CN208367156U - A kind of solar cell Performance Test System - Google Patents
A kind of solar cell Performance Test System Download PDFInfo
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- CN208367156U CN208367156U CN201820728404.6U CN201820728404U CN208367156U CN 208367156 U CN208367156 U CN 208367156U CN 201820728404 U CN201820728404 U CN 201820728404U CN 208367156 U CN208367156 U CN 208367156U
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Abstract
The utility model embodiment provides a kind of solar cell Performance Test System, including inert gas filled aerostat and solar cell test module, the aerostat is connected with the solar cell test module, and the solar cell test module includes solar cell and the test device for testing solar battery performance.Solar cell test module is connected aerostat by the utility model, carries out loop test to the working performance of solar cell under high altitude environment, and records institute's measured data in real time.It is close in terms of the setting for making the environmental parameters such as light intensity, spatial distribution and the temperature tested in environment with actual environmental parameter, improves the accuracy of solar cell the performance test results.And solar cell test system structure provided by the utility model is simple, light-weight, can be applied to high hollow testing.
Description
Technical field
The utility model relates to aerostatics and solar cell applied technical fields, more particularly to a kind of solar cell
Performance Test System.
Background technique
In recent years, efficient spatial solar cell has significant progress, and is widely used near space field, is advection
The ideal non-renewable energy of the various near space vehicles such as layer dirigible, solar energy unmanned plane, aerostat.
When carrying out solar cell Performance Evaluation, need to obtain accurate performance ginseng of the solar cell near space environment
Number.And this test carried out at present on ground using solar simulator, in parameters such as light intensity, spatial distribution and environment temperatures
Setting in terms of with actual environment have difference, be not enough to reflect the real performance of solar cell.
Utility model content
The utility model is light intensity, spatial distribution and environment temperature etc. during solving traditional solar cell performance test
With the differentiated defect of actual environment in terms of the setting of parameter, a kind of solar cell Performance Test System and its detection side are provided
Method.
The utility model provides a kind of solar cell Performance Test System, including inert gas filled aerostat and too
Positive battery testing module, the aerostat are connected with the solar cell test module, the solar cell test module
Including solar cell and for the test device of testing solar battery performance.
Wherein, the system also includes parachute, gondola, the first hawser and the second hawsers；The parachute upper end passes through
First hawser is connected with the aerostat, and the lower end of the parachute is connected by the second hawser with the gondola
It connects；The solar cell test module is installed in the gondola.
Wherein, the test device include solar radiation sensor, solar cell temperature sensor, solar cell bracket,
Current sensor and voltage sensor；
The solar radiation sensor is for measuring solar radiation；The solar cell temperature sensor is for measuring the sun
The temperature of battery；The solar cell bracket is for carrying solar cell；The current sensor is for measuring through sun electricity
The electric current in pond, the voltage sensor are used to measure the voltage at the solar cell both ends.
Wherein, the test device further includes data recording equipment, and the data recording equipment is passed with the electric current respectively
Sensor, voltage sensor, solar radiation sensor are connected with solar cell temperature sensor, are passed for acquiring by solar radiation
The data of sensor, solar cell temperature sensor, voltage sensor and current sensor transmission.
Wherein, the test device further includes load component, the load component include switch controller, charge switch,
Capacitor, resistance and discharge switch；
Described charge switch one end connects the capacitor, and the other end is electric with the switch controller and the sun respectively
Pond is connected, and for receiving the instruction of switch controller, controls charging and cut-off of the solar cell to capacitor；
Described discharge switch one end connects the resistance, the other end respectively with the switch controller and the capacitor phase
Connection, for receiving the instruction of switch controller；Control electric discharge and cut-off of the resistance to capacitor.
Wherein, the solar cell is normal cell, battery component or is connected and/or composed in parallel by multiple battery components
Cell array
Wherein, the capacitor is single capacitor or capacitor array capacitors series connection and/or composed in parallel by more.
Wherein, the resistance is single resistance or electric resistance array resistance series connection and/or composed in parallel by more.
Solar cell test module is connected high-altitude by solar cell Performance Test System provided by the embodiment of the utility model
Balloon carries out loop test to the working performance of solar cell under high altitude environment, and records institute's measured data in real time.Make test wrapper
It is close, improves too with actual environmental parameter in terms of the setting of the environmental parameters such as light intensity, spatial distribution and temperature in border
The accuracy of positive electricity pond the performance test results.
Detailed description of the invention
Fig. 1 is the structural schematic diagram according to solar cell Performance Test System provided by the embodiment of the utility model；
Fig. 2 is the structural schematic diagram according to test device provided by the embodiment of the utility model；
Fig. 3 is the structural schematic diagram according to load component provided by the embodiment of the utility model；
Fig. 4 is the scene schematic diagram separated according to aerostat provided by the embodiment of the utility model with parachute；
In figure, 1. aerostats；2. the first hawser；3. parachute；4. gondola；5. solar cell test module；6. the sun
Battery；7. solar radiation sensor；8. solar cell temperature sensor；9. solar cell bracket；10. data recording equipment；11.
