JP4682237B2 - Manufacturing method of solar cell module - Google Patents

Description

  The present invention relates to a method for manufacturing a solar cell module. In particular, the present invention relates to a method for manufacturing a solar cell module in which solar cells are sealed with resin between a light-receiving surface side transparent plate and a back plate.

  In recent years, awareness of environmental protection has increased, and solar power generation has become even more important. The solar battery cell is sandwiched between protective materials, sealed with a transparent resin, and used outdoors as a solar battery module. As a transparent resin for sealing, an ethylene-vinyl acetate copolymer (hereinafter abbreviated as EVA) resin or the like is used, which is sandwiched between a protective material and a solar battery cell. It is sealed by solidifying after heating and melting. In order to arrange and wire solar cells efficiently, it is preferable to seal a plurality of solar cells in one solar cell module.

  In addition, the installation location of solar cells has been diversified recently, and it has been used not only on the roof of buildings but also on the wall. When using it for a wall, not only it attaches to an outer wall, but the wall itself is also comprised with a solar cell module. In this case, since it has a great influence on the appearance of the building, it is important to make the solar cell modules regularly arranged without defects. At the same time, there is a demand for a large-area solar cell module having sufficient strength as a building structure.

  In the utility model registration No. 2500794 (patent document 1), in a laminate formed by joining two plate-like bodies via an adhesive sheet so as to sandwich a solar cell between the two adhesive sheets, A laminated body is described in which a sheet piece having a thickness substantially equal to that of the solar cell is sandwiched between gaps formed between the adhesive sheets outside the solar cell. By adopting such a configuration, the thickness of the peripheral portion of the laminated body can be made uniform, and moisture can hardly enter the gap from the outside, so that peeling can be prevented. It is described that EVA is used as an adhesive sheet and plate glass is used on both sides as a plate-like body.

  Japanese Patent Laid-Open No. 2003-110127 (Patent Document 2) discloses a solar cell module in which a plurality of solar cells are arranged between a front cover and a back cover and sealed with a transparent filler such as EVA. A solar cell module in which translucent spacers (setting blocks) are arranged between cells is described. As this spacer, it is described that it is optimal to use the same material as the transparent filler and the same thickness as the solar battery cell. It is said that this spacer can secure an air flow path without being deformed only by its own weight. Thus, it is described that a solar cell module having no air remaining therein can be manufactured.

  Japanese Unexamined Patent Publication No. 59-022978 (Patent Document 3) describes a filled adhesive sheet for a solar cell module containing an ethylene copolymer and an organic peroxide and having an embossed pattern on both sides thereof. Has been. The adhesive sheet has an embossed pattern, so that blocking of the sheet can be prevented, it is excellent in deaeration in the process of modularization, and it is said that bubbles are not easily generated. The embodiment of the publication describes a bonding method in which the temperature is raised to 150 ° C. while reducing the pressure in a vacuum laminator, the pressure is continuously reduced at 150 ° C. for 1 hour, and then the pressure reduction is stopped.

  In Japanese Patent Application Laid-Open No. 09-036405 (Patent Document 4), a photovoltaic element is formed between a front surface member and a back surface member through a sealing material resin, and the stacked body is a vacuum of 5 Torr or less. A solar cell module is described that is held for 5 to 40 minutes at a predetermined temperature, and then thermocompression-bonded at a vacuum degree of 5 Torr or less, and is cooled and bonded after the thermocompression bonding. It is said that a module that is less likely to cause peeling of the surface member and less likely to remain bubbles is provided by thermocompression bonding under such conditions. It is also described that the problem of remaining bubbles can be improved by inserting a non-woven fabric between the solar battery cell and the encapsulant resin and letting the air in the laminate escape through the voids in the non-woven fabric.

  In Japanese Patent Application Laid-Open No. 61-069179 (Patent Document 5), a solar panel laminated body in which solar cells are laminated between a cover glass and a back material through a filler is degassed by a double vacuum method. In addition, in the method for manufacturing a solar cell panel having a bonding step by pressurization after heating, there is a method for manufacturing a solar cell panel that uses EVA as a filler and holds the double vacuum chamber in a specific temperature range for a specific time. Are listed. By pasting together under specific temperature conditions, EVA can be completely crosslinked without foaming and yellowing. Under the conditions described in the examples, heating was started after the pressure was reduced to 0.3 Torr (about 0.0004 MPa), and when the temperature of the substrate surface on the heater side reached 140 ° C., vacuum pressing was performed and crosslinking was performed at 148 ° C. After the reaction, the vacuum pressure bonding is released after cooling to 50 ° C. or lower.

  However, when many cells are connected and sandwiched between two plates and sealed by thermocompression bonding, it is difficult to avoid damage to the solar cells. In particular, when the number of cells is large and the area of the entire module is large, a large load is likely to be applied unevenly, and it is inevitable that some cells that receive an excessive load are damaged. In a module, a number of cells are connected in series with each other, so that if a single cell breaks, a series of connected cells will not function. If the cell breaks, it not only impairs the appearance but also greatly reduces the power generation performance, so it must be discarded as a defective product. Therefore, there is a demand for a sealing method in which cell damage is less likely to occur.

Utility Model Registration No. 2500974 Japanese Patent Laid-Open No. 2003-110127 JP 59-022978 JP 09-034055 A Japanese Patent Laid-Open No. 61-069179

  The present invention has been made to solve such a problem, and provides a method for manufacturing a solar cell module capable of preventing the solar cell from being damaged when the solar cell is sealed with a resin. It is intended to do.

