METHOD OF MANUFACTURING SHINGLED SOLAR MODULE AND THE SHINGLED SOLAR MODULE

Abstract

The present disclosure relates to a method of manufacturing shingled solar module and the shingled solar module. The method includes steps of: arranging solar cells and conductive sheets on a top surface of a bottom package feature along a second direction in a shingled manner into a plurality of solar cell strings, wherein the conductive sheets are disposed at trailing ends of the solar cell strings, and the solar cell strings are arranged along a first direction perpendicular to the second direction to form a cell array; arranging a first busbar and a second busbar on a top or a bottom or the cell array, where the first busbar is in contact with main grid lines of the solar cells at initial ends of the respective solar cell strings, and the second busbar is in electrical contact with the conductive sheets of the respective solar cell strings; and laminating a combined feature comprised of the top package feature, the cell array, and the bottom package feature. In the method according to the present disclosure, the arranging step and the shingling step are combined as one step, in which the cells are shingled and arranged directly on the bottom package feature . In this way, the method is advantageous for operation and can be implemented efficiently at low costs.

Claims

1. A method of manufacturing a shingled solar module comprising a bottom package feature, a top package feature, and a cell array secured between the bottom package feature and the top package feature, characterized in that the method comprises steps of: arranging solar cells and conductive sheets on a top surface of the bottom package feature along a second direction in a shingled manner into a plurality of solar cell strings, wherein the conductive sheets are disposed at trailing ends of the solar cell strings, the respective solar cells are conductively connected to one another via contact of main grid lines, the conductive sheets are in contact with main grid lines of solar cells adjacent thereto, the respective solar cells and the conductive sheets are secured relative to each other via adhesives, and the solar cell strings are arranged along a first direction perpendicular to the second direction to form a cell array; arranging a first busbar and a second busbar on a top side or a bottom side of the cell array, wherein the first busbar is in contact with main grid lines of the solar cells at initial ends of the respective solar cell strings, the second busbar is in electrical contact with the conductive sheets of the respective solar cell strings, and each busbar is of a continuous strip structure and the busbars are configured to collect current from the cell array and export the current; and laminating a combined feature comprising the top package feature, the cell array, and the bottom package feature.

2. The method according to claim 1, characterized by further comprising: arranging a first conductive adhesive feature on a top surface of the solar cell at an initial end of each of the solar cell strings, the first conductive adhesive feature being in direct contact with a main grid line of the solar cell at the initial end; arranging a second conductive adhesive feature on a top surface of each of the conductive sheets, wherein respective conductive adhesive features of the adjacent solar cell strings are spaced apart in the first direction, and wherein the top package feature comprises a top panel, the first busbar and the second busbar are applied to a bottom surface of the top panel, and the first busbar and the second busbar are aligned with the respective conductive adhesive features in a direction perpendicular to the cell array such that the busbars can simultaneously come into contact with the respective conductive adhesive features of all the solar cell strings, the conductive adhesive features are applied through at least one of dispensing, painting, spraying and printing.

3. The method according to claim 2, characterized in that the top package feature further comprises a top flexible film disposed between the top panel and the cell array, and the method further comprises: arranging apertures corresponding to the conductive adhesive features on the top flexible film, conductive adhesive features electrically connect to the busbars via apertures.

4. The method according to claim 3, characterized in that the step of applying the first conductive adhesive feature and the second conductive adhesive feature is implemented after arranging the top flexible film on the cell array, and includes: applying a conductive adhesive material on the top flexible film, such that the conductive adhesive material flows through the apertures onto a top surface of the cell array and is solidified as the first conductive adhesive feature and the second conductive adhesive feature.

5. (canceled)

6. The method according to claim 1, characterized in that the first busbar and the second busbar are arranged on the cell array, wherein the first busbar is arranged on a top surface of the solar cell at the initial end of the respective solar cell strings and configured to connect, via a conductive adhesive feature or welding, main grid lines of the respective solar cells in contact therewith, and the second busbar is arranged on a top surface of the respective conductive sheets and configured to connect the respective conductive sheets via a conductive adhesive feature or welding.

