WO2019041965A1 - 用于柔性太阳能电池性能测试的支撑装置及测试方法 - Google Patents

用于柔性太阳能电池性能测试的支撑装置及测试方法 Download PDF

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Publication number
WO2019041965A1
WO2019041965A1 PCT/CN2018/091132 CN2018091132W WO2019041965A1 WO 2019041965 A1 WO2019041965 A1 WO 2019041965A1 CN 2018091132 W CN2018091132 W CN 2018091132W WO 2019041965 A1 WO2019041965 A1 WO 2019041965A1
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WIPO (PCT)
Prior art keywords
solar cell
flexible solar
plane frame
placement plane
battery
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PCT/CN2018/091132
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English (en)
French (fr)
Inventor
姜中钱
黄显艺
刘红刚
连重炎
薛朝伟
胡鹏臣
龙巍
Original Assignee
米亚索乐装备集成（福建）有限公司
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Application filed by 米亚索乐装备集成（福建）有限公司 filed Critical 米亚索乐装备集成（福建）有限公司
Priority to EP18842694.4A priority Critical patent/EP3691115A1/en
Publication of WO2019041965A1 publication Critical patent/WO2019041965A1/zh

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    • 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

Definitions

  • the present application relates to a support device, and more particularly to a support device and a test method for performance testing of a flexible solar cell.
  • the flexible solar cell is a kind of thin film solar cell, and has the advantages of advanced technology, excellent performance, low cost and wide application. Its components can be applied to BIPV (Building Integrated Photovoltaic), solar charging treasure, solar backpack, solar tent, solar flashlight, solar car and even solar aircraft.
  • BIPV Building Integrated Photovoltaic
  • the solar cell main body 100 is made of a conductive material which can be attracted by a magnet as a substrate.
  • the front side is coated, the back side is the battery electrode I, the solar cell main body 100 has the electrode II lead end 200, and the electrode II is led out by the gate electrode 300. Since the electrodes I and II are respectively located on different surfaces of the solar cell theme 100, the two electrodes are displaced up and down, and the upper and lower probes cannot be directly connected to the power source, and such batteries are flexible and difficult to fix when placed.
  • the purpose of the present application is to provide a support device and a test method for the performance test of a flexible solar cell to solve the technical problem that the flexible solar cell in the related art is difficult to fix and difficult to access in two stages of the power supply, and can effectively support and fix Flexible solar cells improve the efficiency of flexible solar cell performance testing and the accuracy of test results.
  • the present application provides a support device for a flexible solar cell performance test, comprising a battery placement plane frame, a magnet and a bus bar, the battery placement plane frame and the bus bar are conductors, and the magnet is adsorbed in the
  • the battery is placed on the surface of one side of the plane frame, and the other side of the battery is placed on the surface of the plane frame is provided with an insulating tape, and the bus bar is fixed on the insulating tape under the magnetic attraction of the magnet.
  • the electrode II terminal of the flexible solar cell is pressed into the range of the insulating tape; the bus bar is provided with a first power connection line, and the battery placement plane frame is provided with a second power source. Connection line.
  • the frame body and the connecting rod are further included, and the connecting rods are two, which are oppositely mounted on the frame body, and the battery placement plane frame can be Rotatingly mounted between the two connecting rods.
  • the frame body comprises a bottom rod, a main rod and a cross beam, and the bottom rod and the main rod are both two, the main rod is vertical Arranging in a straight direction, the bottom rods are arranged in a horizontal direction, and the bottoms of the two main rods are respectively fixedly connected to one of the bottom rods; the cross beams are at least two, and are fixedly disposed between two of the main rods .
  • the opposite sides of the two main rods are provided with slide rails, and the connecting rods are mounted on the slide rails by bolt assemblies.
  • the beam is three, wherein two of the beams are disposed at the top and the bottom of the main rod, and the remaining one of the beams is disposed at the The middle of the main pole.
  • the connecting rod is made of an insulating material
  • the connecting rod comprises a mounting section and an angle adjusting section, and the two are an integral J-shaped structure, a mounting portion mounting hole, a first mounting hole and a second mounting hole are sequentially arranged from top to bottom on the mounting section, and the connecting rod is installed through the first mounting hole and the second mounting hole and the bolt assembly
  • the angle adjusting section is provided with an arc angle adjusting hole, the upper end of the battery placing plane frame is connected with the plane frame mounting hole, and the lower end is connected with the arc angle adjusting hole.
