This disclosure relates generally to photovoltaic (PV) modules and, more specifically, advanced interconnect systems and methods for producing strings of shingled PV cells for use in PV modules.
Some known photovoltaic (PV) strings are constructed by shingling cells using PV cell segments cut from full size PV cells. Constructing PV modules using strings of shingled cells reduces electrical and optical losses compared to the conventional solar modules in which full size cells are soldered using copper ribbons on silver busbars.
Shingling of cells with ECA requires very tight control over the dispensing parameters. Slight deviations can cause the segments to short, resulting in total loss of power for the shorted segment. Further, the properties of the particular ECA typically constrain the dimensions of the overlap between two PV cell segments. For example, the lateral shear on the cured ECA and the amount of ECA that comes out from between the contacts requires a certain minimum overlap between two cells connected by the ECA. Reducing overlap between cells improves module output and reduces Cell-to-Module (CTM) losses. In the example arrangement 10, the contacts 40 and 50 are about 1.0 millimeters (mm) wide. Gaps 70 on either side of the contacts 40 and 50 are needed because of the ECA 60. Gaps 70 are each about 0.25 mm wide, resulting in a total overlap 80 of about 1.5 mm. Thus, in the arrangement 10, a section of the segment 30 that is 1.5 mm wide and spans the entire width of the segment is covered by segment 20, receives no sunlight, and produces no electricity.
Moreover, installed PV modules are exposed to sun, wind, snow, rain, ice, and the like. PV modules need to be designed to withstand the resulting cycles of temperature changes, mechanical loading and unloading, foreign object impacts, and other stresses produced in the field. Specifically, PV modules need to absorb the applied stresses and maintain electrical conductivity between cells, or PV cell segments. It is unclear whether ECAs will be able to maintain suitable connection and conductivity, because aging of ECAs is not a well-studied field.
This Background section is intended to introduce the reader to various aspects of the art that may be related to various aspects of the present disclosure, which are described and/or claimed below. This discussion is believed to be helpful in providing the reader with background information to facilitate better understanding of the various aspects of the present disclosure. Accordingly, it should be understood that these statements are to be read in this light, and not as admissions of prior art.
According to one aspect of this disclosure, a photovoltaic (PV) module includes a front layer, a rear layer, and a string of series connected PV cell segments laminated between the front layer and the rear layer. Each PV cell segment has a front surface including a front electrode and a rear surface including a rear electrode. Adjacent PV cell segments are overlapped by an overlap amount with the front electrode of one of the adjacent PV cell segments disposed under and directly contacting the rear electrode of the other of the adjacent PV cell segments. At least one adhesive strip is attached to the bottom surfaces of a pair of adjacent PV cell segments.
Another aspect of this disclosure is a method of making a photovoltaic (PV) string of PV cell segments. Each PV cell segment has a front surface with a front electrode and a rear surface with a rear electrode. The method includes positioning a first PV cell segment and positioning a second PV cell segment overlapping a portion of the first PV cell segment. The second PV cell segment is positioned such that the front electrode of one of the first and second PV cell segments directly contacts with the rear electrode of the other of the first and second PV cell segments. A first adhesive strip is applied across the rear surfaces of the first and second PV cell segments.
Various refinements exist of the features noted in relation to the above-mentioned aspects. Further features may also be incorporated in the above-mentioned aspects as well. These refinements and additional features may exist individually or in any combination. For instance, various features discussed below in relation to any of the illustrated embodiments may be incorporated into any of the above-described aspects, alone or in any combination.
Corresponding reference characters indicate corresponding parts throughout the several views of the drawings.
Referring initially to
The laminate 102 includes a top surface 106 (also referred to as a sun receiving side) and a bottom surface 108 (shown in
As shown in
Each string of PV cells within laminate 102 includes multiple PV cells connected in series. In the example embodiment, each string of PV cells includes multiple PV cell segments connected in series. The strings of PV cells within laminate 102 are electrically connected to each other in series, parallel, or a combination of series and parallel connections to produce a desired output voltage and current. In embodiments with multiple PV cell strings, the PV cell strings are typically coupled to each other within a junction box. Alternatively, the PV cell strings may be coupled together within the laminate 102.
As shown in
In some less preferred embodiments, modules with shingled cells are manufactured without the use of adhesive strips 402. In laminated PV modules, however, the encapsulant (such as EVA, PVB, TPU, polyolefin, silicones, EPDM and ionomers) can expand and contract significantly more than the PV cells segments with changing temperatures. This may result in the PV cell segments separating over time, resulting in open circuits. Adhesive strips 406 help compensate for this differential expansion and help ensure that the cell segments don't slide away from each other.
