CN105703702A - Space intensive type solar panel structure - Google Patents
Space intensive type solar panel structure Download PDFInfo
- Publication number
- CN105703702A CN105703702A CN201610038297.XA CN201610038297A CN105703702A CN 105703702 A CN105703702 A CN 105703702A CN 201610038297 A CN201610038297 A CN 201610038297A CN 105703702 A CN105703702 A CN 105703702A
- Authority
- CN
- China
- Prior art keywords
- solar panels
- space
- supporting plate
- intensive type
- type solar
- 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.)
- Granted
Links
- 239000000758 substrate Substances 0.000 claims abstract description 16
- 239000000843 powder Substances 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 8
- 239000000919 ceramic Substances 0.000 claims description 6
- 229920002261 Corn starch Polymers 0.000 claims description 3
- 239000004113 Sepiolite Substances 0.000 claims description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 3
- 239000010425 asbestos Substances 0.000 claims description 3
- 229910052810 boron oxide Inorganic materials 0.000 claims description 3
- 239000011852 carbon nanoparticle Substances 0.000 claims description 3
- 239000001913 cellulose Substances 0.000 claims description 3
- 229920002678 cellulose Polymers 0.000 claims description 3
- 229910052878 cordierite Inorganic materials 0.000 claims description 3
- 239000008120 corn starch Substances 0.000 claims description 3
- 239000006063 cullet Substances 0.000 claims description 3
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 claims description 3
- JSKIRARMQDRGJZ-UHFFFAOYSA-N dimagnesium dioxido-bis[(1-oxido-3-oxo-2,4,6,8,9-pentaoxa-1,3-disila-5,7-dialuminabicyclo[3.3.1]nonan-7-yl)oxy]silane Chemical compound [Mg++].[Mg++].[O-][Si]([O-])(O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2)O[Al]1O[Al]2O[Si](=O)O[Si]([O-])(O1)O2 JSKIRARMQDRGJZ-UHFFFAOYSA-N 0.000 claims description 3
- 229910052895 riebeckite Inorganic materials 0.000 claims description 3
- 235000019355 sepiolite Nutrition 0.000 claims description 3
- 229910052624 sepiolite Inorganic materials 0.000 claims description 3
- 239000011863 silicon-based powder Substances 0.000 claims description 3
- 229910052613 tourmaline Inorganic materials 0.000 claims description 3
- 229940070527 tourmaline Drugs 0.000 claims description 3
- 239000011032 tourmaline Substances 0.000 claims description 3
- 238000010248 power generation Methods 0.000 abstract description 2
- 230000008033 biological extinction Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 3
- 238000000498 ball milling Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- 239000005995 Aluminium silicate Substances 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 235000012211 aluminium silicate Nutrition 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004210 cathodic protection Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229960000935 dehydrated alcohol Drugs 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229960004756 ethanol Drugs 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000013083 solar photovoltaic technology Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S30/00—Structural details of PV modules other than those related to light conversion
- H02S30/10—Frame structures
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C14/00—Glass compositions containing a non-glass component, e.g. compositions containing fibres, filaments, whiskers, platelets, or the like, dispersed in a glass matrix
-
- 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
Abstract
The invention discloses a space intensive type solar panel structure, and the structure comprises a substrate and a plurality of solar panels laid on the substrate. There is a gap between each two solar panels, and the structure is characterized in that two ends of each gap are respectively provided with a support plate; the support plates are provided with a group of solar panels; the solar panels on the support plates are narrower than the solar panels on the substrate, so as to adapt to the gaps; through adding one panel between each two solar panels, the structure can increase the density, reduces the cost, increases the light absorbing area, and improves the power generation efficiency.
