CN112278708A - Calibration and grounding test system and method for solar cell module - Google Patents
Calibration and grounding test system and method for solar cell module Download PDFInfo
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- CN112278708A CN112278708A CN202011109561.7A CN202011109561A CN112278708A CN 112278708 A CN112278708 A CN 112278708A CN 202011109561 A CN202011109561 A CN 202011109561A CN 112278708 A CN112278708 A CN 112278708A
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- 238000012360 testing method Methods 0.000 title claims abstract description 111
- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000007246 mechanism Effects 0.000 claims abstract description 97
- 230000008569 process Effects 0.000 claims abstract description 9
- 230000009471 action Effects 0.000 claims description 6
- 206010014405 Electrocution Diseases 0.000 abstract 1
- 238000001514 detection method Methods 0.000 description 4
- 230000007547 defect Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 206010014357 Electric shock Diseases 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
- B65G15/00—Conveyors having endless load-conveying surfaces, i.e. belts and like continuous members, to which tractive effort is transmitted by means other than endless driving elements of similar configuration
- B65G15/30—Belts or like endless load-carriers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
- B65G47/00—Article or material-handling devices associated with conveyors; Methods employing such devices
- B65G47/22—Devices influencing the relative position or the attitude of articles during transit by conveyors
- B65G47/24—Devices influencing the relative position or the attitude of articles during transit by conveyors orientating the articles
-
- 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
- H02S50/00—Monitoring or testing of PV systems, e.g. load balancing or fault identification
- H02S50/10—Testing of PV devices, e.g. of PV modules or single PV cells
-
- 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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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
- Testing Of Individual Semiconductor Devices (AREA)
Abstract
The invention relates to a solar cell module correcting and grounding test system, which comprises a rack, and an input mechanism, a correcting mechanism, a test mechanism, an output mechanism and a control platform which are sequentially arranged on the rack, wherein the input mechanism, the correcting mechanism, the test mechanism and the output mechanism are all connected to the control platform; the input mechanism is used for inputting the solar cell module, and the correction mechanism is used for adjusting the position of the input solar cell module; the testing mechanism is used for testing the corrected solar cell module; the output mechanism is used for outputting the tested solar cell module and carrying out the next process. The invention has the advantages that: the assembly line of having accomplished solar module fast detects, and reduction artifical the participation by a wide margin has still avoided the risk of electrocution to the at utmost when having improved work efficiency, has reduced the potential safety hazard.
Description
Technical Field
The invention relates to a solar cell module correction and grounding test system and a method thereof, which are used for correcting and testing a solar cell module.
Background
The solar cell module is usually required to be subjected to grounding impedance safety inspection, namely grounding test, and is used for testing the grounding resistance of the solar cell module, and the grounding test is favorable for the safe contact of the solar cell module with other articles and personnel in installation and use so as to achieve the purposes of insulation, electric leakage prevention and safe use.
Most of the current detection is performed manually, and the defects are as follows: because the human direct contact solar energy component, consequently, in test work, there is the potential safety hazard great, because rely on artifical the completion, can appear lou examining usually, cause detection efficiency low.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides a system and a method for correcting and testing grounding of a solar cell module, and the technical scheme of the invention is as follows:
a solar cell module correction and grounding test system comprises a rack, and an input mechanism, a correction mechanism, a test mechanism, an output mechanism and a control platform which are sequentially arranged on the rack, wherein the input mechanism, the correction mechanism, the test mechanism and the output mechanism are all connected to the control platform; the input mechanism is used for inputting the solar cell module, and the correction mechanism is used for adjusting the position of the input solar cell module; the testing mechanism is used for testing the corrected solar cell module; the output mechanism is used for outputting the tested solar cell module and carrying out the next process.
The input mechanism comprises an input support, an input conveyor belt and input guide plates, the input conveyor belt is rotatably arranged on the input support, four input guide plates are uniformly arranged on the rack at the periphery of the input conveyor belt, and a sliding groove matched with the solar cell module is arranged on the inner side of each input guide plate; two input guide plates are arranged on one side of the input conveyor belt, and two input guide plates are arranged on the other side of the input conveyor belt; each of the input guide plates has a portion disposed adjacent to the input conveyor belt and another portion disposed outside the input conveyor belt.