7. The method according to claim 1, characterized by further comprising a step of applying an adhesive which includes applying the adhesive on each of the solar cells and the conductive sheets, where the adhesive is disposed between each pair of solar cell and conductive sheet adjacent to each other when the solar cells are arranged in the solar cell strings, further comprising a step of: detecting quality of the adhesive via a camera when applying the adhesive, and removing, based on detection results, solar cells where the adhesive is not applied correctly, the step of detecting is performed simultaneously with the step of applying the adhesive, and can provide close-loop feedback to the step of applying the adhesive; in a process of shingling the solar cells in solar cell strings, heat and/or pressure applied to overlapping portions between the solar cells to condense the adhesive.

8.-9. (canceled)

10. The method according to claim 7, characterized by further comprising either: (a) the steps of: (i) arranging a entire solar cell sheet, (ii) laser grooving the entire solar cell sheet and applying the adhesive, and (iii) splitting the whole solar cell sheet into a plurality of solar cells, or (b) the steps of: arranging a entire solar cell sheet, (ii) laser grooving the entire solar cell sheet, (iii) splitting the whole solar cell sheet into a plurality of solar cells, and (iv) applying the adhesive on each of the solar cells.

11.-12. (canceled)

13. The method according to claim 1, characterized in that the bottom package feature comprises a bottom panel and a bottom flexible film disposed between the bottom panel and the cell array, and the method further comprises a step of applying an adhesive on a top surface of the bottom flexible film prior to arranging the solar cells on the bottom package feature, characterized in that the step of applying the adhesive comprises: applying multiple groups of dot-like adhesives on the top surface of the bottom flexible film, where each group of the dot-like adhesives corresponds to one of the solar cell strings and includes one or more rows of dot-like features, and the dot-like adhesives are all arranged sequentially along the second direction and configured to engage bottom surfaces of the respective solar cells in the solar cell string.

14. (canceled)

15. The method according to claim 1, characterized by comprising a step of applying an adhesive after arranging the solar cells on the bottom package feature into the solar cell strings, which comprises: applying a strip adhesive on each of the solar cell strings along a second direction, to enable the strip adhesive to traverse the solar cell string.

16. The method according to claim 1, characterized in that the steps of arranging the solar cells into solar cell strings and arranging the solar cell strings into the cell array are implemented by electrostatic absorption or vacuum absorption; in a process of arranging the solar cells into the solar cell strings, quality of laminates are detected via a camera, and detection results are fed back to a monitoring platform in time; a manufacturing system further comprises a control device which is associated with the detection mechanism and configured to control a lamination mechanism based on the detection results of the detection mechanism, and prior to a lamination step, defect detection is performed on pieces to be laminated using EL or PL electroluminescence, and if detection indicates a piece to be laminated is unqualified, defect detection will be performed again after recovery of the piece.

17.-19. (canceled)

20. The method of claim 1, characterized by further comprising a step of arranging the top package feature and a step of arranging the bottom package feature, wherein the step of arranging the bottom package feature comprises: arranging a bottom panel, and applying EVA, POE or silica gel to form a flexible film arranged between the bottom panel and the cell array; and wherein the step of arranging the bottom package feature comprises: applying EVA, POE or silica gel to form a flexible film arranged between a top panel and the cell array, and arranging the top panel.

21. The method according to claim 1, characterized in that the adhesive is not conductive.

22. (canceled)

23. A shingled solar module, comprising a bottom package feature, a transparent top package feature, and a cell array disposed between the bottom package feature and the top package feature, the cell array comprising at least two solar cell strings arranged sequentially along a first direction, characterized in that, each of the solar cell strings comprises a plurality of solar cells and a conductive sheet disposed at trailing ends of the plurality of solar cells, the plurality of solar cells and the conductive sheet being arranged in shingled manner sequentially along a second direction perpendicular to the first direction and secured relative to each other via an adhesive, wherein the respective solar cells are conductively connected through contact of main grid lines, and the conductive sheet is in contact with the main grid lines of the solar cells adjacent thereto, wherein the shingled solar module is provided with a first busbar and a second busbar disposed together on a top or bottom side of the cell array, where the first busbar is configured to be in electrically contact with main grid lines of the solar cells at initial ends of the respective solar cell strings, the second busbar is configured to be in electric contact with the conductive sheets of the respective solar cell strings, and the each busbar is of a continuous structure and the busbars are configured to collect current from the cell array and export the current.

