CN204906259U - Solar array power generation system and aerostatics device - Google Patents

Solar array power generation system and aerostatics device Download PDF

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Publication number
CN204906259U
CN204906259U CN201520657103.5U CN201520657103U CN204906259U CN 204906259 U CN204906259 U CN 204906259U CN 201520657103 U CN201520657103 U CN 201520657103U CN 204906259 U CN204906259 U CN 204906259U
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solar array
intensity
aerostatics
sun sensor
illumination
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CN201520657103.5U
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不公告发明人
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Dongguan Dongguan Institute Of Science And Technology Innovation
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Dongguan Frontier Technology Institute
Shenzhen Kuang Chi Space Technology Co Ltd
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy

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Abstract

The utility model provides a solar array power generation system and aerostatics device, this system includes: sun sensor, solar array, wherein, the plane is set to on solar array's surface, the driver part is connected with solar array and sun sensor, and when the driver part lay in the primary importance, solar array lay in the second place, and wherein, when solar array was in the second place, solar array received an illumination intensity, when the control signal of driver part response sun sensor output drove the third position from the primary importance, solar array was driven the fourth position from the second place, and wherein, when solar array was in the fourth position, solar array received the 2nd illumination intensity, and wherein, the 2nd illumination intensity is greater than an illumination intensity. Through the utility model discloses, solar array has been solved in the correlation technique under the condition that the Sun's rays can not penetrate directly, problem that the generating efficiency is low.