The correcting mechanism comprises a correcting support, a correcting conveying belt, correcting guide plates and a clamping mechanism, wherein the correcting conveying belt is rotatably installed on the correcting support, the rack far away from one end of the input support is provided with the two correcting guide plates, the two correcting guide plates are symmetrically arranged along the correcting support, the inner side of each correcting guide plate is provided with a sliding groove matched with the solar cell module, and the clamping mechanism is installed at the correcting support and corrects the solar cell module.
The clamping mechanism comprises a driving motor arranged along the vertical direction, the driving motor is arranged on a motor mounting plate at the upper part of the correcting conveying belt, and the motor mounting plate is arranged on the rack and is parallel to the correcting bracket; a motor shaft of the driving motor is provided with a driving gear, rack grooves are formed in motor mounting plates on two sides of the driving gear, the two rack grooves are arranged in a diagonal manner, and a rack meshed with the driving gear is slidably mounted in each rack groove; one end of each rack is meshed with the driving gear, and the other end of each rack is provided with a clamping plate; the two clamping plates are respectively positioned at two sides of the correction conveying belt, are in movable fit with the solar cell modules placed on the correction conveying belt, are close to or far away from the solar cell modules, and correct the solar cell modules.
The testing mechanism comprises a testing support, a testing conveyer belt, a lifting air cylinder and a testing frame, wherein the testing conveyer belt is rotatably installed on the testing support, one end of the testing support, which is far away from the correcting support, is provided with a testing guide plate, the two testing guide plates are symmetrically arranged along the testing support, the air cylinder support is installed on a frame on the upper portion of the testing support, the lifting air cylinder is installed on the air cylinder support, a testing frame is installed on a piston rod of the lifting air cylinder, and the testing frame is fixedly provided with a grounding tester which is in contact with the solar battery component under the action of the lifting air cylinder to test the solar battery component on the testing conveyer belt.
The output mechanism comprises an output support, an output conveyor belt and output guide plates, the output conveyor belt is rotatably arranged on the output support, the output direction of the output conveyor belt is perpendicular to the input direction of the input conveyor belt, the output guide plates are arranged on the rack at the output end of the output conveyor belt, and the two output guide plates are symmetrically arranged along the output support.
A calibration and grounding test method for a solar cell module comprises the following steps:
(1) inputting a solar cell module;
(2) correcting and adjusting the position of the input solar cell module;
(3) testing the corrected solar cell module;
(4) displaying and storing the tested data;
(5) and outputting the tested solar cell module, and performing the next process.
In the step (1), the input conveyor belt conveys the solar cell module, and the output of the solar cell module is finished under the guidance of the input guide plate; in the step (5), the output conveyor belt outputs the solar cell module, and the output of the solar cell module is completed under the guidance of the output guide plate.
And (2) driving the driving gear to rotate by the driving motor to drive the racks on two sides of the driving gear to slide in a reciprocating manner, driving the clamping plate arranged on the racks to move in a reciprocating manner when the racks slide, so that the solar cell module on the correction conveying belt is corrected, and the guiding output of the solar cell module is finished under the action of the correction guide plate.
In the step (3), the lifting cylinder drives the test frame to move downwards to drive the grounding tester to contact with the solar cell module on the test conveyer belt and perform testing, and after the testing is finished, the lifting cylinder drives the test frame to move upwards and the test conveyer belt drives the solar cell module to output.
The invention has the advantages that: the input mechanism, the correcting mechanism, the testing mechanism, the output mechanism and the control platform are arranged on the rack in sequence, and the input mechanism, the correcting mechanism, the testing mechanism and the output mechanism are all connected to the control platform; the input mechanism is used for inputting the solar cell module, and the correction mechanism is used for adjusting the position of the input solar cell module; the testing mechanism is used for testing the corrected solar cell module; the output mechanism is used for outputting the tested solar cell module and performing the next process, and through the arrangement of the series of structures, the assembly line detection of the solar cell module is rapidly completed, the manual participation is greatly reduced, the working efficiency is improved, meanwhile, the electric shock risk is avoided to the greatest extent, and the potential safety hazard is reduced.
Drawings
Fig. 1 is a schematic view of the main structure of the present invention.
