CN102749942B - Assembly line constant-temperature system for solar cell modules - Google Patents

Assembly line constant-temperature system for solar cell modules Download PDF

Info

Publication number
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
Authority
CN
China
Prior art keywords
incubation cavity
temperature
climate control
control module
temperature sensor
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.)
Expired - Fee Related
Application number
CN201110098678.4A
Other languages
Chinese (zh)
Other versions
CN102749942A (en
Inventor
刘海弟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CEEG Shanghai Solar Science and Technology Co Ltd
Original Assignee
CEEG Shanghai Solar Science and Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by CEEG Shanghai Solar Science and Technology Co Ltd filed Critical CEEG Shanghai Solar Science and Technology Co Ltd
Priority to CN201110098678.4A priority Critical patent/CN102749942B/en
Publication of CN102749942A publication Critical patent/CN102749942A/en
Application granted granted Critical
Publication of CN102749942B publication Critical patent/CN102749942B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Photovoltaic Devices (AREA)
  • Air Conditioning Control Device (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

A kind of streamline constant temperature system for solar module
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.
CN201110098678.4A 2011-04-19 2011-04-19 Assembly line constant-temperature system for solar cell modules Expired - Fee Related CN102749942B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110098678.4A CN102749942B (en) 2011-04-19 2011-04-19 Assembly line constant-temperature system for solar cell modules

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110098678.4A CN102749942B (en) 2011-04-19 2011-04-19 Assembly line constant-temperature system for solar cell modules

Publications (2)

Publication Number Publication Date
CN102749942A CN102749942A (en) 2012-10-24
CN102749942B true CN102749942B (en) 2014-06-25

Family

ID=47030223

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110098678.4A Expired - Fee Related CN102749942B (en) 2011-04-19 2011-04-19 Assembly line constant-temperature system for solar cell modules

Country Status (1)

Country Link
CN (1) CN102749942B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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)

* Cited by examiner, † Cited by third party
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 Novel heating temperature control system of solar energy silicon wafer cleaning wool making

Patent Citations (5)

* Cited by examiner, † Cited by third party
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 Novel heating temperature control system of solar energy silicon wafer cleaning wool making
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

Also Published As

Publication number Publication date
CN102749942A (en) 2012-10-24

Similar Documents

Publication Publication Date Title
CN107532511B (en) Compressed air stores power generator and compressed air stores electricity-generating method
CN203771528U (en) Intelligent IH water heating stove
CN106711548B (en) Air thermal management system for power battery of pure electric vehicle and working method of air thermal management system
CN204993246U (en) Photovoltaic module backplate cooling system
CN106288754A (en) One is provided multiple forms of energy to complement each other drying unit
CN202221538U (en) Cabin intelligent constant temperature controller of wind generator
KR101518243B1 (en) Hybrid Type Collecting Solar Energy for Hot Water
CN201637193U (en) Heat pump system of multi-heat sources
CN102749942B (en) Assembly line constant-temperature system for solar cell modules
CN104677180A (en) Cooling tower energy saving system and method
CN104534685A (en) Split type solar energy and air source heat pump combining system
CN211476848U (en) Energy-saving control device for cooling tower fan
CN202067160U (en) Assembly line constant temperature device for solar cell module
CN209904580U (en) Thermal management system of high-power fuel cell commercial vehicle
CN203355744U (en) Test box provided with independent heating channel and refrigerating channel
CN205611144U (en) Intelligent quantitative air supply arrangement
CN205714893U (en) A kind of air supply device and co-generation unit
CN203501386U (en) Frequency conversion driving system of central air conditioner
CN211476225U (en) Management device of constant temperature and humidity air conditioner
CN201242234Y (en) Anion high-efficiency empty power electronic cooling/warming air conditioner
CN103388854A (en) Hot water supply system capable of comprehensively utilizing energy sources
CN203366151U (en) Testing chamber with shared blower motor for heating channel and refrigeration channel
CN203351939U (en) Constant temperature laser of temperature-compensating type
CN202267161U (en) Capillary network air-conditioning equipment
CN110442080A (en) A kind of energy-saving plant control system and its control method based on PLC

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140625

Termination date: 20170419

CF01 Termination of patent right due to non-payment of annual fee