24. The shingled solar module according to claim 23, characterized in that a top surface of a solar cell at an initial end of each of the solar cell strings is provided thereon with a first conductive adhesive feature in direct contact with a main grid line of the same solar cell, a top surface of the conductive sheet is provided thereon with a second conductive feature, respective conductive adhesive features of the solar cell strings adjacent to each other are spaced apart in the first direction, the top package feature comprises a top panel, and the busbars are formed on a bottom surface of the top panel and aligned with the respective conductive adhesive features in a direction perpendicular to the cell array, enabling the busbars to come into contact with the corresponding conductive adhesive features of the solar cell strings at the same time.

25. The shingled solar module according to claim 24, characterized in that the top package feature further comprises a top flexible film disposed between the top panel and the cell array, and the top flexible film is provided thereon with apertures corresponding to the conductive adhesive features, conductive adhesive features electrically connect to the busbars via apertures.

26. The shingled solar module according to claim 24, characterized in that each section of the conductive adhesive feature is of a dot-like structure, or a strip structure extending along the first direction; the busbars are formed on the cell array, where the first busbar connects the main grid lines at the initial ends of the respective solar cell strings, and the second busbar connects the conductive sheets of the respective solar cell strings.

27.-29. (canceled)

30. The shingled solar module according to claim 23, characterized in that the adhesive is arranged between each of the solar cells and the bottom package feature such that all of the solar cells are secured relative to the bottom package feature; characterized in that the bottom package feature comprises a bottom panel and a bottom flexible film disposed between the bottom panel and the cell array, and the adhesive is applied onto a top surface of the bottom flexible film.

31. (canceled)

32. The shingled solar module according to claim 30, characterized in that the adhesive includes multiple groups of dot-like adhesives pre-arranged on the top surface of the bottom flexible film, each group of the dot-like adhesives corresponds to one of the solar cell strings, each group of the dot-like adhesives comprises one or more rows of dot-like adhesives, and the dot-like adhesives are all arranged sequentially along the second direction and configured to engage a bottom surface of each of the solar cells in the solar cell string.

33. The shingled solar module according to claim 23, characterized in that each of the solar cell strings is provided thereon with the adhesive of a strip structure extending along the second direction and traversing the solar cell string; and the adhesive is not conductive.

34. The shingled solar module according to claim 23, characterized in that the bottom package feature comprises a bottom panel and a flexible film disposed between the bottom panel and the cell array, the flexible film is of an EVA film structure, POE film structure or silica gel film structure, and the top package feature comprises a top panel and a flexible film disposed between the top panel and the cell array, the flexible film is of an EVA film structure, POE film structure or silica gel film structure.

35.-36. (canceled)

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0070] In order to better understand the above and other objectives, features and advantages of the present disclosure, preferred embodiments as shown in the accompanied drawings are provided. Throughout the drawings, the same or similar reference symbols refer to the same or similar elements. It would be appreciated by those skilled in the art that the drawings are provided to illustrate the preferred embodiments of the present disclosure, without suggesting any limitation to the scope of the present disclosure, and respective components therein are not drawn to scale.

[0071] FIG. 1 is a explosive view of a shingled solar module in a process according to a first embodiment of the present disclosure;

[0072] FIG. 2A is a sectional view that the shingled solar module in FIG. 1 cut along an A-A line, and FIG. 2B is a sectional view that the shingled solar module in FIG. 1 cut along a B-B line;

[0073] FIG. 3 is a explosive view of a shingled solar module in a process according to a second embodiment of the present disclosure;

[0074] FIG. 4 is a explosive view of a shingled solar module in a process according to a third embodiment of the present disclosure; and

[0075] FIG. 5 is a explosive view of a shingled solar module in a process according to a fourth embodiment of the present disclosure.

DETAILED DESCRIPTION OF EMBODIMENTS

[0076] Reference will now be made to the drawings to describe in detail the embodiments of the present disclosure. The description here is only about preferred embodiments of the present disclosure, and those skilled in the art would envision, on the basis of the preferred embodiments described herein, other manners that can implement the present disclosure, which also fall into the scope of the present disclosure.

[0077] The present disclosure provides a shingled solar module and manufacturing method thereof. FIGS. 1-5 illustrate some preferred embodiments of the present disclosure. Reference will now be made to the drawings to describe respective embodiments.

