CN102749942B - Assembly line constant-temperature system for solar cell modules - Google Patents
Assembly line constant-temperature system for solar cell modules Download PDFInfo
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- CN102749942B CN102749942B CN201110098678.4A CN201110098678A CN102749942B CN 102749942 B CN102749942 B CN 102749942B CN 201110098678 A CN201110098678 A CN 201110098678A CN 102749942 B CN102749942 B CN 102749942B
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- incubation cavity
- temperature
- climate control
- control module
- temperature sensor
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- 238000004378 air conditioning Methods 0.000 claims abstract description 12
- 238000011534 incubation Methods 0.000 claims description 36
- 230000005540 biological transmission Effects 0.000 claims description 22
- 238000009413 insulation Methods 0.000 claims description 11
- 239000011324 bead Substances 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 abstract description 11
- 210000001503 joint Anatomy 0.000 abstract 1
- 238000004140 cleaning Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000011056 performance test Methods 0.000 description 2
- 229910021419 crystalline silicon Inorganic materials 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
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- Photovoltaic Devices (AREA)
Abstract
The invention relates to an assembly line constant-temperature system for solar cell modules, which comprises a first constant-temperature table, a second constant-temperature table, a temperature controller, a drive module and a temperature sensor; the first constant-temperature table comprises a first air-conditioning module and a first heat-preserving chamber which communicate with each other; the second constant-temperature table comprises a second air-conditioning module and a second heat-preserving chamber which communicate with each other; the first heat-preserving chamber is in butt joint with the second heat-preserving chamber to form an integrated heat-preserving chamber; the drive module comprises variable-frequency motors and drive shafts, wherein the variable-frequency motors are connected with the drive shafts, the drive shafts are mounted in the middle of the integrated heat-preserving chamber, and the solar cell modules are arranged on the drive shafts; the temperature controller is respectively connected with the first air-conditioning module, the second air-conditioning module and the temperature sensor; and the temperature sensor is arranged at the outlet of the second heat-preserving chamber. Compared with the prior art, the assembly line constant-temperature system has the advantages of high production efficiency, small size, labor intensity decrease, manpower cost reduction and the like.
Description
Technical field
The present invention relates to a kind of constant temperature system of solar components, especially relate to a kind of streamline constant temperature system for solar module.
Background technology
In crystalline silicon solar cell modules is produced, according to international standard IEC61215 regulation, electrical component performance test requires MUT module under test temperature at 25 ± 2 DEG C.For ensureing the accuracy of test data.At present, adopt Special constant temperature chamber to carry out constant temperature to assembly both at home and abroad, special test chamber off-line test.There is following defect in this mode:
1, can not carry out assembly on-the-spot Production line to test from cleaning, cannot form assembly whole production process streamline, make assembly output bas line degree be difficult to improve.
2, Special constant temperature chamber, test cabinet land area are large, and general every hundred megawatt production capacities need to approximately 400 square metres;
3, conventionally adopt 20/holder to stack constant temperature, constant temperature time is long, and poor temperature uniformity affects electric performance test accuracy.
4, assembly needs manually to Special constant temperature chamber, test cabinet shifts, and consuming time and take manpower, labour intensity is large, production efficiency is low.
Summary of the invention
Object of the present invention is exactly the streamline constant temperature system for solar module that provides in order to overcome the defect that above-mentioned prior art exists that a kind of production efficiency is high, volume is little, reduces labour intensity and cost of labor.
Object of the present invention can be achieved through the following technical solutions:
For a streamline constant temperature system for solar module, it is characterized in that, comprise the first thermostatic platform, the second thermostatic platform, temperature controller, transmission module, temperature sensor;
The first described thermostatic platform comprises the first Climate Control Module, the first incubation cavity that are interconnected; The second described thermostatic platform comprises the second Climate Control Module, the second incubation cavity that are interconnected; The first described incubation cavity docks with the second incubation cavity and forms integral heat insulation chamber;
Described transmission module comprises variable-frequency motor, transmission shaft, and described variable-frequency motor is connected with transmission shaft, and described transmission shaft is arranged on middle part, integral heat insulation chamber, and described solar module is located on transmission shaft;
Described temperature controller is connected with the first Climate Control Module, the second Climate Control Module, temperature sensor respectively; Described temperature sensor is located at the exit of the second incubation cavity; Temperature controller, according to temperature sensor signal, is selected hot blast or cold wind pattern automatically.
The first described Climate Control Module includes the first air-conditioning, the first air supply duct, the first return air duct, and the first described air supply duct is located at the first incubation cavity exit, and the first described return air duct is located at the first incubation cavity inflow point.