Because there is no ECA between the segments 402 and 404, they can be positioned with a smaller overlap 408 than similar cells using ECA. The overlap 408 is typically less than about 1.5 mm. In various embodiments, the overlap 408 is less than about 1.0 mm, less than about 0.5 mm, or less than about 0.1 mm. In particular embodiments, the overlap 408 is about 0.9 mm, 0.2 mm, or 0.1 mm. The minimum overlap 408 is determined at least in part by the dimensions of the front and rear electrodes of the PV cell segments, the amount of friction between the adjacent front and rear electrodes 400 and 202, the strength of the adhesive strips 406, the manufacturing tolerances, and the like. If the overlap 408 is too small, contact between front and rear electrodes 404 and 202 may be compromised, resulting in an increase of resistance between the adjacent PV cell segments 208.
The effective resistance between PV cell segments 402 and 404 is simply the contact resistance between electrode busbar 202 and rear electrode 400.
As shown in
The assembly 700 is configured to allow inline testing of the string 705 of PV cell segments 208. Each segment position 704 includes an electrically conductive test contact 712 that is configured to contact the rear electrode 400 of the PV cell segment 208 positioned in that segment position 704. The uppermost segment position 714 includes an upper contact 716 configured to contact the upper electrode/bus bar of the PV cell segment 208 positioned in segment position 714. The test contacts 712 are connected to a switch 718. Switch 718 and upper contact 716 are connected to first and second contacts 717 and 719 (respectively) of a test terminal 720. Switch 718 allows for selective coupling of one or more PV cell segments 208 to test terminal 720 to permit one or more PV cell segments 208 to be tested in position on the assembly 700. Thus, when the switch is connected as shown in
An ammeter 722 is connected between upper contact 716 and test contact 719 to allow measurement of current through one or more PV cell segments 208 of the string 705. Electrical parameters of the string 705 and/or individual cell segments 208, such as open circuit voltage (Voc), short circuit current (Isc), maximum power current(Imp), maximum power voltage (Vmp), fill factor (FF), series resistance (Rs), shunt resistance (Rsh), power, efficiency, and the like, can be measured by attaching appropriate hardware to the test terminal 720. This allows defective and/or lower performing cell segments 208 to be easily detected and replaced. Reverse current at specified voltages may be applied to help determine which (if any) cell segments 208 are likely to cause failure in the field.
After the string passes inspection, at 904, the string is turned over to expose the rear sides of the PV cell segments. Adhesive strips are applied to the rear surface of the segments to hold them in place.
At 906, the assembled and bonded string of PV cell segments proceeds to PV module layup, in which the string is incorporated, along with front glass, encapsulant, rear sheet, additional strings of PV cell segments, into a PV module layup to be laminated into a PV laminate.
Several PV panels were constructed and tested using the techniques described herein.
An EL image of a first test panel 1000 is shown in
Several PV panels similar to panel 1000 were produced with strings of PV cell segments shingled with different amounts of overlap between PV cell segments. Specifically, additional panels were constructed with a 0.9 mm overlap, a 0.2 mm overlap, a 0.1 mm overlap, and a 0.05 mm overlap. All of these panels did not use ECA between electrodes of the segments and used two separate strips of adhesive for each pair of PV cell segments, similar to PV cell string 600 (shown in
Similarly constructed panels were subjected to mechanical load tests simulating wind and snow loads, followed by thermal cycling. During thermal cycling some of the PV cell segments moved out of place. This movement may have been possible due to the characteristics of the adhesive tape used to hold the shingled PV cell segments together and/or the configuration of placement of the adhesive strips. Despite the movement, the mechanical load test performance of the cells was very good.
When PV panels using strings constructed similar to string 600 (
In further tests, PV panels were constructed using strings of PV cell segments constructed similar to string 500 (shown in
The test panels described above were constructed with PV cell segments made from passive emitter rear contact (PERC) cells. Test panels were also constructed using heterojunction technology (HJT) cells. An EL image of an HJT based test panel 1500 is shown in
The techniques described herein may be used to produce flexible PV panels. The electrical connection between front and rear electrodes of shingled PV cell segments in strings of PV cell segments without ECA are more mechanically compliant than the connections in some known systems. Once ECA has been cured, it is fairly rigid and inflexible. As a panel of shingled PV cell segments constructed with ECA bends, such as when a heavy load is applied to the middle of the panel, electrical contact between adjacent PV cell segments is often partially or completely compromised. In panels built according to this disclosure without ECA, the adjacent PV cell segments have a greater range of motion relative to each other before the electrical connection is compromised.
In
The PV modules described herein leverages the electrodes (i.e., busbars) on PV cell segments to directly make contact with each other. There is no ECA or solder between the electrodes of adjacent cell segments holding them together. For the purpose of layup, several cells are laid up with the desired overlap and held together using an insulating adhesive tape. To maintain electrical contact between adjacent cells of a shingled array, sufficient compressive forces are applied by means of lamination between polymer layers. To avoid lateral shear and separation of cells, a combination of frictional forces between cells and adhesive strength of insulating tape are used.
PV modules with directly contacting electrodes (i.e., without ECA) between shingled cells provide numerous advantages over PV modules that include ECA between electrodes of shingled cells.