First Embodiment

[0078] FIGS. 1, 2A and 2B illustrate a shingled solar module 1 according to a first embodiment of the present disclosure. It would be appreciated that, since the shingled solar module 1 as shown in FIG. 1 is in the progress of manufacturing, the respective components are separated, which should form an integral package feature after the manufacturing is completed. As shown in FIG. 1, the shingled solar module 1 includes a bottom package feature 145, a transparent top package feature 123, and a cell array 11 that can be secured between the bottom package feature 145 and the top package feature 123.

[0079] Wherein, the cell array 11 may generally be read as an array of solar cells 112, the solar cells 112 are arranged to form solar cell strings in a shingled manner, and a plurality of the solar cell strings in turn are arranged to form a cell array 11. A top conductive feature includes a top panel 12 and a top flexible film 13 disposed between the top panel 12 and the cell array 11 while a bottom conductive feature includes a bottom panel 15 and a bottom flexible film 14 disposed between the bottom panel 15 and the cell array 11. The top panel 12 and the bottom panel 15, for example, may be rigid panels, such as tempered glass. The top panel 12 may also be a polymer back plate. The top flexible film 13 and the bottom flexible film 14 may have a flexible film structure formed of EVA, POE or silica gel, respectively.

[0080] Specifically, each solar cell string includes a plurality of solar cells 12 arranged in a shingled manner in a second direction D2, and a conductive sheet 113 disposed at trailing ends of the plurality of solar cells 112. The solar cell 112 is provided at the top surface with a front electrode 17 and at the bottom surface with a back electrode 18. The conductive sheet 113 is formed of a conductive material.

[0081] For example, if the respective solar cells 112 in the solar cell string are arranged in the manner as shown in FIGS. 2A and 2B (i.e., for every two adjacent solar cells 112, the back electrode 18 of the preceding solar cell 112 is in contact with the front electrode 17 of the following), the front electrode 17 of the solar cell 112 at the initial end of the solar cell string is exposed, and the back electrode 18 of the last solar cell 112 of the solar cell string is also exposed. In order to form a loop, busbars are required to be simultaneously in contact with the exposed front electrode 17 and back electrode 18 of the solar cell string. Providing the conductive sheet 113 at the trailing end of the solar cell string enables busbars 121 disposed on the top surface of the solar cell string to be in contact with the back electrode 18. Specifically, the conductive sheets 113 can be configured in a structure similar to that of the common solar cell 112 and arranged at the trailing end of the solar cell string in a shingled manner, such that the conductive sheet 113 can be in contact with the back electrode 18 of the last solar cell 112 of the solar cell string. If conductively contacting with the top surface of the conductive sheet 113, the busbars 121 are actually in conductive contact with the back electrode 18 of the last solar cell 112. In this embodiment, conductive connection between the conductive sheet 113 and the busbar 121 is achieved via a conductive adhesive feature 16.

[0082] Referring back to FIG. 1, a first conductive adhesive feature 16a is disposed on the top surface of the solar cell 112 at the initial end of the solar cell string and configured in direct contact with the front electrode 17 of the same solar cell 12, and a second conductive adhesive feature 16b is disposed on the top surface of the conductive sheet 113. A corresponding conductive adhesive feature of an adjacent solar cell string is spaced apart in a first direction D1. Each section of the first conductive adhesive feature 16a and the second conductive adhesive feature 16b may be of a dot-like structure, or a strip structure extending in the first direction D1. In the embodiment, respective solar cells 112 are conductively connected to one another via direct contact of main grid lines. However, in other embodiments not shown, the solar cells 112 can be in conductive contact via conductive glue.

[0083] The busbars are formed on the bottom surface of the top panel 12, and their positions are schematically shown with dotted lines on the top panel 12. The busbars include a first busbar 121a and a second busbar 121b, where the first busbar 121a is aligned with the first conductive adhesive feature 16a in a direction perpendicular to the cell array 11, and the second busbar 121b is aligned with the second conductive adhesive feature 16b in the direction perpendicular to the cell array 11, such that the busbar can be in contact with the conductive adhesive features corresponding to all the solar cell strings simultaneously.

[0084] In addition, the top flexible film 13 is provided thereon with apertures 131 corresponding to the first conductive adhesive feature 16a and the second conductive adhesive feature 16b, through which the conductive adhesive structure can pass to come into contact with the busbars.