The second described Climate Control Module comprises the second air-conditioning, the second air supply duct, the second return air duct, and the second described air supply duct is located at the second incubation cavity inflow point, and the second described return air duct is located at the second incubation cavity exit.
Also comprise deep bead, split-wind plate, described deep bead is located at the two ends in integral heat insulation chamber, and described split-wind plate is located at respectively the middle part of the first incubation cavity, the second incubation cavity.
Compared with prior art, the present invention has the following advantages:
1, realize assembly automatic constant-temperature Production line, belong to domestic, international pioneering;
2, monolithic module automated movement constant temperature, constant temperature time is short, and temperature is even, and Level temperature difference is less than 1 DEG C, and production efficiency is high;
3, realization, to the Production line of test from cleaning, has greatly improved assembly output bas line degree and optimization component and has produced line structure;
4, assembly constant temperature land area greatly reduces, and land area is only 10% of Special constant temperature chamber;
5, the on-the-spot automatic constant-temperature of assembly, does not need manually to carry to solidifying chamber, greatly reduces labour intensity, cost of labor.
Brief description of the drawings
Fig. 1 is structural representation of the present invention.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Embodiment
As shown in Figure 1, a kind of streamline constant temperature system for solar module, comprises the first thermostatic platform 1, the second thermostatic platform 2, temperature controller 3, transmission module 4, temperature sensor 5;
The first described thermostatic platform 1 comprises the first Climate Control Module, the first incubation cavity 14 that are interconnected; The second described thermostatic platform 2 comprises the second Climate Control Module, the second incubation cavity 24 that are interconnected; The first described incubation cavity 14 docks with the second incubation cavity 24 and forms integral heat insulation chamber;
Described transmission module 4 comprises variable-frequency motor, transmission shaft 41, described variable-frequency motor is connected with transmission shaft 41, described transmission shaft 41 is arranged on middle part, integral heat insulation chamber, and described solar module 8 is located on transmission shaft 41, and transmission speed can be according to productive temp setting, adjustment;
Described temperature controller 3 is connected with the first Climate Control Module, the second Climate Control Module, temperature sensor 5 respectively; Described temperature sensor 5 is located at the exit of the second incubation cavity 24; Temperature controller 3, according to temperature sensor signal, is selected hot blast or cold wind pattern automatically.
The first described Climate Control Module includes the first air-conditioning 11, the first air supply duct 12, the first return air duct 13, and the first described air supply duct 12 is located at the first incubation cavity 14 exits, and the first described return air duct 13 is located at the first incubation cavity 14 inflow points.The second described Climate Control Module comprises the second air-conditioning 21, the second air supply duct 22, the second return air duct 23, and the second described air supply duct 22 is located at the second incubation cavity 24 inflow points, and the second described return air duct 23 is located at the second incubation cavity 24 exits.Arrange like this and form constant temperature streamline middle part for air intake, two ends are return air, realize the equilibrium of insulation cavity temperature wind field; Air-conditioning is selected refrigeration, heating power according to 10 DEG C of (minimum)~30 of solar module 8 production scene temperature DEG C (the highest), assembly transmission speed and assembly control temperature.
The present invention also comprises deep bead 7, split-wind plate 6, and described deep bead 7 is located at the two ends in integral heat insulation chamber, and described split-wind plate 6 is located at respectively the middle part of the first incubation cavity 14, the second incubation cavity 24.It is upper and lower keeping warmth space that transmission shaft 31 is divided into incubation cavity, and the deep bead 7, the split-wind plate 6 that in incubation cavity, arrange, carry out wind flow distribution, forms balanced wind field, realizes assembly top and bottom temperature consistent, and the temperature difference is not more than 1 DEG C.
The whole line floor area of the present invention is little, and 50MW subassembly line is about 25m
2, can conveniently be connected to form a whole set of streamline with other production process streamlines.
Transmission module 4 drives assembly slowly by integral heat insulation chamber so that speed to be set, and first, second Climate Control Module is selected the sending of heat, cold wind, return air circulation automatically according to assembly.When assembly temperature during lower than 23 DEG C air-conditioning system send hot blast, when assembly temperature Climate Control Module when in 27 DEG C send cold wind.Climate Control Module, incubation cavity, split-wind plate, deep bead form balanced wind field assembly are carried out to progressive heating, be incubated or lower the temperature, be incubated.Assembly arrives 25 ± 2 DEG C from feed end to discharge end temperature.