Fig. 2 is a top view of fig. 1.
Fig. 3 is a schematic view of the connection relationship between the lifting cylinder and the testing frame in the testing mechanism in fig. 1.
Detailed Description
The invention will be further described with reference to specific embodiments, and the advantages and features of the invention will become apparent as the description proceeds. These examples are illustrative only and do not limit the scope of the present invention in any way. It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention, and that such changes and modifications may be made without departing from the spirit and scope of the invention.
Referring to fig. 1 to 3, the invention relates to a calibration and grounding test system for a solar cell module, which comprises a rack 1, and an input mechanism 2, a calibration mechanism 3, a test mechanism 4, an output mechanism 5 and a control platform 6 which are sequentially installed on the rack, wherein the input mechanism 2, the calibration mechanism 3, the test mechanism 4 and the output mechanism 5 are all connected to the control platform 6; the input mechanism 2 is used for inputting the solar battery assembly, and the correction mechanism 3 is used for adjusting the position of the input solar battery assembly; the testing mechanism 4 is used for testing the corrected solar cell module; the output mechanism 5 is used for outputting the tested solar cell module and performing the next process.
The input mechanism 2 comprises an input bracket 11, an input conveyor belt and input guide plates 12, wherein the input conveyor belt (not shown) is rotatably arranged on the input bracket 11 and driven by a conventional belt transmission mechanism, four input guide plates 12 are uniformly arranged on the frame 1 at the periphery of the input conveyor belt, and the inner side of each input guide plate 12 is provided with a chute matched with the solar cell module; two input guide plates are arranged on one side of the input conveyor belt, two input guide plates are arranged on the other side of the input conveyor belt, and input guide of the solar cell module to be tested is realized through the four input guide plates; each of the input guide plates 12 has a portion disposed adjacent to the input conveyor belt and another portion disposed outside the input conveyor belt.
The correcting mechanism comprises a correcting support 21, a correcting conveying belt, a correcting guide plate 25 and a clamping mechanism, wherein the correcting conveying belt is rotatably installed on the correcting support 21, two correcting guide plates 25 are installed on a rack which is far away from one end of the input support 11 on the correcting support 21, the two correcting guide plates 25 are symmetrically arranged along the correcting support 21, a sliding groove matched with the solar cell module is formed in the inner side of each correcting guide plate 25, and the clamping mechanism is installed at the correcting support and is used for correcting the solar cell module.
The clamping mechanism comprises a driving motor arranged along the vertical direction, the driving motor is arranged on a motor mounting plate at the upper part of the correcting conveying belt, and the motor mounting plate is arranged on the rack 1 and is parallel to the correcting bracket 21; a driving gear 24 is installed on a motor shaft of the driving motor 24, rack grooves are formed in motor installation plates on two sides of the driving gear 24, the two rack grooves are arranged in a diagonal manner, and a rack 23 meshed with the driving gear 24 is installed in each rack groove in a sliding manner; one end of each rack 23 is meshed with the driving gear 24, and the other end is provided with a clamping plate 22; the two clamping plates 22 are respectively positioned at two sides of the correction conveyer belt, are in movable fit with the solar cell modules placed on the correction conveyer belt, are close to or far away from the solar cell modules and are used for correcting the solar cell modules; when the solar cell module is close to the solar cell module, the solar cell module is clamped, and the purpose of correction is achieved; when the solar cell module is far away from the testing mechanism, the calibration conveying belt conveys the solar cell module to the testing mechanism.
As shown in fig. 2 and 3, the testing mechanism includes a testing support 31, a testing conveyer belt, a lifting cylinder 332 and a testing frame 333, the testing conveyer belt is rotatably mounted on the testing support 31, a testing guide plate 32 is mounted at one end of the testing support 31 far away from the calibration support, the two testing guide plates 32 are symmetrically arranged along the testing support, a cylinder support 331 is mounted on a rack on the upper portion of the testing support, the lifting cylinder 332 is mounted on the cylinder support 331, the testing frame 333 is mounted on a piston rod of the lifting cylinder, a grounding tester 334 is fixedly mounted on the testing frame, and the grounding tester 334 is in contact with the solar battery component under the action of the lifting cylinder to test the solar battery component on the testing conveyer belt.