  • the battery placement plane frame is provided with four connecting portions, wherein the upper two connecting portions are rotatable through the rotating shaft and the plane mounting hole The two lower connecting portions are connected to the arcuate angle adjusting hole by a locking member.
  • the insulating tape is an insulating tape pasted on the surface of the other side of the battery placement plane frame.
  • the lower portion of the battery placement plane frame is provided with a boss, and the boss and the bus bar are located on the same side of the battery placement plane frame.
  • the present application also provides a performance testing method for a flexible solar cell, which is applied to a supporting device as described above, the method comprising:
  • the flexible solar cell which is made of a conductive material capable of being attracted by a magnet, on the battery placement plane, such that the electrode II terminal of the flexible solar cell is placed on the insulating tape,
  • the electrode I on the back side of the solar cell body of the flexible solar cell is in direct contact with the cell placement plane frame;
  • the first power connection line and the second power connection line are respectively connected to a power source to perform performance analysis on the flexible solar cell.
  • the method further includes:
  • the insulating tape is an insulating tape adhered to a plate surface on the other side of the battery placement plane frame.
  • the method further includes:
  • the angle at which the battery is placed in the plane frame is adjusted by the connecting rod.
  • the present application provides a support device for a flexible solar cell performance test, comprising a battery placement plane frame, a magnet and a bus bar, the battery placement plane frame and the bus bar are conductors, and the magnet is adsorbed in the
  • the battery is placed on the surface of one side of the plane frame, and the other side of the battery is placed on the surface of the plane frame is provided with an insulating tape, and the bus bar is fixed on the insulating tape under the magnetic attraction of the magnet.
  • a second power source is disposed on the bus bar with a first power connection line, and a second power source is disposed on the bus bar. Connection line.
  • This application uses a special support device instead of the manual fixing method, which greatly improves the performance test efficiency.
  • a flexible solar cell is carried by a battery placed flat frame, and the effective fixing of the flexible solar cell is realized by the magnet and the bus bar, which not only improves the fixing efficiency of the flexible solar cell, but also can effectively improve the accuracy of the performance test.
  • Figure 1 is a structural view of a flexible substrate solar cell
  • FIG. 2 is a view showing a state of use of an embodiment of the present application
  • Figure 3 is a schematic view showing the structure of a magnet adsorbed on the back of a battery rack
  • Figure 5 is an isometric view of the frame
  • Figure 6 is an isometric view of the connecting rod
  • Figure 7 is an isometric view of the battery placement plane frame
  • FIG. 8 is a flow chart of a performance testing method for a flexible solar cell according to an embodiment of the present application.
  • FIG. 9 is a flow chart of a performance testing method for a flexible solar cell provided by another embodiment of the present application.
  • a supporting device for a flexible solar cell performance test includes a battery placement plane frame 3, a magnet 4, and a bus bar 5, the battery placement plane frame 3 and The bus bars 5 are all conductors, the magnets 4 are adsorbed on the surface of the battery placement plane frame 3, and the other side of the battery placement plane frame 3 is provided with an insulating tape.
  • the bus bar 5 is fixed on the insulating tape under the magnetic attraction of the magnet 4 for pressing the lead end of the motor II of the flexible solar cell within the range of the insulating tape; the bus bar 5 is provided with a first power connection line 18, and the battery placement plane frame 3 is provided with a second power connection line 19.
  • the insulating tape is an insulating tape 17 adhered to the surface of the battery placing plane frame 3, and the insulating tape 17 and the magnet 4 are located on the two plate faces opposite to the battery placing plane frame 3.
  • the insulating tape 17 may not be attached to the battery placement plane frame 3 when the support device is in a non-use state; and is attached to the battery placement plane frame 3 when the support device is in use.
  • the insulating tape may be an insulating coating formed directly on the surface of the battery placement plane frame 3.
  • the insulating tape 17 is first applied in the lateral direction on the upper portion of the battery placing plane frame 3, and then the flexible solar cell in which the conductive material capable of being attracted by the magnet 4 is used as a substrate is placed on the battery.
  • the flat frame 3 is placed, and the electrode II terminal 200 is placed on the insulating tape 17, and the back surface of the solar cell main body 100 (i.e., the electrode I) is in direct contact with the battery placement plane frame 3.
  • the bus bar 5 is placed on the terminal end 200 of the electrode II and is located within the range of the insulating tape 17, and since the bus bar 5 can be attracted by the magnet 4, the bus bar 5 can press the terminal end 200 of the electrode II.
  • the first power connection line 18 and the second power connection line 19 are respectively connected to the power source to perform performance analysis on the flexible solar cell.