Description

Solar array electricity generation system and aerostatics device
Technical field
The utility model relates to field of solar energy, in particular to a kind of solar array electricity generation system and aerostatics device.
Background technology
Solar cell, also known as photocell, is the optoelectronic semiconductor thin slice utilizing the sunlight direct generation of electricity, and solar cell can generation current when being arrived by illumination.
Here it should be noted that, what solar cell only had just can be reached maximum generating efficiency by under the condition of sun direct projection, and under the condition of non-solar light direct beam, generating efficiency can reduce.In the solar cell of all multiple types, Monocrystalline silicon cell piece photovoltaic efficiency is the highest, but Monocrystalline silicon cell piece low light level poor performance, namely must have sunlight direct projection, if sunlight can not direct projection when, monocrystalline silicon battery battle array cannot generate electricity.
For solar array in correlation technique when sunray can not direct projection, the problem that generating efficiency is low, not yet proposes effective solution at present.
Utility model content
Main purpose of the present utility model is to provide a kind of solar array electricity generation system and aerostatics device, with to solve in correlation technique solar array when sunray can not direct projection, the problem that generating efficiency is low.
To achieve these goals, a kind of solar array electricity generation system is provided.This system comprises: sun sensor; Solar array, wherein, plane is arranged on the surface of solar array; Driver part, is connected with solar array and sun sensor, and when driver part is positioned at primary importance, solar array is positioned at the second place, and wherein, when solar array is in the second place, solar array receives the first intensity of illumination; When the control signal that driver part response sun sensor exports is driven into the 3rd position from primary importance, solar array is driven to the 4th position from the second place, wherein, when solar array is in the 4th position, solar array receives the second intensity of illumination, wherein, the second intensity of illumination is greater than the first intensity of illumination.
Further, rotating parts, is connected with solar array, and wherein, when rotating parts rotates motion, rotating parts drives solar array to rotate around the vertical symmetry axis of solar array.
Further, the shape of sun sensor is N prism, and wherein, each side of N prism is provided with an optical sensor, wherein, N be more than or equal to 3 natural number.
Further, N number of side of N prism is parallel to the rotating shaft of rotating parts.
Further, when solar array is in the 4th position, solar array is parallel with the first side of N prism, wherein, and the Intensity of the sunlight that other side that the Intensity of the sunlight that the first side receives is greater than N prism receives.
Further, this system also comprises: electric pressure converter, and wherein, electric pressure converter comprises: input, is connected with solar array; Output, for export the electric energy that solar array is produced carry out voltage transitions after the signal of telecommunication that obtains.
Further, energy-storage battery is lithium-ion energy storage battery.
According to another aspect of the present utility model, also provide a kind of aerostatics device.This aerostatics device comprises: aerostatics, for providing buoyancy lift; Gondola, hangs on the below of aerostatics; And above-mentioned any one solar array electricity generation system; Wherein, sun sensor and solar array are arranged at the outside of gondola.
Further, sun sensor is arranged at the top of gondola.
Further, solar array hangs on the below of gondola.
According to utility model embodiment, solar array electricity generation system comprises: sun sensor; Solar array, wherein, plane is arranged on the surface of solar array; Driver part, is connected with solar array and sun sensor, and when driver part is positioned at primary importance, solar array is positioned at the second place, and wherein, when solar array is in the second place, solar array receives the first intensity of illumination; When the control signal that driver part response sun sensor exports is driven into the 3rd position from primary importance, solar array is driven to the 4th position from the second place, wherein, when solar array is in the 4th position, solar array receives the second intensity of illumination, wherein, the second intensity of illumination is greater than the first intensity of illumination.By the utility model, to solve in correlation technique solar array when sunray can not direct projection, the problem that generating efficiency is low.
Accompanying drawing explanation
The accompanying drawing forming a application's part is used to provide further understanding of the present utility model, and schematic description and description of the present utility model, for explaining the utility model, is not formed improper restriction of the present utility model.In the accompanying drawings:
Fig. 1 is the schematic diagram of the electricity generation system of solar array according to the utility model embodiment;
Fig. 2 is the schematic diagram of the electricity generation system of a kind of optional solar array according to the utility model embodiment; And
Fig. 3 is the schematic diagram of the electricity generation system of another optional solar array according to the utility model embodiment.
Embodiment
It should be noted that, when not conflicting, the embodiment in the application and the feature in embodiment can combine mutually.Below with reference to the accompanying drawings and describe the utility model in detail in conjunction with the embodiments.
The utility model scheme is understood better in order to make those skilled in the art person, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is only the embodiment of the utility model part, 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 should belong to the scope of the utility model protection.
It should be noted that, term " first ", " second " etc. in specification of the present utility model and claims and above-mentioned accompanying drawing are for distinguishing similar object, and need not be used for describing specific order or precedence.Should be appreciated that the data used like this can be exchanged, in the appropriate case so that embodiment of the present utility model described herein.In addition, term " comprises " and " having " and their any distortion, intention is to cover not exclusive comprising, such as, contain those steps or unit that the process of series of steps or unit, method, system, product or equipment is not necessarily limited to clearly list, but can comprise clearly do not list or for intrinsic other step of these processes, method, product or equipment or unit.
The utility model provides a kind of solar array electricity generation system, and this solar array electricity generation system can comprise as lower component: solar array 10, sun sensor 20 and driver part 30.
Solar array 10, wherein, plane is arranged on the surface of solar array 10.Here it should be noted that, in this programme, above-mentioned solar array 10 can be monocrystaline silicon solar cell, multi-crystal silicon film solar battery, amorphous silicon thin-film solar cell etc.
Driver part 30, is connected with solar array 10 and sun sensor 20, when driver part 30 is positioned at primary importance, solar array is positioned at the second place, wherein, when solar array 10 is in the second place, solar array 10 receives the first intensity of illumination; When the control signal that driver part 30 responds sun sensor 20 output is driven into the 3rd position from primary importance, solar array 10 is driven to the 4th position from the second place, wherein, when solar array 10 is in the 4th position, solar array 10 receives the second intensity of illumination, wherein, the second intensity of illumination is greater than the first intensity of illumination.