[0085] In this embodiment, the respective solar cells 112 are secured relative to one another via an adhesive among the respective solar cells 112. For example, the adhesive may be applied to each solar cell 112 to adhere it to a further solar cell 112 when the two are shingled. Alternatively, each solar cell string may be provided with a transparent adhesive which may be of a strip structure extending along the second direction and traversing the solar cell string. Preferably, the adhesive may only acts for adhering, which is not conductive.

[0086] As can be seen from the above, since the adhesive can secure the respective solar cells 112 relative to one another and the top package feature 123, the bottom package feature 145 and the solar cells 112 can be secured as one piece after lamination, the shingled solar module 1 according to the embodiment may not be provided with a welding ribbon.

[0087] According to the present embodiment, there is further provided a method of manufacturing the shingled solar module 1 as shown in FIG. 1, which includes an arranging and shingling step, busbar arrangement step, and lamination step.

[0088] In the arranging and shingling step, on the top surface of the bottom flexible film 14, the solar cells 112 and the conductive sheets 113 are arranged as a plurality of solar cell strings in a shingled manner in the second direction D2. In the circumstance, the conductive sheets 113 are disposed at the trailing ends of the respective solar cell strings, the respective solar cells 112 are electrically connected via direct contact of main grid lines, the conductive sheets 113 are in direct contact with the main grid lines of the solar cells 112 adjacent thereto, the respective solar cell strings are arranged along the first direction D1 perpendicular to the second direction D2 to form a cell array 11, and the respective solar cells 112 and the conductive sheets 113 are secured relative to each other via an adhesive. The shingling process may be implemented by electrostatically absorbing or vacuum-absorbing the solar cells 112 onto the bottom flexible film 14.

[0089] As mentioned above, in this step, the arranging step and the shingling step are combined as one, where shingling is performed directly on the bottom package feature, the respective cells are secured relative to one another, and arrangement is implemented when shingling is being performed. Such step is advantageous for operation and can be implemented efficiently at low costs.

[0090] Wherein, the step of applying the adhesive may include: applying the adhesive on each solar cell 112 and the conductive sheet 113, to ensure that the adhesive is present between each pair of the adjacent solar cell 112 and the conductive sheet 113 when the solar cells 112 are arranged in a solar cell string. Furthermore, when the adhesive is being applied, quality of the adhesive is detected via a camera, and the solar cells 12 where the adhesive is not correctly applied are removed based on the detection results. More preferably, the detection step is performed when the adhesive is applied, and the detection step can provide close-loop feedback to the step of applying the adhesive.

[0091] The busbar arrangement step includes: arranging a first busbar 121a and a second busbar 121b on the top of the cell array 11, or arranging a first busbar 121a and a second busbar 121b at the bottom of the cell array 11, such that the first busbar 121 is in electrical contact with the main grid line of the solar cell 112 at the initial end of the respective solar cell string, and the second busbar 121b is in electrical contact with the conductive sheets 113 of the respective solar cell strings. Both of the busbars are of a continuous strip structure and configured to collect current from the cell array 11 and export the same.

[0092] Specifically, in the shingled solar module 1 as shown in FIG. 1, the busbars in the embodiment are disposed on the bottom surface of the top panel 12. The method according to the present application further includes a step of arranging conductive adhesive features. The step of arranging conductive adhesive features includes: arranging a first conductive adhesive feature 16a on the top surface of the solar cell 112 at the initial end of each solar cell string, to make the first conductive adhesive feature 16a in direct contact with the main grid lines (which is the front electrode 17 in this embodiment) of the solar cell 12 at the initial end; and arranging a second conductive adhesive feature 16b on the top surface of each conductive sheet 113, where the conductive adhesive features corresponding to the adjacent solar cell strings are spaced apart in the first direction D1.

[0093] In addition, the top package feature 123 includes a top panel 12 and a top flexible film 13; two busbars 121 are respectively disposed at two sides of the bottom surface of the top panel 12 and aligned with the respective conductive adhesive features in a direction perpendicular to the cell array 11, enabling simultaneous contact with the respective conductive adhesive features of all the solar cell strings.

[0094] Moreover, the method further includes: arranging apertures 131 corresponding to the conductive adhesive features on the top flexible film 13, through which the conductive adhesive features electrically connect to the busbars via apertures.