  • the present application makes full use of the characteristics that the flexible solar cell can be adsorbed by the magnet, and the fast fixing of the flexible solar cell is realized by placing the plane frame 3 and the magnet 4 on the battery, thereby effectively improving the fixing efficiency.
  • the battery placement plane frame 3 and the bus bar 5 are both conductors, the bus bar 5 can be connected to each electrode II terminal 200, and then connected to the power source through the first power connection line 18, and the battery placement plane frame 3 can be connected to each electrode I. And then accessing the power source through the second power connection line 19, effectively solving the problem that the electrodes of the flexible solar battery are inconvenient to connect.
  • the present application further includes a frame body 1 and a connecting rod 2, and the connecting rods 2 are two, oppositely mounted on the frame body 1, the battery is placed.
  • the plane frame 3 is rotatably mounted between the two connecting rods 2.
  • the connecting rod 2 should have an insulating effect, and is preferably made of an insulating material; of course, a non-insulating material can also be used, and when a non-insulating material is used, it is necessary to pass a brush insulating coating or an insulating sleeve on the outside. Make it insulated.
  • the inner side of the connecting rod 2 is provided with a slide rail.
  • the battery placement plane frame 3 can be adjusted in angle by the connecting rod 2 to meet the requirements of different angles when performing performance analysis on the flexible solar cell.
  • the lower portion of the battery placement plane frame 3 is provided with a boss 16, a boss 16 and a bus bar. 5 is on the same side.
  • the frame body 1 includes a bottom rod 6, a main rod 7 and a beam 8, and the bottom rod 6 and the main rod 7 are both two.
  • the main rod 7 is in the vertical direction.
  • the bottom rods 6 are arranged in a horizontal direction, and the bottoms of the two main rods 7 are respectively fixedly connected to one bottom rod 6; at least two beams 8 are fixedly disposed between the two main rods 7.
  • the frame 1 adopting such a structure not only has a simple structure, a low manufacturing cost, but also the strength of the frame can meet the use requirements.
  • the opposite sides (ie, the inner side) of the two main rods 7 are provided with slide rails, and the connecting rods 2 are mounted on the slide rails by bolt assemblies, in particular, the nut portions of the screw can be installed.
  • the screw is passed through the mounting hole on the connecting rod 2 and then fixed by the nut.
  • the rail structure can adopt various forms.
  • the bolt assembly can be replaced with The connector of the corresponding track structure can be used.
  • the beam 8 is preferably three, two of which are disposed at the top and the bottom of the main rod 7, and the remaining one of the beams 8 is disposed at the middle or the upper portion of the main rod 7.
  • the connecting rod 2 is made of an insulating material, and includes a mounting section 9 and an angle adjusting section 10, which are an integral "J"-shaped structure, and the mounting section 9 is sequentially arranged from top to bottom.
  • a plane mounting hole 11 There is a plane mounting hole 11, a first mounting hole 12 and a second mounting hole 13, and the connecting rod 2 is mounted on the sliding rail through the first mounting hole 12 and the second mounting hole 13 and the bolt assembly; the angle adjusting section 10 is provided
  • the arc angle adjusting hole 14 is connected to the plane frame mounting hole 11 at the upper end of the battery placing plane frame 3, and the lower end is connected to the curved angle adjusting hole 14.
  • the battery placement plane frame 3 is provided with four connecting portions 15, wherein the upper two connecting portions 15 are rotatably connected to the plane frame mounting hole 11 through the rotating shaft, and the lower two connecting portions 15 pass the locking member and the curved angle adjusting hole 14 connection.
  • FIG. 8 is a flow chart of a performance testing method for a flexible solar cell according to an embodiment of the present application.
  • the method can be used in a support device as shown in any of Figures 2 to 7, the method comprising:
  • Step 801 placing a flexible solar cell with a conductive material capable of being attracted by the magnet 4 as a substrate on the battery placement plane frame 3, so that the electrode II terminal 200 of the flexible solar cell is placed on the insulating tape, and the insulating tape may be
  • the battery is placed on the plane frame 3
  • the insulating coating on the battery placement plane frame 3 is directly formed, and the electrode I located on the back surface of the solar cell body 100 of the flexible solar cell is in direct contact with the battery placement plane frame 3;
  • Step 802 placing the bus bar 5 on the terminal end 200 of the electrode II, and located in the range of the insulating tape;
  • step 803 the first power connection line 18 and the second power connection line 19 are respectively connected to a power source for performance analysis of the flexible solar cell.