The absence of ECA reduces the material costs of producing a module. Depending the on module output and cost structure of different materials, the overall cost advantage could be $0.01-$0.1 per watt. Typically, ECA contains highly conductive silver (Ag) particles. Depending on cell design and process conditions, 1-30 mg of ECA is required between cells. The costs can be prohibitively high. Additionally, ECA is typically stored frozen and requires personnel and equipment to freeze, thaw, and recycle the ECA, which adds to the cost of module production. Because ECA is not used to bond the electrodes of adjacent PV cell segments (which need a certain width for proper adhesion to ECA), the width of the electrodes on the segments of the modules described herein may be reduced, which reduces the amount of material (typically silver) needed to produce the electrodes. The techniques described herein can reduce the amount of silver used for cell electrodes to zero, resulting in significant cost savings while enhancing cell performance.
In the absence of foreign materials (e.g., ECA) between shingled cells, the materials making intimate contact (i.e. the front and rear electrodes) are the same type of material. As a result, mismatch in the coefficients of thermal expansion (CTE) of different materials is non-existent. CTE mismatch is a problem that is known to facilitate and worsen cracks in solar cells over time.
PV modules made according to this disclosure have lower effective resistance than known modules. As described above, in shingled solar array designs with ECA, the effective resistance between two cells is the sum of contact resistance values due to two interfaces with the ECA, as well as the bulk resistance of the ECA. Modules produced according to this disclosure do not include ECA between electrodes. The effective resistance between two cell segments without ECA is simply the contact resistance between the two electrodes. The contacting surfaces are generally made of the same metal (typically silver) which often reduces the series resistance of the solar module.
Modules of embodiments of this disclosure have a lower likelihood of shunting cells than modules that use ECA between cell segments. Conductive adhesives, if not dispensed carefully, can create shunts that can result in significant loss of array power. In the absence of such materials, the risk of shunting cells is almost completely eliminated.
Modules without ECA between the electrodes of shingled PV cell segments can have a smaller overlap, thereby reducing shading and improving the overall efficiency of the module. In known modules with ECA, the minimum permissible overlap between two shingled cells depends on the viscosity of the bonding material. The spread coverage of the adhesive dictates the minimum value of cell overlap. By eliminating ECA, the constraint on cell overlap is significantly reduced. Further, by reducing overlap, it is possible to ensure that the active area in a solar module remains the same while reducing the number of cells used. This results in significant reduction of CTM losses while also saving on the cost of solar cells. For example, if eighty-two PV cells are shingled with a 1.5 mm overlap in a PV module, the module will produce more than twelve watts less power than the same 82 cells in a non-overlapped module. If the overlap is reduced to 0.9 mm, a module with 80 cells produces 0.08 W less power than the 82 cell non-overlapped module. If the overlap is further reduced to 0.2 mm, a module with 78 overlapped cells produces 9.48 W more than the 82 cell non-overlapped module.
Modules with PV cell segments in direct contact without ECA are subjected to less stress during manufacture and may be more reliable. Manufacturing strings with ECA requires a heat source to cure the ECA. The source is typically a thermal mass maintained between 100° C. and 200° C. Curing the ECA with this thermal mass places extra thermal cycle stresses on the PV cells, which can lead to premature failure of the PV module with ECA. Moreover, the equipment used for curing the ECA and the electricity needed to operate the equipment adds to the cost of producing a PV module with ECA between cells.
Modules produced with the techniques described herein are more flexible and tolerant than known modules produced with ECA. This allows the modules to have thinner frames, allows thinner laminates to be constructed, allows strings to run along the length of them module, and allows for the production of flexible PV panels.
The techniques described herein also permit in-line inspection/metrology of solar cell strings that is not available in strings made with ECA between PV cell segments. Strings made using foreign material to make electrical contact between cell segments cannot be tested until the foreign material is fully cured and bonded to cells. At that time, if there is a bad connection or a bad cell segment, significant effort is needed to remove the bonded, defective cell segment. The strings produced as described herein permit in-line testing/metrology throughout the assembly process. It is possible to accept/reject individual PV cell segments as the strings are constructed, without requiring any significant rework. This can drastically improve the yield and quality of production facilities.
When introducing elements of the present invention or the embodiment(s) thereof, the articles “a”, “an”, “the” and “said” are intended to mean that there are one or more of the elements. The terms “comprising”, “including” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements.
Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about,” “approximately,” and “substantially,” is not to be limited to the precise value specified. In at least some instances, the approximating language may correspond to the precision of an instrument for measuring the value. Here and throughout the specification and claims, range limitations may be combined and/or interchanged; such ranges are identified and include all the sub-ranges contained therein unless context or language indicates otherwise.
As various changes could be made in the above without departing from the scope of the invention, it is intended that all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
This application claims priority to U.S. provisional patent application Ser. No. 62/272,950, filed 30 Dec. 2015, which is hereby incorporated by reference in its entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/US2016/068720 | 12/27/2016 | WO | 00 |
Number | Date | Country | |
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62272950 | Dec 2015 | US |