Description
Technical field
The present invention relates to technical field of solar, be specifically related to a kind of space-intensive type solar panels structure。
Background technology
By solar cell array, the electric station that solar radiation can be converted to electric energy is called solar photovoltaic power plant。Solar photovoltaic power plant can be divided into independent solar photovoltaic power station and grid-connected solar photovoltaic power plant according to the method for operation。The independently-powered solar photovoltaic power plant that is not connected with public electric wire net is called off-network photovoltaic plant。It is mainly used in the areas without electricity away from public electric wire net and some Code in Hazardous Special Locations; as for outlying remote rural area, pastoral area, island, plateau, desert agriculture and animal husbandry fisherman illumination be provided, see TV, the basic household electricity such as listen to the radio programme, for communication relay station, coastal special place provides power supply with inland waterway navigation aids, oil and gas pipeline cathodic protection, meteorological power station, road team and frontier sentry etc.。Autonomous system is made up of solar cell array, system controller, accumulator battery, DC/AC inverter etc.。It is connected with public electric wire net and the power solar photovoltaic power plant of task of shared is called grid-connected photovoltaic power station, it is that solar energy power generating enters large-scale commercial power generating stage, becomes the important development direction of power industry ingredient, is the main trend of world today's solar photovoltaic technology development。
General solar panels are planar fashion, and it is arranged is by the tiling of several solar panels side by side, reaches to collect the purpose of sunlight。For preventing short circuit, between two pieces of solar panels, it is provided with non-electric power generation domain, i.e. space, the confined space of the substrate of the existence in this space waste, therefore, in limited region, how to promote the extinction area of solar panels, be the present invention target that is intended to reach。
Summary of the invention
The technical problem to be solved is in that to provide a kind of reasonable in design, it is possible to reduce the space-intensive type solar panels structure of cost。
The technical problem to be solved realizes by the following technical solutions:
A kind of space-intensive type solar panels structure, including substrate and be laid in the multi-disc solar panels on substrate, space is left between every two pieces of solar panels, it is characterized in that, it is respectively arranged at two ends with a supporting plate in this space, described supporting plate is provided with one group of solar panels, solar panels on supporting plate are than the solar panels width on substrate more narrowly, to adapt to space, add one piece by the space between two pieces of solar panels, by increasing capacitance it is possible to increase density, reduce cost, increase extinction area, improve generating efficiency。
The height of described supporting plate is identical with the width in space, keeps good suitability, is unlikely to block sunlight。
Described supporting plate is that nonmetallic materials are made, and is absent from conductivity issues, simultaneously corrosion-resistant。
Described supporting plate is made up of the component of following weight: cullet 108kg, cordierite 1.5kg, cellulose 0.4kg, active carbon nanoparticles 0.1kg, silicon powder 1.55kg, corn starch 1.35kg, flake asbestos 1.6kg, sepiolite powder 2.8kg, boron oxide 0.6kg, tourmaline powder 0.6kg, complex phase ceramic powder 20kg。This supporting plate hardness is high, and stable performance, anti-corrosion insulation effect is good。
The invention has the beneficial effects as follows: the present invention is novel in design, the space on substrate is made full use of by simple in construction, increases the extinction area of whole solar panels, improves generating efficiency, reduces cost。
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram。
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and effect and be easy to understand, below in conjunction with being specifically illustrating, the present invention is expanded on further。
Embodiment 1
Referring to Fig. 1: a kind of space-intensive type solar panels structure, including substrate 1 and tiling multi-disc solar panels 2 on substrate 1, space is left between every two pieces of solar panels 2, it is respectively arranged at two ends with a supporting plate 3 in this space, described supporting plate 3 is provided with solar panels 4 between one group of space, space solar panels 4 on supporting plate 3 are than solar panels 2 width on substrate 1 more narrowly, to adapt to space, one piece is added by the space between two pieces of solar panels, density can be increased, reduce cost, increase extinction area, improve generating efficiency。The height of described supporting plate 3 is identical with the width in space, keeps good suitability, is unlikely to block sunlight。Described supporting plate 3 is made for nonmetallic materials, is absent from conductivity issues, simultaneously corrosion-resistant。
Embodiment 2
Referring to Fig. 1: a kind of space-intensive type solar panels structure, including substrate 1 and tiling multi-disc solar panels 2 on substrate 1, space is left between every two pieces of solar panels 2, it is respectively arranged at two ends with a supporting plate 3 in this space, described supporting plate 3 is provided with solar panels 4 between one group of space, space solar panels 4 on supporting plate 3 are than solar panels 2 width on substrate 1 more narrowly, to adapt to space, one piece is added by the space between two pieces of solar panels, density can be increased, reduce cost, increase extinction area, improve generating efficiency。The height of described supporting plate 3 is identical with the width in space, keeps good suitability, is unlikely to block sunlight。Described supporting plate 3 is made for nonmetallic materials, is absent from conductivity issues, simultaneously corrosion-resistant。Wherein supporting plate is made up of the component of following weight: cullet 108kg, cordierite 1.5kg, cellulose 0.4kg, active carbon nanoparticles 0.1kg, silicon powder 1.55kg, corn starch 1.35kg, flake asbestos 1.6kg, sepiolite powder 2.8kg, boron oxide 0.6kg, tourmaline powder 0.6kg, complex phase ceramic powder 20kg。This supporting plate hardness is high, and stable performance, anti-corrosion insulation effect is good。