  • the flexible solar cell is carried by the battery placed plane frame, and the effective fixing of the flexible solar cell is realized by the magnet and the bus bar, which not only improves the fixing efficiency of the flexible solar cell, but also improves the fixing efficiency of the flexible solar cell. Can effectively improve the accuracy of performance testing of flexible solar cells.
  • FIG. 9 is a flow chart of a performance testing method for a flexible solar cell according to another embodiment of the present application.
  • the method can be used in a supporting device as shown in any one of FIGS. 2 to 7.
  • the insulating tape in the device may be an insulating tape 17 adhered to a battery mounting plane frame, the method comprising:
  • Step 901 in the upper portion of the battery placement plane frame 3 is affixed with insulating tape 17 in the transverse direction;
  • Step 902 placing a flexible solar cell with a conductive material capable of being attracted by the magnet 4 as a substrate on the battery placement plane frame 3, so that the electrode II terminal 200 of the flexible solar cell is placed on the insulating tape 17, located in the flexible solar cell.
  • the electrode I on the back side of the solar cell main body 100 is in direct contact with the battery placement plane frame 3;
  • Step 903 placing the bus bar 5 on the terminal end 200 of the electrode II, and located in the range of the insulating tape 17;
  • Step 904 the first power connection line 18 and the second power connection line 19 are respectively connected to the power source for performance analysis of the flexible solar cell;
  • step 905 the angle at which the battery is placed on the plane frame 3 is adjusted by the connecting rod 2.
  • the angle at which the battery placing plane frame 3 is adjusted can also be adjusted by the connecting rod 2.

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Abstract

本申请公开了一种用于柔性太阳能电池性能测试的支撑装置及测试方法，包括电池放置平面架、磁铁和汇流杆，所述电池放置平面架和所述汇流杆均为导体，所述磁铁吸附在所述电池放置平面架一侧的板面上，所述电池放置平面架的另一侧的板面上设有绝缘带，所述汇流杆在所述磁铁的磁力吸附作用下固定在所述绝缘带上，用于将所述柔性太阳能电池的电池II引出端压紧在所述绝缘带的范围内；所述汇流杆上设有第一电源连接线，所述电池放置平面架上设有第二电源连接线。本申请能够有效支撑并固定柔性太阳能电池，提高柔性太阳能电池性能测试的效率及测试结果的准确性。