Particularly, in the present embodiment, above-mentioned sun sensor 20 can keep the annexation of radio communication with driver part 30, sun sensor 20 is after receiving intensity of illumination, control information can be generated according to the intensity of illumination received, then above-mentioned control information is wirelessly transmitted to driver part 30 by sun sensor 20, driver part 30 is connected to above-mentioned solar array 10, therefore, driver part 30 is when occurrence positions change, also there is corresponding change in the position of solar array 10, such as, is driven to the 4th position from the second place.It should be noted that, the intensity of illumination that solar array 10 receives when the 4th position is greater than the intensity of illumination of solar array 10 received by two positions.
The utility model embodiment, by sun sensor 20 real-time reception intensity of illumination, and then generate control information according to intensity of illumination, above-mentioned control information is sent to driver part 30 by above-mentioned sun sensor 20 again, above-mentioned driver part 30 drives solar array 10 according to control information, the surface of solar array 10 is made to receive more intensity of illumination, namely the scheme of the present embodiment can realize the position of solar array 10 is changed along with the change shining upon direction, solar array 10 continues to follow the tracks of sunray all the time and namely keeps maximized reception intensity of illumination, improve the generating efficiency of sun paroxysm electric system, solve in solar array when receive intensity of illumination weak, the technical problem that generating efficiency is low.
Alternatively, above-mentioned driver part 30 can comprise rotating parts, this rotating parts can be connected with solar array 10, thus drive solar array 10 synchronous rotary, such as, when rotating parts rotates motion, rotating parts can drive solar array 10 to be rotated counterclockwise around the vertical symmetry axis of himself or to turn clockwise.
Alternatively, the shape of above-mentioned sun sensor 20 is a N prism, N can for the natural number being more than or equal to 3, N number of side of N prism is respectively arranged an optical sensor, it should be noted that, the intensity of illumination that each of N prism receives is different, therefore, the intensity of illumination that each optical sensor receives is also different, therefore the different illumination intensity that sun sensor 20 can receive according to optical sensor on N number of side determines side i.e. the first side that intensity of illumination is maximum, then control information is generated, this control information rotates for controlling driver part 30, driver part 30 drives solar array 10 to rotate, to make solar array 10 parallel with the first side, like this, solar array 10 can receive maximum intensity of illumination, generating efficiency reaches maximum.In a kind of preferred embodiment, N=8.
Alternatively, N number of side of above-mentioned N prism can be parallel to the rotating shaft of above-mentioned rotating parts.
Alternatively, the solar cell power generation system that the utility model provides can also comprise electric pressure converter, this electric pressure converter can comprise input and output, this input is connected with solar array 10, receive the electric energy that solar array 10 produces, electric pressure converter carries out voltage transitions to above-mentioned electric energy, and exports energy-storage battery to by output and carry out power storage.It should be noted that, above-mentioned energy-storage battery can be lithium-ion energy storage battery.
The utility model also provides a kind of aerostatics device, and as shown in Figure 1, this aerostatics device can comprise:
Aerostatics 40, for providing buoyancy lift, in the present embodiment, aerostatics 40 can be HAA, aerostat etc.
Gondola 08, hangs on the below of aerostatics 40, and in the present embodiment, gondola 08 adopts and draws in the net structure 50 and be connected with aerostatics 40; And
Be arranged on the sun sensor 20 on gondola 08, solar array 10 and driver part 30.
Alternatively, above-mentioned sun sensor 20 can be arranged at the top of gondola, and above-mentioned solar cell can be suspended on the below of gondola.
A kind of preferred embodiment below in conjunction with Fig. 1 to 3 pair of this programme is described:
As Fig. 1, aerostatics device can comprise gondola 08, and above-mentioned solar array 10 can hang on below gondola 08, and for receiving sunray with generating, sun sensor 20 can be eight prisms, and driver part 30 bottom is connected with solar array 10.
Particularly, eight sides of sun sensor 20 are respectively placed with an optical sensor, and the intensity of illumination received by each optical sensor is different, and the side of sun sensor 20 is parallel to the vertical symmetry axis of solar array 10.As shown in Figure 2, solar array 10 is in the second place, the intensity of illumination that sun sensor 20 can receive according to the optical sensor on each side determines the first side, the intensity of illumination that optical sensor on this first side receives is maximum, then sun sensor 20 generates control information, and this control information is sent to driver part 30, driver part 30 drives solar array 10 according to control information, solar array 10 is made to move to the 4th position from the second place, as shown in Figure 3, solar array 10 is when the 4th position, solar array 10 is parallel with above-mentioned first side, therefore the intensity of illumination received by solar array 10 is also maximum.
It should be noted that, in a kind of preferred embodiment, the aerostatics device that the present embodiment provides can carry out the moveable position of default solar array 10 according to the number of side in N prism, such as, sun sensor 20 in aerostatics device is eight prisms, so for eight sides of eight prisms, preset eight fixed positions corresponding with eight sides respectively, eight fixed positions that above-mentioned eight positions can be able to move to for solar array 10, when solar array 10 moves to the first fixed position, the sensitive surface of solar array 10 and the first side keeping parallelism of eight prisms, when solar array 10 moves to the second fixed position, the sensitive surface of solar array 10 and the second side keeping parallelism of eight prisms.
As can be seen here, solar cell power generation system in the application both can be applied in underground, also high-altitude can be applied in, high-altitude aerostatics rests in the air for a long time, solar energy is needed constantly to provide institute's energy requirement, by the scheme that above-described embodiment provides, during the aerostatics real time kinematics of high-altitude, the solar array 10 that high-altitude aerostatics gondola hangs for 08 time can along with sun angle real-time change.The system that the present embodiment provides can make solar array 10 aim at the sun in real time, improves generating efficiency, effectively ensure that aerostatics energy resource supply.
Optionally, above-mentioned driver part 30 can comprise direct current machine.
To sum up, this programme advantage is the efficiency that improve mono-crystalline silicon solar electricity generation system, meets the energy demand of high-altitude aerostatics.
In the above-described embodiments, the description of each embodiment is all emphasized particularly on different fields, in certain embodiment, there is no the part described in detail, can see the associated description of other embodiments.
In several embodiments that the application provides, should be understood that, disclosed device, the mode by other realizes.Such as, device embodiment described above is only schematic, the division of such as unit, be only a kind of logic function to divide, actual can have other dividing mode when realizing, such as multiple unit or assembly can in conjunction with or another system can be integrated into, or some features can be ignored, or do not perform.Another point, shown or discussed coupling each other or direct-coupling or communication connection can be by some interfaces, and the indirect coupling of device or unit or communication connection can be electrical or other form.
These are only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection range of the present utility model.