The output mechanism comprises an output support 41, an output conveyor belt and output guide plates 42, the output conveyor belt is rotatably arranged on the output support 41, the output direction of the output conveyor belt is perpendicular to the input direction of the input conveyor belt, the output guide plates 42 are arranged on a rack at the output end of the output conveyor belt, and the two output guide plates 42 are symmetrically arranged along the output support 41.
The invention also relates to a method for correcting and testing the grounding of the solar cell module, which comprises the following steps:
(1) inputting a solar cell module;
(2) correcting and adjusting the position of the input solar cell module;
(3) testing the corrected solar cell module;
(4) displaying and storing the tested data;
(5) and outputting the tested solar cell module, and performing the next process.
In the step (1), the input conveyor belt conveys the solar cell module, and the output of the solar cell module is finished under the guidance of the input guide plate; in the step (5), the output conveyor belt outputs the solar cell module, and the output of the solar cell module is completed under the guidance of the output guide plate.
And (2) driving the driving gear to rotate by the driving motor to drive the racks on two sides of the driving gear to slide in a reciprocating manner, driving the clamping plate arranged on the racks to move in a reciprocating manner when the racks slide, so that the solar cell module on the correction conveying belt is corrected, and the guiding output of the solar cell module is finished under the action of the correction guide plate.
In the step (3), the lifting cylinder drives the test frame to move downwards to drive the grounding tester to contact with the solar cell module on the test conveyer belt and perform testing, and after the testing is finished, the lifting cylinder drives the test frame to move upwards and the test conveyer belt drives the solar cell module to output.
The input mechanism, the correcting mechanism, the testing mechanism, the output mechanism and the control platform are arranged on the rack in sequence, and the input mechanism, the correcting mechanism, the testing mechanism and the output mechanism are all connected to the control platform; the input mechanism is used for inputting the solar cell module, and the correction mechanism is used for adjusting the position of the input solar cell module; the testing mechanism is used for testing the corrected solar cell module; the output mechanism is used for outputting the tested solar cell module and carrying out the next process, and the assembly line detection of the solar cell module is rapidly completed through the arrangement of the series of structures.
Claims (10)
1. A solar module correction and grounding test system is characterized by comprising a rack, and an input mechanism, a correction mechanism, a test mechanism, an output mechanism and a control platform which are sequentially arranged on the rack, wherein the input mechanism, the correction mechanism, the test mechanism and the output mechanism are all connected to the control platform; the input mechanism is used for inputting the solar cell module, and the correction mechanism is used for adjusting the position of the input solar cell module; the testing mechanism is used for testing the corrected solar cell module; the output mechanism is used for outputting the tested solar cell module and carrying out the next process.
2. The system according to claim 1, wherein the input mechanism comprises an input support, an input conveyor belt and input guide plates, the input conveyor belt is rotatably mounted on the input support, four input guide plates are uniformly mounted on the frame around the input conveyor belt, and a chute matched with the solar cell module is arranged on the inner side of each input guide plate; two input guide plates are arranged on one side of the input conveyor belt, and two input guide plates are arranged on the other side of the input conveyor belt; each of the input guide plates has a portion disposed adjacent to the input conveyor belt and another portion disposed outside the input conveyor belt.
3. The system according to claim 1 or 2, wherein the correcting mechanism comprises a correcting bracket, a correcting conveyor belt, a correcting guide plate and a clamping mechanism, the correcting conveyor belt is rotatably mounted on the correcting bracket, two correcting guide plates are mounted on the rack at one end of the correcting bracket, which is far away from the input bracket, the two correcting guide plates are symmetrically arranged along the correcting bracket, a sliding groove matched with the solar cell module is arranged on the inner side of each correcting guide plate, and the clamping mechanism is mounted at the correcting bracket to correct the solar cell module.
4. The solar cell module calibration and grounding test system according to claim 3, wherein the clamping mechanism comprises a driving motor arranged along the vertical direction, the driving motor is mounted on a motor mounting plate at the upper part of the calibration conveying belt, the motor mounting plate is mounted on the rack and is arranged in parallel with the calibration bracket; a motor shaft of the driving motor is provided with a driving gear, rack grooves are formed in motor mounting plates on two sides of the driving gear, the two rack grooves are arranged in a diagonal manner, and a rack meshed with the driving gear is slidably mounted in each rack groove; one end of each rack is meshed with the driving gear, and the other end of each rack is provided with a clamping plate; the two clamping plates are respectively positioned at two sides of the correction conveying belt, are in movable fit with the solar cell modules placed on the correction conveying belt, are close to or far away from the solar cell modules, and correct the solar cell modules.