[0095] Preferably, the step of applying the first conductive adhesive feature 16a and the second conductive adhesive 16b is implemented after arranging the top flexible film 13 on the cell array 11 and includes: applying a conductive adhesive material at two sides of the top flexible film, such that the conductive adhesive material flows through the apertures 131 to the top surface of the cell array 11 and is condensed there as the first conductive adhesive feature 16a and the second conductive adhesive feature 16b. Furthermore, the conductive adhesive features may be applied from process of dispensing, painting, spraying or printing.

[0096] Typically, small pieces of the solar cell 112 are split from an entire sheet of solar cell, and the step of applying the adhesive may be arranged before or after splitting. For example, the entire sheet of solar cell may be laser grooved, applied with an adhesive, and then split into a plurality of solar cells 112. Alternatively, the entire sheet of the solar cell may be laser grooved and then split into a plurality of solar cells 112, and the adhesive is subsequently applied to each solar cell 112.

[0097] Preferably, the step of shingling solar cells 112 and the step of applying the adhesive may be implemented simultaneously. For example, when the solar cells 112 are shingled to form solar cell strings, heat and/or pressure applied to the overlapping portions between the solar cells 112. Alternatively, the adhesive here is cured through air drying, ultraviolet rays solidifying.

[0098] Also preferably, in the process of arranging the solar cells 112 into solar cell strings, the quality of the shingled cells is detected via a detection device such as a camera, and the detection results are fed back to a monitoring platform in real time. More preferably, the manufacturing system further includes a control device which is associated with a mechanism for detection and configured for close-loop controlling the mechanism for detection.

[0099] The last step of the manufacturing process is a lamination step. In the lamination step, the top package feature 123, the cell array 11 and the bottom package feature 145 are laminated together. Prior to the lamination step, defect detection is performed on pieces to be laminated using EL electroluminescence or PL electroluminescence. If the detection indicates a piece is unqualified, defect detection is performed again after recovery of the piece to be laminated.

[0100] Since the aforesaid steps achieve the effect that the shingled solar module 1 is packaged and secured, and the solar cells 112 are conductively connected and can export the current, a step of applying a welding ribbon is not necessary any longer.

Second Embodiment

[0101] FIG. 3 illustrates a shingled solar module 2 according to a second embodiment of the present disclosure, in which the parts identical or similar to those in the first embodiment will be omitted or described briefly.

[0102] The shingled solar module 2 includes a cell array 21, a top package feature 223 having a top panel 22 and a top flexible film 23, and a bottom package feature 245 having a bottom panel 25 and a bottom flexible film 24.

[0103] In this embodiment, busbars are both disposed on the cell array 21. Wherein, a first busbar 26a is disposed on the top surface of the solar cell at the initial end of all the solar cell strings and configured to connect, via a conductive adhesive feature or welding, all the front electrodes of the respective solar cells in contact therewith; and a second busbar 26b is disposed on the top surfaces of the respective conductive sheets and configured to connect the respective conductive sheets via a conductive adhesive feature or welding.

[0104] The top panel 22 may be formed of a non-conductive transparent or opaque material, and it is unnecessary to provide a conductive mechanism, like a busbar, on the top panel 22.

Third Embodiment

[0105] FIG. 4 illustrates a shingled solar module 3 according to a third embodiment of the present disclosure, in which the parts identical or similar to those in the first embodiment will be omitted or described briefly.

[0106] The shingled solar module 3 includes a top package feature 323, a bottom package feature, and a cell array 31. The top package feature 323 includes a top panel 32 and a top flexible film 33 while the bottom package feature includes a bottom panel 35 and a bottom flexible film 34. The top panel 32 at the lower surface is provided with a first busbar 321a and a second busbar 321b; the top flexible film 33 is provided thereon with apertures 331 through which a first conductive adhesive feature 36a and a second conductive adhesive feature 36b on the cell array 31 can pass to come into electrical contact with the respective busbars.

[0107] In the present embodiment, an adhesive 341 is applied onto the top surface of the bottom flexible film 34. When shingled on the upper surface of the bottom flexible film 34, the respective solar cells can be secured relative to the bottom flexible film 34 via the adhesive 341 and thus secured relative to one another.

[0108] Preferably, as shown in FIG. 4, the adhesive 341 includes multiple groups of dot-like adhesives 341 pre-arranged on the top surface of the bottom flexible film 34, where each group of dot-like adhesives 341 corresponds to a solar cell string, each group of dot-like adhesives 341 includes one or more rows, and such adhesives 341 are all arranged along a second direction and each configured to engage the bottom surface of every solar cell in the solar cell string.