Claims (4)
1. for a streamline constant temperature system for solar module, it is characterized in that, comprise the first thermostatic platform, the second thermostatic platform, temperature controller, transmission module, temperature sensor;
The first described thermostatic platform comprises the first Climate Control Module, the first incubation cavity that are interconnected; The second described thermostatic platform comprises the second Climate Control Module, the second incubation cavity that are interconnected; The first described incubation cavity docks with the second incubation cavity and forms integral heat insulation chamber;
Described transmission module comprises variable-frequency motor, transmission shaft, and described variable-frequency motor is connected with transmission shaft, and described transmission shaft is arranged on middle part, integral heat insulation chamber, and described solar module is located on transmission shaft;
Described temperature controller is connected with the first Climate Control Module, the second Climate Control Module, temperature sensor respectively; Described temperature sensor is located at the exit of the second incubation cavity; Temperature controller, according to temperature sensor signal, is selected hot blast or cold wind pattern automatically.
2. a kind of streamline constant temperature system for solar module according to claim 1, it is characterized in that, the first described Climate Control Module includes the first air-conditioning, the first air supply duct, the first return air duct, the first described air supply duct is located at the first incubation cavity exit, and the first described return air duct is located at the first incubation cavity inflow point.
3. a kind of streamline constant temperature system for solar module according to claim 1, it is characterized in that, the second described Climate Control Module comprises the second air-conditioning, the second air supply duct, the second return air duct, the second described air supply duct is located at the second incubation cavity inflow point, and the second described return air duct is located at the second incubation cavity exit.
4. a kind of streamline constant temperature system for solar module according to claim 1, it is characterized in that, also comprise deep bead, split-wind plate, described deep bead is located at the two ends in integral heat insulation chamber, and described split-wind plate is located at respectively the middle part of the first incubation cavity, the second incubation cavity.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201110098678.4A CN102749942B (en) | 2011-04-19 | 2011-04-19 | Assembly line constant-temperature system for solar cell modules |
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CN201110098678.4A CN102749942B (en) | 2011-04-19 | 2011-04-19 | Assembly line constant-temperature system for solar cell modules |
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CN102749942A CN102749942A (en) | 2012-10-24 |
CN102749942B true CN102749942B (en) | 2014-06-25 |
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CN201110098678.4A Expired - Fee Related CN102749942B (en) | 2011-04-19 | 2011-04-19 | Assembly line constant-temperature system for solar cell modules |
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CN111551310B (en) * | 2020-05-12 | 2024-05-14 | 苏州纳芯微电子股份有限公司 | Temperature adjusting device and calibration system with same |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000022193A (en) * | 1998-07-06 | 2000-01-21 | Sharp Corp | Solar cell module |
FR2913919A1 (en) * | 2007-03-23 | 2008-09-26 | Valeo Systemes Thermiques | Ventilating, heating and air conditioning auxiliary installation for motor vehicle, has management unit managing operation of auxiliary installation for selecting electrical power supply sources supplying electrical units |
CN101620448A (en) * | 2009-07-29 | 2010-01-06 | 北京北方微电子基地设备工艺研究中心有限责任公司 | Temperature monitoring method and device of production line device |
CN201508401U (en) * | 2009-06-26 | 2010-06-16 | 北京卓立汉光仪器有限公司 | Solar battery piece test device |
CN201601137U (en) * | 2009-06-02 | 2010-10-06 | 上海圣微电子科技发展有限公司 | A new type of heating and temperature control system in solar silicon wafer cleaning and texturing |
-
2011
- 2011-04-19 CN CN201110098678.4A patent/CN102749942B/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000022193A (en) * | 1998-07-06 | 2000-01-21 | Sharp Corp | Solar cell module |
FR2913919A1 (en) * | 2007-03-23 | 2008-09-26 | Valeo Systemes Thermiques | Ventilating, heating and air conditioning auxiliary installation for motor vehicle, has management unit managing operation of auxiliary installation for selecting electrical power supply sources supplying electrical units |
CN201601137U (en) * | 2009-06-02 | 2010-10-06 | 上海圣微电子科技发展有限公司 | A new type of heating and temperature control system in solar silicon wafer cleaning and texturing |
CN201508401U (en) * | 2009-06-26 | 2010-06-16 | 北京卓立汉光仪器有限公司 | Solar battery piece test device |
CN101620448A (en) * | 2009-07-29 | 2010-01-06 | 北京北方微电子基地设备工艺研究中心有限责任公司 | Temperature monitoring method and device of production line device |
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