Description

用于柔性太阳能电池性能测试的支撑装置及测试方法
本申请要求于2017年08月30日提交中国国家知识产权局、申请号为201721101938.8、实用新型名称为“用于柔性太阳能电池性能测试的支撑装置”的中国专利申请的优先权，其全部内容通过引用结合在本申请中。
技术领域
本申请涉及一种支撑装置，特别是一种用于柔性太阳能电池性能测试的支撑装置及测试方法。
背景技术
柔性太阳能电池是薄膜太阳能电池的一种，具有技术先进、性能优良、成本低廉和用途广泛等优点。其组件可应用于BIPV(Building Integrated Photovoltaic，光伏建筑一体化)、太阳能充电宝、太阳能背包、太阳能帐篷、太阳能手电筒，太阳能汽车甚至太阳能飞机上。
而在柔性太阳能电池中，有一种以能被磁铁吸引的导电材料作衬底的电池，其结构如图1所示，太阳能电池主体100以能被磁铁吸引的导电材料作衬底，该衬底正面镀膜，背面为电池电极Ⅰ，太阳能电池主体100上具有电极Ⅱ引出端200，电极Ⅱ由栅极300引出。由于电极Ⅰ和电极Ⅱ分别位于太阳能电池主题100的不同表面，其两电极上下错位，无法用上下探针直接接入电源，且此类电池柔性大，在放置时较难固定。在电池性能分析过程中，由于没有针对此类电池的成套固定和接入电源装置，大量时间往往会花费在电池的固定以及电源两极的接入上，且易产生电池表面不平，电极接触不良等影响电池性能分析的因素。
发明内容
本申请的目的是提供一种用于柔性太阳能电池性能测试的支撑装置及测试方法，以解决相关技术中的柔性太阳能电池难以固定和电源两级难以接入的技术问题，它能够有效支撑并固定柔性太阳能电池，提高柔性太阳能电池性能 测试的效率及测试结果的准确性。
本申请提供了一种用于柔性太阳能电池性能测试的支撑装置，包括电池放置平面架、磁铁和汇流杆，所述电池放置平面架和所述汇流杆均为导体，所述磁铁吸附在所述电池放置平面架一侧的板面上，所述电池放置平面架的另一侧的板面上设有绝缘带，所述汇流杆在所述磁铁的磁力吸附作用下固定在所述绝缘带上，用于将所述柔性太阳能电池的电极II引出端压紧在所述绝缘带的范围内；所述汇流杆上设有第一电源连接线，所述电池放置平面架上设有第二电源连接线。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，还包括架体和连接杆，所述连接杆为2根，相对地安装在所述架体上，所述电池放置平面架可转动地安装在2根所述连接杆之间。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述架体包括底杆、主杆和横梁，所述底杆和所述主杆均为2根，所述主杆沿竖直方向布置，所述底杆沿水平方向布置，2根所述主杆的底部分别固定连接1根所述底杆；所述横梁至少为2根，固定设置在2根所述主杆之间。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，2根所述主杆相对的侧面上设有滑轨，所述连接杆通过螺栓组件安装在所述滑轨上。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述横梁为3根，其中两根所述横梁设置在所述主杆的顶部和底部，剩余一根所述横梁设置在所述主杆的中部。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述连接杆采用绝缘材质制成，所述连接杆包括安装段和角度调节段，二者为一体式J字形结构，所述安装段上自上至下依次设有平面架安装孔、第一安装孔和第二安装孔，所述连接杆通过所述第一安装孔和所述第二安装孔和所述螺栓组件安装在所述滑轨上；所述角度调节段上设有弧形角度调节孔，所述电池放置平面架的上端与所述平面架安装孔连接，下端与所述弧形角度调节孔连接。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述电池放置平面架上设有4个连接部，其中上面2个所述连接部通过转轴与所述平面架安 装孔可转动连接，下面2个所述连接部通过锁紧件与所述弧形角度调节孔连接。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述绝缘带是粘贴在所述电池放置平面架的另一侧的板面上的绝缘胶带。
前述的用于柔性太阳能电池性能测试的支撑装置中，优选地，所述电池放置平面架的下部设有凸台，所述凸台与所述汇流杆位于所述电池放置平面架同侧。
本申请还提供了一种用于柔性太阳能电池的性能测试方法，应用于如上述的支撑装置中，所述方法包括：