Voltage sensor；12. load component；13. current sensor；14. charge switch；15. discharge switch；16. switch controller；
17. capacitor；18. resistance；19. the second hawser.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, is explicitly described the technical scheme in the embodiment of the utility model, it is clear that described reality
Applying example is one module embodiments of the utility model, instead of all the embodiments.Based on the embodiments of the present invention, ability
It is practical new to belong to this for domain those of ordinary skill every other embodiment obtained without making creative work
The range of type protection.
Fig. 1 is the structural schematic diagram according to solar cell Performance Test System provided by the embodiment of the utility model.Such as Fig. 1
Shown, solar cell Performance Test System includes inert gas filled aerostat 1 and solar cell test module 5, described
Aerostat 1 is connected with the solar cell test module 5, the solar cell test module 5 include solar cell 6 and
Test device for testing solar battery performance.
Solar cell is the semiconductor component that can effectively absorb solar energy, and convert it into electric energy.With Ban conductor Gui ﹑
The luminous energy of the sun is become the device of electric energy by the materials such as copper indium gallium selenide.It is excellent with the property leaned on high ﹐ service life long ﹐ transfer efficiency height etc.
Point.When carrying out solar cell Performance Evaluation, need to obtain accurate performance parameter of the solar cell near space environment.And
This test carried out at present on ground using solar simulator, in setting for the parameters such as light intensity, spatial distribution and environment temperature
Setting aspect and actual environment has difference, is not enough to reflect the real performance of solar cell.Therefore it needs to carry out solar cell real
Performance test in the near space environment of border.Carrying out this test needs suitable carrier.In the prior art, available
Carrier is exactly stratospheric airship, solar energy unmanned plane and aerostat.The system complex of stratospheric airship and solar energy unmanned plane,
It is at high cost, manipulation difficulty is big, be not suitable for being used to the special testing experiment for carrying out solar cell.In comparison, aerostat system
Easy to operate, achievable near space flight in sky, is proper carrier.Aerostat is also known as High altitude scientific balloon, is
Refer to the unpowered aerostatics in stratosphere flight, refers in particular to zero-pressure formula aerostat in the narrow sense.Since aerostat is cheap, group
Active flight is convenient, the test period is short, therefore increasingly by the favor of scientific worker.
Referring to Fig.1, solar cell Performance Test System includes inert gas filled aerostat 1 and solar cell test
Module 5, the aerostat 1 are connected with the solar cell test module 5, and the solar cell test module 5 includes too
Positive electricity pond and test device for testing solar battery performance.Solar cell test module 5 is connected into aerostat 1, it is high
It is filled with inert gas in air balls 1, the solar cell test module 5 is driven to go up to the air.To solar cell 6 under high altitude environment
Working performance carries out loop test, and real-time recorded data.
Solar cell test module 5 is connected height by solar cell Performance Test System provided by the embodiment of the utility model
Air balls 1 carry out loop test to the working performance of solar cell 6 under high altitude environment, and record institute's measured data in real time.Make to survey
It is close, improves with actual environmental parameter in terms of the setting of the environmental parameters such as light intensity, spatial distribution and temperature in test ring border
The accuracies of solar cell the performance test results.
On the basis of the above embodiments, the system also includes parachute 3, gondola 4, the first hawser 2 and the second hawsers
19；3 upper end of parachute is connected by first hawser 2 with the aerostat 1, and the lower end of the parachute 3 is logical
The second hawser 19 is crossed to be connected with the gondola 4；The solar cell test module 5 is installed in the gondola 4.
As shown in Figure 1, solar cell test module 5 is installed in the gondola 4.4 upper end of gondola passes through the second hawser 19
Connect the lower end of parachute 3.The upper end of parachute 3 connects aerostat 1 by the first hawser 2.Inertia is filled in aerostat 1
Gas drives the solar cell test module 5 to go up to the air.Loop test is carried out to the working performance of solar cell 6.Aerostat
It is recorded in real time in 1 flight course and transmits institute's measured data.After the completion of test, the first hawser 2 is cut off, releases a parachute 3, by gondola
4 slow be down to ground and recycled.
The present embodiment carries out loop test to the working performance of solar cell under high altitude environment, and records surveyed number in real time
According to.Improve the accuracy of solar cell the performance test results.The system structure is simple, at low cost.After the completion of test, utilize
Parachute 3 recycles solar cell test module 5, reduces costs.
