over terminal; 6, energy storage battery.
Embodiment
In order to make those skilled in the art person understand better technical scheme of the present invention, and make above-mentioned purpose of the present utility model, feature and a little can more become apparent, below in conjunction with principle schematic 1 and structural representation Fig. 2, the utility model is described in further detail.
In conjunction with Fig. 1 and Fig. 2, operation principle of the present invention is described, flexible high-efficiency solar components parts 2,3,4 and 5 absorb solar energy, and its dress is changed to electric energy, by connecting line, be connected power-supply management system 6 with change-over terminal, and after processing by power-supply management system by electrical power storage in energy storage battery group 7, power-supply management system is connected with fuselage optional equipment with unmanned plane operational system with change-over terminal by data wire.Wherein, flexible high-efficiency solar components is made by carbon fiber counterdie, can be used as fuselage surface material unmanned plane frame is covered, and it is inner that power-supply management system and energy storage battery group are integrated in solar energy unmanned plane.When unmanned plane flies under illumination condition, the solar components system of fuselage is that electric energy turns round for motor and fuselage optional equipment by transform light energy, and electric energy more than needed will charge to energy storage battery simultaneously, keep whole UAS normally to move.
Claims (9)
1. the solar energy system for unmanned plane, it is characterized in that it be by thickness between 0.3mm-5mm, energy density is at the solar cell chip module between 0.1g/w-30g/w, the power-supply management system being connected with solar module, the energy storage battery being connected with power-supply management system and be integrated in change-over terminal on power-supply management system and form.
2. a kind of solar energy system for unmanned plane according to claim 1, is characterized in that cell piece in solar module can be a kind of in amorphous silicon, Copper Indium Gallium Selenide, GaAs.
3. a kind of solar energy system for unmanned plane according to claim 1, it is characterized in that the cell piece photoelectric conversion efficiency in solar module is 15%-50%, thickness is 0.05-1mm, and unit specific energy is 0.1w/g-5w/g, and bending diameter is 10mm-22mm.
4. a kind of solar energy system for unmanned plane according to claim 1, the counterdie that it is characterized in that solar module is carbon fiber material.
5. a kind of solar energy system for unmanned plane according to claim 1, is characterized in that power-supply management system is comprised of unilateral diode, solar maximum power tracking system, voltage stabilizing chip.
6. a kind of solar energy system for unmanned plane according to claim 1, is characterized in that energy storage battery energy density reaches 200wh/kg-400wh/kg.
7. a kind of solar energy system for unmanned plane according to claim 1, is characterized in that energy storage battery is a kind of in circular lithium battery, flexible package lithium cell.
8. a kind of solar energy system for unmanned plane according to claim 1, the connected mode that it is characterized in that energy storage battery is combination in parallel or series connection.
9. a kind of solar energy system for unmanned plane according to claim 1, is characterized in that its change-over terminal can be powered to various electronic, can be used as input simultaneously and charges to energy storage battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320570163.4U CN203491953U (en) | 2013-09-13 | 2013-09-13 | Solar energy system for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320570163.4U CN203491953U (en) | 2013-09-13 | 2013-09-13 | Solar energy system for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
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| CN203491953U true CN203491953U (en) | 2014-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201320570163.4U Expired - Lifetime CN203491953U (en) | 2013-09-13 | 2013-09-13 | Solar energy system for unmanned plane |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
| CN104309809A (en) * | 2014-10-23 | 2015-01-28 | 黄守瑜 | Agricultural unmanned helicopter |
| CN104810892A (en) * | 2015-05-06 | 2015-07-29 | 山东大学 | Hybrid power source system for bird-like flapping-wing air vehicle and method for hybrid power source system |
| CN105905305A (en) * | 2016-04-22 | 2016-08-31 | 中国计量大学 | Energy management system of solar unmanned aerial vehicle |
| TWI620689B (en) * | 2017-01-24 | 2018-04-11 | 林清富 | Solar cell module for unmanned aerial vehicle |
| TWI642597B (en) * | 2017-11-29 | 2018-12-01 | 英屬維爾京群島商飛思捷投資股份有限公司 | Small solar-powered unmanned aircraft |
| CN110550217A (en) * | 2019-09-21 | 2019-12-10 | 浙江驭云航空科技有限公司 | Unmanned aerial vehicle's extension continuation of journey device |
-
2013
- 2013-09-13 CN CN201320570163.4U patent/CN203491953U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103840745A (en) * | 2013-09-13 | 2014-06-04 | 武汉美格科技有限公司 | Solar energy system for unmanned plane to use |
| CN104309809A (en) * | 2014-10-23 | 2015-01-28 | 黄守瑜 | Agricultural unmanned helicopter |
| CN104810892A (en) * | 2015-05-06 | 2015-07-29 | 山东大学 | Hybrid power source system for bird-like flapping-wing air vehicle and method for hybrid power source system |
| CN105905305A (en) * | 2016-04-22 | 2016-08-31 | 中国计量大学 | Energy management system of solar unmanned aerial vehicle |
| TWI620689B (en) * | 2017-01-24 | 2018-04-11 | 林清富 | Solar cell module for unmanned aerial vehicle |
| TWI642597B (en) * | 2017-11-29 | 2018-12-01 | 英屬維爾京群島商飛思捷投資股份有限公司 | Small solar-powered unmanned aircraft |
| US10974828B2 (en) * | 2017-11-29 | 2021-04-13 | Psj International Ltd. | Small solar-powered unmanned aircraft |
| CN110550217A (en) * | 2019-09-21 | 2019-12-10 | 浙江驭云航空科技有限公司 | Unmanned aerial vehicle's extension continuation of journey device |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP02 | Change in the address of a patent holder |
Address after: 430206, No. 10, hi tech Road, East Lake hi tech Zone, Hubei, Wuhan, A, building 999, overseas talent building, Wuhan future science and Technology City Patentee after: FLEXTECH Co. Address before: 430206, No. 999, hi tech Road, Dongxihu hi tech Zone, Hubei, Wuhan, No. 10, building 4, block A, future science and Technology City Patentee before: FLEXTECH Co. |
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| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 430206, No. 10, hi tech Road, East Lake hi tech Zone, Hubei, Wuhan, A, building 999, overseas talent building, Wuhan future science and Technology City Patentee after: FLEXTECH CO. Address before: 430206, No. 10, hi tech Road, East Lake hi tech Zone, Hubei, Wuhan, A, building 999, overseas talent building, Wuhan future science and Technology City Patentee before: FLEXTECH Co. |
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| CX01 | Expiry of patent term |
Granted publication date: 20140319 |
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| CX01 | Expiry of patent term |