将以能被磁铁吸引的导电材料做衬底的所述柔性太阳能电池放于所述电池放置平面架上，使得所述柔性太阳能电池的电极Ⅱ引出端置于所述绝缘带上，位于所述柔性太阳能电池的太阳能电池主体背面的电极Ⅰ与所述电池放置平面架直接接触；
将所述汇流杆放于所述电极Ⅱ引出端上，并位于所述绝缘胶带范围内；
将所述第一电源连接线和第二电源连接线分别接入电源，以便对所述柔性太阳能电池进行性能分析。
前述的用于柔性太阳能电池性能测试的性能测试方法中，优选地，所述方法还包括：
所述绝缘带是粘贴在所述电池放置平面架的另一侧的板面上的绝缘胶带。
前述的用于柔性太阳能电池性能测试的性能测试方法中，优选地，所述方法还包括：
通过所述连接杆调节所述电池放置平面架的角度。
本申请提供了一种用于柔性太阳能电池性能测试的支撑装置，包括电池放置平面架、磁铁和汇流杆，所述电池放置平面架和所述汇流杆均为导体，所述磁铁吸附在所述电池放置平面架一侧的板面上，所述电池放置平面架的另一侧的板面上设有绝缘带，所述汇流杆在所述磁铁的磁力吸附作用下固定在所述绝缘带上，用于将所述柔性太阳能电池的电机II引出端压紧在所述绝缘带的范围内；所述汇流杆上设有第一电源连接线，所述电池放置平面架上设有第二电源连接线。本申请使用专用支撑装置来代替人工固定方式，极大地提高了性能测试效率。本申请通过电池放置平面架来承载柔性太阳能电池，通过磁铁和汇流杆实现对柔性太阳能电池的有效固定，不但提高了柔性太阳能电池的固定效 率，而且能够有效提高性能测试的准确性。
附图说明
图1是柔性衬底太阳能电池结构图；
图2是本申请一种实施方式的使用状态图；
图3是磁铁吸附在电池放置平面架背面的结构示意图；
图4是本申请另一种实施方式的结构示意图；
图5是架体的轴测图；
图6是连接杆的轴测图；
图7是电池放置平面架的轴测图；
图8是本申请一种实施方式提供的用于柔性太阳能电池的性能测试方法的流程图；
图9是本申请另一种实施方式提供的用于柔性太阳能电池的性能测试方法的流程图。
附图标记说明：1-架体，2-连接杆，3-电池放置平面架，4-磁铁，5-汇流杆，6-底杆，7-主杆，8-横梁，9-安装段，10-角度调节段，11-平面架安装孔，12-第一安装孔，13-第二安装孔，14-弧形角度调节孔，15-连接部，16-凸台，17-绝缘胶带，18-第一电源连接线，19-第二电源连接线，100-太阳能电池主体，200-电极Ⅱ引出端，300-栅极。
具体实施方式
下面详细描述本申请的实施例，所述实施例的示例在附图中示出，其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的，仅用于解释本申请，而不能解释为对本申请的限制。
本申请的实施例：如图2和图3所示，一种用于柔性太阳能电池性能测试的支撑装置，包括电池放置平面架3、磁铁4和汇流杆5，所述电池放置平面架3和所述汇流杆5均为导体，所述磁铁4吸附在所述电池放置平面架3一侧的板面上，所述电池放置平面架3的另一侧的板面上设有绝缘带，所述汇流杆 5在所述磁铁4的磁力吸附作用下固定在所述绝缘带上，用于将所述柔性太阳能电池的电机II引出端压紧在所述绝缘带的范围内；所述汇流杆5上设有第一电源连接线18，所述电池放置平面架3上设有第二电源连接线19。
可选地，绝缘带是粘贴在所述电池放置平面架3的板面上的绝缘胶带17，绝缘胶带17与磁铁4位于电池放置平面架3相对的两个板面上。该绝缘胶带17在支撑装置处于非使用状态时，可以不粘贴在电池放置平面架3上；而当支撑装置处于使用状态时，再粘贴在电池放置平面架3上。或者该绝缘带也可以是直接形成在电池放置平面架3板面上的绝缘涂层。
具体地，当对柔性太阳能电池进行性能测试时，先在电池放置平面架3的上部沿横向粘贴绝缘胶带17，然后将以能被磁铁4吸引的导电材料作衬底的柔性太阳能电池放于电池放置平面架3上，并使得电极Ⅱ引出端200置于绝缘胶带17上，太阳能电池主体100的背面(即电极Ⅰ)与电池放置平面架3直接接触。将汇流杆5放于电极Ⅱ引出端200上，并位于绝缘胶带17范围内，由于汇流杆5可以被磁铁4吸引，因此汇流杆5可以压紧电极Ⅱ引出端200。然后将第一电源连接线18和第二电源连接线19分别接入电源便可对柔性太阳能电池进行性能分析。
本申请充分利用了柔性太阳能电池可以被磁铁吸附的特性，通过电池放置平面架3和磁铁4实现对柔性太阳能电池的快速固定，有效提高了固定效率。由于电池放置平面架3和汇流杆5均为导体，所以汇流杆5可以连接各电极Ⅱ引出端200，再通过第一电源连接线18接入电源，而电池放置平面架3可以连接各电极Ⅰ,再通过第二电源连接线19接入电源，有效解决柔性太阳能电池的电极不方便连接的问题。
在另一种实施方式中，如图4所示，本申请还包括架体1和连接杆2,所述连接杆2为2根，相对地安装在所述架体1上，所述电池放置平面架3可转动地安装在2根所述连接杆2之间。需要说明的是，连接杆2应当具备绝缘效果，优选采用绝缘材料制作；当然也可采用非绝缘材质，在采用非绝缘材质时需要在其外部通过刷绝缘涂层或套设绝缘套管等手段使其具备绝缘效果。连接杆2的内侧设置有滑轨。