5. The system according to claim 4, wherein the testing mechanism comprises a testing support, a testing conveyer belt, a lifting cylinder and a testing frame, the testing conveyer belt is rotatably mounted on the testing support, a testing guide plate is mounted at one end of the testing support, which is far away from the calibrating support, the two testing guide plates are symmetrically arranged along the testing support, a cylinder support is mounted on a rack at the upper part of the testing support, the lifting cylinder is mounted on the cylinder support, the testing frame is mounted on a piston rod of the lifting cylinder, and a grounding tester is fixedly mounted on the testing frame and is in contact with the solar battery assembly under the action of the lifting cylinder to test the solar battery assembly on the testing conveyer belt.
6. The system according to claim 5, wherein the output mechanism comprises an output support, an output conveyor belt and output guide plates, the output conveyor belt is rotatably mounted on the output support, the output direction of the output conveyor belt is perpendicular to the input direction of the input conveyor belt, the output guide plates are mounted on the frame at the output end of the output conveyor belt, and the two output guide plates are symmetrically arranged along the output support.
7. A method for correcting and testing grounding of a solar cell module is characterized by comprising the following steps:
(1) inputting a solar cell module;
(2) correcting and adjusting the position of the input solar cell module;
(3) testing the corrected solar cell module;
(4) displaying and storing the tested data;
(5) and outputting the tested solar cell module, and performing the next process.
8. The method according to claim 7, wherein in the step (1), the input conveyor belt conveys the solar cell module, and the output of the solar cell module is completed under the guidance of the input guide plate; in the step (5), the output conveyor belt outputs the solar cell module, and the output of the solar cell module is completed under the guidance of the output guide plate.
9. The method for calibrating and testing the grounding of the solar cell module as claimed in claim 7, wherein in the step (2), the driving motor drives the driving gear to rotate, so as to drive the racks on both sides of the driving gear to slide back and forth, and the racks slide to drive the clamping plates mounted on the racks to move back and forth, so as to calibrate the solar cell module on the calibration conveying belt, and the solar cell module is guided and output under the action of the calibration guide plate.
10. The method according to claim 7, wherein in the step (3), the lifting cylinder drives the test frame to move downwards to drive the grounding tester to contact with the solar cell module on the test conveyor belt for testing, and after the test is completed, the lifting cylinder drives the test frame to move upwards to drive the test conveyor belt to drive the solar cell module to output.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011109561.7A CN112278708A (en) | 2020-10-16 | 2020-10-16 | Calibration and grounding test system and method for solar cell module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011109561.7A CN112278708A (en) | 2020-10-16 | 2020-10-16 | Calibration and grounding test system and method for solar cell module |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112278708A true CN112278708A (en) | 2021-01-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011109561.7A Pending CN112278708A (en) | 2020-10-16 | 2020-10-16 | Calibration and grounding test system and method for solar cell module |
Country Status (1)
| Country | Link |
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| CN (1) | CN112278708A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113636318A (en) * | 2021-08-09 | 2021-11-12 | 安徽兆拓新能源科技有限公司 | Outer frame profile arranging device for solar cell module processing |
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| CN209023741U (en) * | 2018-10-18 | 2019-06-25 | 无锡百晟科技有限公司 | A kind of conveying device with driving means |
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| JP2010056252A (en) * | 2008-08-28 | 2010-03-11 | Nisshinbo Holdings Inc | Tester for solar cell |
| CN202107332U (en) * | 2011-06-16 | 2012-01-11 | 北京北方微电子基地设备工艺研究中心有限责任公司 | Transmission equipment and support plate |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113636318A (en) * | 2021-08-09 | 2021-11-12 | 安徽兆拓新能源科技有限公司 | Outer frame profile arranging device for solar cell module processing |
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Application publication date: 20210129 |
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| RJ01 | Rejection of invention patent application after publication |