Fig. 2 is the structural schematic diagram according to test device provided by the embodiment of the utility model, as shown in Fig. 2, test dress
It sets and is passed including solar radiation sensor 7, solar cell temperature sensor 8, solar cell bracket 9, current sensor 13 and voltage
Sensor 11；
The solar radiation sensor 7 is for measuring solar radiation；The solar cell temperature sensor 8 is for measuring too
The temperature in positive electricity pond 6；The solar cell bracket 9 is for carrying solar cell 6；The current sensor 13 passes through for measuring
The electric current of solar cell 6, the voltage sensor 11 are used to measure the voltage at 6 both ends of solar cell.
Referring to Fig. 2, solar cell 6 is separately connected solar radiation sensor 7, solar cell temperature sensor 8, solar cell
Bracket 9, current sensor 13 and voltage sensor 11.Wherein, solar radiation sensor 7 is for measuring solar radiation；It is described too
Positive battery temperature sensor 8 is used to measure the temperature of solar cell 6；The solar cell bracket 9 is for carrying solar cell 6；
The current sensor 13 is used to measure the electric current by solar cell 6, and the voltage sensor 11 is for measuring the sun
The voltage at 6 both ends of battery.
The present embodiment tests the work in every performance to solar cell under high altitude environment, and is provided with intensity of solar radiation
With the test of solar cell temperature, compared with existing solar cell test macro, test data is more comprehensive.
On the basis of the various embodiments described above, the test device further includes data recording equipment 10, the data record
Equipment 10 respectively with the current sensor 13, voltage sensor 11, solar radiation sensor 7 and solar cell temperature sensor
8 are connected, for acquiring by solar radiation sensor 7, solar cell temperature sensor 8, voltage sensor 11 and current sense
The data that device 13 transmits.
The present embodiment tests the work in every performance to solar cell under high altitude environment, and records institute's measured data in real time.
Improve the accuracy of solar cell the performance test results.
On the basis of the various embodiments described above, the test device further includes load component 12, and the load component 12 wraps
Include switch controller 16, charge switch 14, capacitor 17, resistance 18 and discharge switch 15；
Described 14 one end of charge switch connects the capacitor 17, the other end respectively with the switch controller 16 and described
Solar cell 6 is connected, and for receiving the instruction of switch controller 16, controls charging and cut-off of the solar cell 6 to capacitor 17；
Described 15 one end of discharge switch connects the resistance 18, the other end respectively with the switch controller 16 and described
Capacitor 17 is connected, for receiving the instruction of switch controller 16；Control electric discharge and cut-off of the resistance 18 to capacitor 17.
Fig. 3 is the structural schematic diagram according to load component 12 provided by the embodiment of the utility model, as shown in figure 3, load
Component 12 includes switch controller 16, charge switch 14, capacitor 17, resistance 18 and discharge switch 15.
Specifically, the step of solar cell performance test includes:
Firstly, switch controller 16 is arranged according to the requirement of 1 message transmission rate of aerostat controls charge switch respectively
14 and discharge switch 15 closure with disconnect duration.Wherein, the control sequential of switch controller 16 is set are as follows: charges in capacitor 17
In period, charge switch 14 is closed, and discharge switch 15 disconnects；It discharges in the period in capacitor 17, charge switch 14 disconnects, and electric discharge is opened
Close 15 closures.
Then, according to the control sequential of setting and duration, switch controller 16 issues instruction, and charge switch 14 is closed, puts
Electric switch 15 disconnects, and solar cell 6 is the charging of capacitor 17, and in the process, 10 synchronous acquisition of data recording equipment is by sun spoke
Penetrate the data that sensor 7, solar cell temperature sensor 8, voltage sensor 11 and current sensor 13 transmit；Reach setting
After duration, switch controller 16 issues instruction, and charge switch 14 disconnects, and discharge switch 15 is closed, and resistance 18 is the electric discharge of capacitor 17.
So far, the sweep test of a solar cell performance is completed.After the completion of single sweep operation test, repeat the above steps, to the sun
The working performance of battery 6 carries out loop test.And drive solar cell test module 5 under high altitude environment using aerostat 1
Loop test is carried out to the working performance of solar cell 6.
Fig. 4 is the scene schematic diagram isolated with parachute 3 according to aerostat 1 provided by the embodiment of the utility model, such as
Shown in Fig. 4, after the completion of solar cell performance test, cut off the first hawser 2, release a parachute 3, by gondola 4 it is slow be down to ground into
Row recycling.
Existing solar cell measuring technology can be divided into two classes.One kind is surveyed using portable battery performance test instrument
Amount, usually once measures a curve, not can be carried out sequential scan tests.Another kind of solar cell test macro can continuously be swept
Retouch test, but system complex, it is desirable that data sampling frequency is high, traffic rate is fast, applied and be difficult to reality on aerostat 1
Now monitor in real time；The test of system not set intensity of solar radiation and solar cell temperature, test data be not comprehensive；Test macro
Weight is big, it is difficult to apply on aerostat 1.