The preparation method of above-mentioned supporting plate is as follows:
1) together being put in nylon ball grinder by above-mentioned raw materials, with agate ball for abrading-ball, ball material mass ratio is 7:1, when rotating speed is 150 revs/min, and continuous ball milling 3 hours in ball mill；
2) raw material after grinding is taken out dry, place into furnace heats between 1520-1560 DEG C, keeping this temperature 4-8 hour, make material reach molten condition；
3) melted material is sent into forming machine, make the supporting plate of the specification that varies in size, send into annealing kiln with conveyer after supporting plate is naturally cooling to 600 DEG C of hardening, anneal complete, supporting plate is sent in air, naturally cool to room temperature in atmosphere；
4) supporting plate after annealing is sent into tempering case, first supporting plate is heated between 660-680 DEG C, stop heating, sending into cold wind from all directions immediately, after rapidly supporting plate being cooled to room temperature, tempering terminates, supporting plate is taken out from tempering case, obtains finished product。
The preparation method of above-mentioned complex phase ceramic powder is as follows:
1) calcined kaolin powder and TiC powder are weighed by the part by weight of 2:3；
2) to the calcined kaolin powder weighed and TiC powder with dehydrated alcohol for disperse medium, wherein powder is 1:30 with the mass ratio of ethanol, ultrasonic disperse 1 hour on supersonic cleaning machine；
3) compound through ultrasonic disperse being put in nylon ball grinder, with agate ball for abrading-ball, ball material mass ratio is 7:1, when rotating speed is 150 revs/min, and continuous ball milling 2 hours in planetary ball mill；
4) powder complete for ball milling is poured in powder dish together with Achates abrading-ball, dry at 80 DEG C；
5) powder dried being sieved, take out Achates abrading-ball, then ground by mixed powder, until without till bigger reunion, so far, preparing of modified ceramic powder is complete。Pottery prepared by this ceramics has that elastic modelling quantity is big, is unlikely to deform, Heat stability is good, physical and chemical performance are stable。
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described。Skilled person will appreciate that of the industry; the present invention is not restricted to the described embodiments; described in above-described embodiment and description is that principles of the invention is described; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements both fall within the claimed scope of the invention。Claimed scope is defined by appending claims and equivalent thereof。
Claims (4)
1. a space-intensive type solar panels structure, including substrate and be laid in the multi-disc solar panels on substrate, between every two pieces of solar panels, leave space, it is characterised in that, it is respectively arranged at two ends with a supporting plate in this space, described supporting plate is provided with one group of solar panels。
2. a kind of space-intensive type solar panels structure according to claim 1, it is characterised in that: the height of described supporting plate is identical with the width in space。
3. a kind of space-intensive type solar panels structure according to claim 1, it is characterised in that: described supporting plate is that nonmetallic materials are made。
4. a kind of space-intensive type solar panels structure according to claim 3, it is characterised in that: described supporting plate is made up of the component of following weight: cullet 108kg, cordierite 1.5kg, cellulose 0.4kg, active carbon nanoparticles 0.1kg, silicon powder 1.55kg, corn starch 1.35kg, flake asbestos 1.6kg, sepiolite powder 2.8kg, boron oxide 0.6kg, tourmaline powder 0.6kg, complex phase ceramic powder 20kg。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610038297.XA CN105703702B (en) | 2016-01-20 | 2016-01-20 | A kind of space-intensive type solar panels structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610038297.XA CN105703702B (en) | 2016-01-20 | 2016-01-20 | A kind of space-intensive type solar panels structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105703702A true CN105703702A (en) | 2016-06-22 |
| CN105703702B CN105703702B (en) | 2018-06-19 |
Family
ID=56227709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610038297.XA Active CN105703702B (en) | 2016-01-20 | 2016-01-20 | A kind of space-intensive type solar panels structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105703702B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6175567A (en) * | 1984-09-20 | 1986-04-17 | Sanyo Electric Co Ltd | Photovoltaic device |
| CN102177591A (en) * | 2008-09-04 | 2011-09-07 | 摩根阳光公司 | Staggered light collectors for concentrator solar panels |
| CN103185959A (en) * | 2011-12-30 | 2013-07-03 | 安徽天柱绿色能源科技有限公司 | Slot type solar concentrator |
| CN103592957A (en) * | 2013-11-11 | 2014-02-19 | 深圳市易能电气技术有限公司 | Solar cell panel array and automatic light following system and method thereof |
| CN104412390A (en) * | 2012-05-31 | 2015-03-11 | 陶氏环球技术有限责任公司 | High utilization photo-voltaic device |
-
2016
- 2016-01-20 CN CN201610038297.XA patent/CN105703702B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6175567A (en) * | 1984-09-20 | 1986-04-17 | Sanyo Electric Co Ltd | Photovoltaic device |
| CN102177591A (en) * | 2008-09-04 | 2011-09-07 | 摩根阳光公司 | Staggered light collectors for concentrator solar panels |
| CN103185959A (en) * | 2011-12-30 | 2013-07-03 | 安徽天柱绿色能源科技有限公司 | Slot type solar concentrator |
| CN104412390A (en) * | 2012-05-31 | 2015-03-11 | 陶氏环球技术有限责任公司 | High utilization photo-voltaic device |
| CN103592957A (en) * | 2013-11-11 | 2014-02-19 | 深圳市易能电气技术有限公司 | Solar cell panel array and automatic light following system and method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105703702B (en) | 2018-06-19 |
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| TR01 | Transfer of patent right |
Effective date of registration: 20230714 Address after: 266000 area B2, 9th floor, block B, Qingdao International Innovation Park, No.1 keyuanwei 1st Road, Laoshan District, Qingdao City, Shandong Province Patentee after: SHANDONG SHICHUAN ENERGY SAVING TECHNOLOGY Co.,Ltd. Address before: 236500 shop 110, building 1, Jiefang community, west of Jiefang Fifth Street, Jieshou City, Fuyang City, Anhui Province Patentee before: JIESHOU JINGHUA TECHNOLOGY INFORMATION CONSULTING SERVICE Co.,Ltd. |
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