通过该结构设计，电池放置平面架3可通过连接杆2调节角度，以满足对柔性太阳能电池进行性能分析时对不同角度的需求。
为了防止因误操作使柔性太阳能电池从电池放置平面架3上脱落，导致电池损坏，优选地，如图7所示，电池放置平面架3的下部设有凸台16，凸台16与汇流杆5位于同侧。通过设置凸台16起到底部限位的作用，可以有效防止柔性太阳能电池从电池放置平面架3上滑落。
下面对架体1做进一步说明，如图5所示，架体1包括底杆6、主杆7和横梁8，底杆6和主杆7均为2根，主杆7沿竖直方向布置，底杆6沿水平方向布置，2根主杆7的底部分别固定连接1根底杆6；横梁8至少为2根，固定设置在2根主杆7之间。采用这种结构的架体1不但结构简单、制造成本低，而且架体强度也能够满足使用需求。
在一种优选方案中，2根主杆7相对的侧面上(即内侧面)设有滑轨，连接杆2通过螺栓组件安装在滑轨上，具体地，可将螺杆上的螺帽部分安装在滑轨内，将螺杆穿过连接杆2上的安装孔后通过螺母进行固定，需要说明的是，轨道结构可以采用多种形式，当采用不同形式的轨道时，将螺栓组件替换成能够与相应轨道结构配合的连接件即可。横梁8优选为3根，其中两根横梁8设置在主杆7的顶部和底部，剩余一根所述横梁8设置在所述主杆7的中部或者中上部。通过滑轨的设置，使连接杆2可沿着轨道在上面两根横梁8之间调节位置，实现对柔性太阳能电池在竖直方向上的调节。
如图6所示，优选地，连接杆2采用绝缘材质制成，其包括安装段9和角度调节段10，二者为一体式“J”字形结构，安装段9上自上至下依次设有平面架安装孔11、第一安装孔12和第二安装孔13，连接杆2通过第一安装孔12和第二安装孔13和螺栓组件安装在滑轨上；角度调节段10上设有弧形角度调节孔14，电池放置平面架3的上端与平面架安装孔11连接，下端与弧形角度调节孔14连接。电池放置平面架3上设有4个连接部15，其中上面2个连接部15通过转轴与平面架安装孔11可转动连接，下面2个连接部15通过锁紧件与弧形角度调节孔14连接。
当需要调节电池放置平面架3的角度时，只需松动下面2个连接部15上 的锁紧件，然后转动电池放置平面架3至合适角度，然后再扭紧锁紧件即可。通过角度调节结构的设置，在测试柔性太阳能电池的性能时，可以满足不同的角度需求，使测量结果更准确。
图8是本申请一种实施方式提供的用于柔性太阳能电池的性能测试方法的流程图。该方法可以用于如图2至图7任一所示出的支撑装置中，该方法包括：
步骤801，将以能被磁铁4吸引的导电材料做衬底的柔性太阳能电池放于电池放置平面架3上，使得柔性太阳能电池的电极Ⅱ引出端200置于绝缘带上，绝缘带可以是在生产电池放置平面架3时直接形成在电池放置平面架3上的绝缘涂层，位于柔性太阳能电池的太阳能电池主体100背面的电极Ⅰ与电池放置平面架3直接接触；
步骤802，将汇流杆5放于电极Ⅱ引出端200上，并位于绝缘带范围内；
步骤803，将第一电源连接线18和第二电源连接线19分别接入电源，以便对柔性太阳能电池进行性能分析。
综上所述，本申请提供的性能测试方法中，通过电池放置平面架来承载柔性太阳能电池，通过磁铁和汇流杆实现对柔性太阳能电池的有效固定，不但提高了柔性太阳能电池的固定效率，而且能够有效提高柔性太阳能电池的性能测试的准确性。
图9是本申请另一实施方式提供的用于柔性太阳能电池的性能测试方法的流程图。该方法可以用于如图2至图7任一所示出的支撑装置中，该装置中的绝缘带可以是粘贴在电池放置平面架上的绝缘胶带17，该方法包括：
步骤901，在电池放置平面架3的上部沿横向粘贴绝缘胶带17；
步骤902，将以能被磁铁4吸引的导电材料做衬底的柔性太阳能电池放于电池放置平面架3上，使得柔性太阳能电池的电极Ⅱ引出端200置于绝缘胶带17上，位于柔性太阳能电池的太阳能电池主体100背面的电极Ⅰ与电池放置平面架3直接接触；
步骤903，将汇流杆5放于电极Ⅱ引出端200上，并位于绝缘胶带17范围内；
步骤904，将第一电源连接线18和第二电源连接线19分别接入电源，以便对柔性太阳能电池进行性能分析；
步骤905，通过连接杆2调节电池放置平面架3的角度。
可选地，当该支撑装置设置在图4所示的连接杆2上时，还可以通过连接杆2调节电池放置平面架3的角度。
当需要调节电池放置平面架3的角度时，只需松动下面2个连接部15上的锁紧件，然后转动电池放置平面架3至合适角度，然后再扭紧锁紧件即可。
本实施例通过角度调节结构的设置，在测试柔性太阳能电池的性能时，可以满足不同的角度需求，使测量结果更准确。
以上依据图式所示的实施例详细说明了本申请的构造、特征及作用效果，以上所述仅为本申请的较佳实施例，但本申请不以图面所示限定实施范围，凡是依照本申请的构想所作的改变，或修改为等同变化的等效实施例，仍未超出说明书与图示所涵盖的精神时，均应在本申请的保护范围内。