The present embodiment, which is realized, carries out loop test to the performance of solar cell.And solar cell provided by the utility model
Test system structure is simple, light-weight, can be applied to high hollow testing.
On the basis of the various embodiments described above, the solar cell 6 is for normal cell, battery component or by multiple battery packs
The cell array that part is connected and/or composed in parallel.
The capacitor 17 is single capacitor or capacitor array capacitors series connection and/or composed in parallel by more.
The resistance 18 is single resistance or electric resistance array resistance series connection and/or composed in parallel by more.
Finally, it should be noted that above embodiments are only to illustrate according to technical side provided by the embodiment of the utility model
Case, rather than its limitations；Although the utility model is described in detail with reference to the foregoing embodiments, for the general of this field
For logical technical staff, it is possible to understand that can in the case where not departing from according to principle provided by the embodiment of the utility model and spirit
It is all according to spirit provided by the embodiment of the utility model to carry out a variety of change, modification, replacement and modification to these embodiments
Within principle, any modification, equivalent replacement, improvement and so on should be included in and be provided according to the utility model embodiment
Protection scope within.
Claims (8)
1. a kind of solar cell Performance Test System, which is characterized in that including inert gas filled aerostat and sun electricity
Pond test module, the aerostat are connected with the solar cell test module, and the solar cell test module includes
Solar cell and test device for testing solar battery performance.
2. system according to claim 1, which is characterized in that the system also includes parachute, gondola, the first hawser and
Second hawser；The parachute upper end is connected by first hawser with the aerostat, the lower end of the parachute
It is connected by the second hawser with the gondola；The solar cell test module is installed in the gondola.
3. system according to claim 1, which is characterized in that the test device includes solar radiation sensor, the sun
Battery temperature sensor, solar cell bracket, current sensor and voltage sensor；
The solar radiation sensor is for measuring solar radiation；The solar cell temperature sensor is for measuring solar cell
Temperature；The solar cell bracket is for carrying solar cell；The current sensor is used to measure through solar cell
Electric current, the voltage sensor are used to measure the voltage at the solar cell both ends.
4. system according to claim 3, which is characterized in that the test device further includes data recording equipment, described
Data recording equipment is sensed with the current sensor, voltage sensor, solar radiation sensor and solar cell temperature respectively
Device is connected, and is passed for acquiring by solar radiation sensor, solar cell temperature sensor, voltage sensor and current sensor
Defeated data.
5. system according to claim 4, which is characterized in that the test device further includes load component, the load
Component includes switch controller, charge switch, capacitor, resistance and discharge switch；
Described charge switch one end connects the capacitor, the other end respectively with the switch controller and the solar cell phase
Connection controls charging and cut-off of the solar cell to capacitor for receiving the instruction of switch controller；
Described discharge switch one end connects the resistance, and the other end is connected with the switch controller and the capacitor respectively
It connects, for receiving the instruction of switch controller, controls electric discharge and cut-off of the resistance to capacitor.
6. system according to claim 1, which is characterized in that the solar cell be normal cell, battery component or by
Multiple cell arrays battery component series connection and/or composed in parallel.
7. system according to claim 5, which is characterized in that the capacitor is single capacitor or is connected by more capacitors
And/or the capacitor array composed in parallel.
8. system according to claim 5, which is characterized in that the resistance is single resistance or is connected by more resistance
And/or the electric resistance array composed in parallel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820728404.6U CN208367156U (en) | 2018-05-16 | 2018-05-16 | A kind of solar cell Performance Test System |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820728404.6U CN208367156U (en) | 2018-05-16 | 2018-05-16 | A kind of solar cell Performance Test System |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108919080A (en) * | 2018-05-16 | 2018-11-30 | 中国科学院光电研究院 | A kind of solar cell Performance Test System and its test method |
| CN109916927A (en) * | 2019-02-28 | 2019-06-21 | 合刃科技（深圳）有限公司 | Defect inspection method, system and device in a kind of battery |
| CN110963017A (en) * | 2019-11-01 | 2020-04-07 | 中国科学院光电研究院 | Planet sampling reentry module carries on platform |
-
2018
- 2018-05-16 CN CN201820728404.6U patent/CN208367156U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108919080A (en) * | 2018-05-16 | 2018-11-30 | 中国科学院光电研究院 | A kind of solar cell Performance Test System and its test method |
| CN109916927A (en) * | 2019-02-28 | 2019-06-21 | 合刃科技（深圳）有限公司 | Defect inspection method, system and device in a kind of battery |
| CN110963017A (en) * | 2019-11-01 | 2020-04-07 | 中国科学院光电研究院 | Planet sampling reentry module carries on platform |
| CN110963017B (en) * | 2019-11-01 | 2021-10-22 | 中国科学院空天信息创新研究院 | Planet sampling reentry module carries on platform |
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