Claims (11)

1. a solar array electricity generation system, is characterized in that, comprising:
Sun sensor;
Solar array, wherein, plane is arranged on the surface of described solar array;
Driver part, be connected with described solar array and described sun sensor, when described driver part is positioned at primary importance, described solar array is positioned at the second place, wherein, when described solar array is in the second place, described solar array receives the first intensity of illumination; When the control signal that described driver part responds the output of described sun sensor is driven into the 3rd position from described primary importance, described solar array is driven to the 4th position from the described second place, wherein, when described solar array is in the 4th position, described solar array receives the second intensity of illumination, wherein, described second intensity of illumination is greater than described first intensity of illumination.
2. system according to claim 1, is characterized in that, described driver part comprises:
Rotating parts, is connected with described solar array, and wherein, when described rotating parts rotates motion, described rotating parts drives described solar array to rotate around the vertical symmetry axis of described solar array.
3. system according to claim 2, is characterized in that, the shape of described sun sensor is N prism, and wherein, each side of described N prism is provided with an optical sensor, wherein, N be more than or equal to 3 natural number.
4. system according to claim 3, is characterized in that, N number of side of described N prism is parallel to the rotating shaft of described rotating parts.
5. system according to claim 3, it is characterized in that, when described solar array is in described 4th position, described solar array is parallel with the first side of described N prism, wherein, the Intensity of the sunlight that other side that the Intensity of the sunlight that described first side receives is greater than described N prism receives.
6. system according to claim 1, is characterized in that, described system also comprises:
Electric pressure converter, wherein, described electric pressure converter comprises:
Input, is connected with described solar array;
Output, for exporting the signal of telecommunication obtained after the electric energy produced described solar array carries out voltage transitions.
7. system according to claim 6, is characterized in that, described system also comprises:
Energy-storage battery, is connected with the output of described electric pressure converter.
8. system according to claim 7, is characterized in that, described energy-storage battery is lithium-ion energy storage battery.
9. an aerostatics device, is characterized in that, comprising:
Aerostatics, for providing buoyancy lift;
Gondola, hangs on the below of described aerostatics; And
Solar array electricity generation system in claim 1 to 8 described in any one;
Wherein, described sun sensor and described solar array are arranged at the outside of described gondola.
10. aerostatics device according to claim 9, is characterized in that, described sun sensor is arranged at the top of described gondola.
11. aerostatics devices according to claim 10, it is characterized in that, described solar array hangs on the below of described gondola.
CN201520657103.5U 2015-08-26 2015-08-26 Solar array power generation system and aerostatics device Active CN204906259U (en)

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Application Number Priority Date Filing Date Title
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107294485A (en) * 2016-04-01 2017-10-24 苏州绿豆豆软件科技有限公司 A kind of optically focused microscope group expansion link, the tuning system and method containing the expansion link

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107294485A (en) * 2016-04-01 2017-10-24 苏州绿豆豆软件科技有限公司 A kind of optically focused microscope group expansion link, the tuning system and method containing the expansion link
CN107294485B (en) * 2016-04-01 2019-05-24 苏州绿豆豆软件科技有限公司 A kind of optically focused microscope group telescopic rod, the tuning system and method containing the telescopic rod

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Effective date of registration: 20230630

Address after: Room 501, Building D2, Songshan Lake International Innovation and Entrepreneurship Community, Songshan Lake High tech Industrial Development Zone, Dongguan City, Guangdong Province, 523000

Patentee after: Dongguan Dongguan Institute of Science and Technology Innovation

Address before: 523000 Room 502, 5th floor, building 1, innovation and Technology Park, Songshanhu high tech Industrial Development Zone, Dongguan City, Guangdong Province

Patentee before: DONGGUAN FRONTIER TECHNOLOGY INSTITUTE

Patentee before: SHENZHEN KUANG-CHI SPACE TECH. Co.,Ltd.