[0109] Accordingly, the method of manufacturing the shingled solar module includes a step of applying the adhesives 341 onto the top surface of the bottom flexible film 34 prior to arranging the solar cells on the bottom package feature. The step of applying the adhesives 341 includes: applying multiple groups of dot-like adhesives 341 on the top surface of the bottom flexible film 34, where each group of dot-like adhesives 341 corresponds to a solar cell string and includes one or more rows of dot-like features, and the dot-like adhesives 341 are all arranged sequentially along the second direction and each configured to engage the bottom surface of the respective solar cell.

Fourth Embodiment

[0110] FIG. 5 illustrates a shingled solar module according to a fourth embodiment of the present disclosure, in which the parts identical or similar to those in the first embodiment will be omitted or described briefly.

[0111] The shingled solar module 4 includes a cell array 41, a top package feature 423 having a top panel 42 and a top flexible film 43, and a bottom package feature 445 having a bottom panel 45 and a bottom flexible film 44.

[0112] In the embodiment, a first busbar 46a and a second busbar 46b are both disposed on the cell array 41. Wherein, the first busbar 46a is disposed on the top surface of the solar cell at the initial end of all the solar cell strings and configured to connect, via a conductive adhesive feature or welding, all the front electrodes of the respective solar cells in contact therewith; and the second busbar 46b is disposed on the top surfaces of the respective conductive sheets and configured to connect the respective conductive sheets via a conductive adhesive feature or welding.

[0113] The top panel 42 may be formed of a non-conductive transparent or opaque material, and it is unnecessary to provide a conductive mechanism, like a busbar, on the top panel 42.

[0114] In the present embodiment, an adhesive 441 is applied onto the top surface of the bottom flexible film 44. When shingled on the upper surface of the bottom flexible film 44, the respective solar cells can be secured relative to the bottom flexible film 44 via the adhesive 441 and thus secured relative to one another.

[0115] Preferably, as shown in FIG. 4, the adhesive 441 includes multiple groups of dot-like adhesives 441 pre-arranged on the top surface of the bottom flexible film 44, where each group of dot-like adhesives 441 corresponds to a solar cell string, each group of dot-like adhesives 441 includes one or more rows, and the adhesives 441 are all arranged along a second direction and each configured to engage the bottom surface of the respective solar cell in the solar cell string.

[0116] The aforementioned embodiments are examples of the method and the structure according to the present disclosure. In the method according to the present disclosure, the arranging step and the shingling step are combined as one step, in which the cells are directly shingled and arranged on the bottom package feature. In this way, the method is advantageous for operation and can be implemented efficiently at low costs. Furthermore, in the shingled solar module according to the present disclosure, the busbars have a convergence effect, and the adhesive plays a securing role. It is unnecessary to additionally provide a welding ribbon or conductive glue therein. Such arrangement can prevent power loss of the cells and avoid a series of problems probably caused by the conductive glue.

[0117] The foregoing description on the various embodiments of the present disclosure has been presented to those skilled in the relevant fields for purposes of illustration, but are not intended to be exhaustive or limited to a single embodiment disclosed herein. As aforementioned, many substitutions and variations will be apparent to those skilled in the art. Therefore, although some alternative embodiments have been described above, those skilled in the art can envision or develop other embodiments more easily. The present disclosure is intended to cover all substitutions, modifications and variations of the present disclosure as described herein, as well as other embodiments falling into the spirits and scope of the present disclosure.

REFERENCE SIGN

[0118] shingled solar module 1, 2, 3, 4 [0119] cell array 11, 21, 31, 41 [0120] top package feature 123, 223, 323, 423 [0121] bottom package feature 145, 245, 345, 445 [0122] top panel 12, 22, 32, 42 [0123] top flexible film 13, 23, 33, 43 [0124] bottom panel 15, 25, 34, 45 [0125] bottom flexible film 14, 24, 34, 44 [0126] first busbar 121a, 26a, 321a, 46a [0127] second busbar 121b, 26b, 321b, 46b [0128] first conductive adhesive feature 16a, 36 [0129] second conductive adhesive feature 16b, 36b [0130] aperture 131, 331 [0131] adhesive 341, 441 [0132] solar cell 112 [0133] conductive sheet 113 [0134] front electrode 17 [0135] back electrode 18 [0136] first direction D1 [0137] second direction D2