Claims (12)

  1. 一种用于柔性太阳能电池性能测试的支撑装置，其特征在于：包括电池放置平面架(3)、磁铁(4)和汇流杆(5)，所述电池放置平面架(3)和所述汇流杆(5)均为导体，所述磁铁(4)吸附在所述电池放置平面架(3)一侧的板面上，所述电池放置平面架(3)的另一侧的板面上设有绝缘带，所述汇流杆(5)在所述磁铁(4)的磁力吸附作用下固定在所述绝缘带上，用于将所述柔性太阳能电池的电极Ⅱ引出端压紧在所述绝缘带的范围内；所述汇流杆(5)上设有第一电源连接线(18)，所述电池放置平面架(3)上设有第二电源连接线(19)。
  2. 根据权利要求1所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：还包括架体(1)和连接杆(2)，所述连接杆(2)为2根，相对地安装在所述架体(1)上，所述电池放置平面架(3)可转动地安装在2根所述连接杆(2)之间。
  3. 根据权利要求2所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述架体(1)包括底杆(6)、主杆(7)和横梁(8)，所述底杆(6)和所述主杆(7)均为2根，所述主杆(7)沿竖直方向布置，所述底杆(6)沿水平方向布置，2根所述主杆(7)的底部分别固定连接1根所述底杆(6)；所述横梁(8)至少为2根，固定设置在2根所述主杆(7)之间。
  4. 根据权利要求3所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：2根所述主杆(7)相对的侧面上设有滑轨，所述连接杆(2)通过螺栓组件安装在所述滑轨上。
  5. 根据权利要求3所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述横梁(8)为3根，其中两根所述横梁(8)设置在所述主杆(7)的顶部和底部，剩余一根所述横梁(8)设置在所述主杆(7)的中部。
  6. 根据权利要求4所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述连接杆(2)采用绝缘材质制成，所述连接杆(2)包括安装段(9)和角度调节段(10)，二者为一体式J字形结构，所述安装段(9)上自上至下依 次设有平面架安装孔(11)、第一安装孔(12)和第二安装孔(13)，所述连接杆(2)通过所述第一安装孔(12)和所述第二安装孔(13)和所述螺栓组件安装在所述滑轨上；所述角度调节段(10)上设有弧形角度调节孔(14)，所述电池放置平面架(3)的上端与所述平面架安装孔(11)连接，下端与所述弧形角度调节孔(14)连接。
  7. 根据权利要求6所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述电池放置平面架(3)上设有4个连接部(15)，其中上面2个所述连接部(15)通过转轴与所述平面架安装孔(11)可转动连接，下面2个所述连接部(15)通过锁紧件与所述弧形角度调节孔(14)连接。
  8. 根据权利要求1至7任一所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述绝缘带是粘贴在所述电池放置平面架(3)的板面上的绝缘胶带(17)。
  9. 根据权利要求1或6或7所述的用于柔性太阳能电池性能测试的支撑装置，其特征在于：所述电池放置平面架(3)的下部设有凸台(16)，所述凸台(16)与所述汇流杆(5)位于所述电池放置平面架(3)同侧。
  10. 一种用于柔性太阳能电池的性能测试方法，其特征在于，应用于如权利要求1至9任一所述的支撑装置中，所述方法包括：
    将以能被磁铁(4)吸引的导电材料做衬底的所述柔性太阳能电池放于所述电池放置平面架(3)上，使得所述柔性太阳能电池的电极Ⅱ引出端(200)置于所述绝缘带上，位于所述柔性太阳能电池的太阳能电池主体(100)背面的电极Ⅰ与所述电池放置平面架(3)直接接触；
    将所述汇流杆(5)放于所述电极Ⅱ引出端(200)上，并位于所述绝缘带范围内；
    将所述第一电源连接线(18)和第二电源连接线(19)分别接入电源，以便对所述柔性太阳能电池进行性能分析。
  11. 根据权利要求10所述的用于柔性太阳能电池的性能测试方法，其特征在于，所述方法还包括：
    在所述电池放置平面架(3)的上部沿横向粘贴绝缘胶带(17)，形成所述绝缘带。
  12. 根据权利要求10所述的用于柔性太阳能电池的性能测试方法，其特征 在于，所述支撑装置上如权利要求2至9任一项所述的装置，所述方法还包括：
    通过所述连接杆(2)调节所述电池放置平面架(3)的角度。
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