The present invention relates to a method for manufacturing a solar cell module in which a plurality of solar cells are sealed with a resin between a light-receiving surface side transparent plate and a back plate, and a plurality of solar cells are arranged at intervals. A first sealing resin sheet that is connected to each other with a conductive wire and covers substantially the entire surface of the light-receiving surface-side transparent plate is disposed between the light-receiving surface-side transparent plate made of a glass plate and the solar battery cell, and is made of a glass plate A second sealing resin sheet that covers substantially the entire surface of the back plate is disposed between the back plate and the solar cell, and the first sealing resin sheet or the second sealing resin sheet is a plurality of sealing resin sheets. The first sealing resin sheet or the second sealing resin sheet is configured by stacking and arranging a part of the electrical wiring in parallel to the solar battery cell in a position overlapping vertically without contacting the solar battery cell. one sealing of the plurality of sealing resin sheet on the inner By placing the resin sheet as missing wider than the width of the electrical wiring portion of the electric wiring, the local loads in the portion of the electrical wiring in the sealing operation while allowing never applied to the solar cell, A method for producing a solar cell module, comprising: discharging air between a light-receiving surface side transparent plate and a back plate; heating and melting a resin; and then cooling and sealing.

  There are various methods for arranging solar cells sealed in the solar cell module depending on purposes and applications. Usually, a plurality of adjacent solar cells are arranged at a predetermined interval and connected to each other by a conducting wire. In addition to this, when connecting non-adjacent cells or conductors at distant positions, or making holes in the back plate and pulling out the electrical wiring, some of the electrical wiring is solar cells. May be arranged at a position that overlaps in the vertical direction without contacting. In such a case, since the electric wiring overlaps on the cell, when a load is applied from above and below, an excessive load is applied to the overlapped portion, and cell cracking easily occurs. On the other hand, cell cracking can be prevented by arranging one sealing resin sheet so as to be missing at the portion of the electrical wiring in the first sealing resin sheet or the second sealing resin sheet.

In the present invention , it is preferable that a portion of the electrical wiring portion where the sealing resin sheet is missing is filled with a sealing resin sheet that is thinner than the missing sealing resin sheet. Moreover, it is also preferable that an insulating film is disposed between the electric wiring and the solar battery cell, and the insulating film is laminated with the solar battery cell and the electric wiring via a sealing resin sheet.

In the present invention , when sealing in the sealing treatment container, the step of heating the sealing resin while maintaining the pressure in the sealing treatment container at 0.05 MPa or more (step 1), a temperature lower than the melting point of the sealing resin In step (step 2) of depressurizing the inside of the sealing treatment container to a pressure of 0.01 MPa or less, step of raising the temperature to a temperature equal to or higher than the melting point of the sealing resin (step 3), It is preferable to perform a sealing operation comprising the steps of increasing the pressure (step 4) and cooling (step 6).

In the present invention, it is preferable that the sealing resin is made of a kind of resin selected from the group consisting of an ethylene-vinyl acetate copolymer, polyvinyl butyral, and polyurethane.

  According to the method for manufacturing a solar cell module of the present invention, when solar cells are arranged and sealed with a transparent resin, the solar cells can be prevented from being damaged.

  Hereinafter, the present invention will be described in detail with reference to the drawings. FIG. 1 is a schematic cross-sectional view of an example of a solar cell module after a sealing operation. 2 and 3 are schematic cross-sectional views of an example of the laminated body before the sealing operation.

  The cross-sectional schematic diagram of an example of the solar cell module 1 obtained by the manufacturing method of the present invention is shown in FIG. In the solar cell module 1, solar cells 4 are sealed with a resin 5 between a light-receiving surface side transparent plate 2 and a back plate 3. Although the number of solar cells 4 sealed in the solar cell module 1 may be one, it is preferable that a plurality of solar cells 4 are sealed. Usually, the light receiving surface 6 and the back surface 7 of the adjacent solar battery cell 4 are connected via the conducting wire 8.

  As the solar battery cell 4 used in the present invention, various solar battery cells such as a single crystal silicon solar battery, a polycrystalline silicon solar battery, an amorphous silicon solar battery, and a compound semiconductor solar battery can be used. These solar cells 4 are generally thin plates having a thickness of 1 mm or less, more generally 0.5 mm or less, and are often quadrangular with sides of 5 cm or more. The substrate can be made of a semiconductor substrate such as silicon or germanium, a glass substrate, a metal substrate, etc. In the case of a silicon substrate, a thin plate is desired due to cost requirements, but it is a hard and brittle material. Therefore, it is particularly easily broken at the time of sealing, and the significance of adopting the production method of the present invention is great.

  The number of solar cells 4 enclosed in one solar cell module 1 is not particularly limited, and may be only one. In that case, only the wiring from the solar battery cell 4 to the outside is connected. However, as the number of solar cells 4 enclosed in one solar cell module 1 increases, the defective product rate resulting from the damage of the solar cells 4 increases. Therefore, there is an actual advantage of adopting the manufacturing method of the present invention. large. Therefore, it is preferable that 10 or more, preferably 30 or more, and more preferably 100 or more solar cells 4 are arranged in one solar cell module 1.

  The width of the gap 9 between the adjacent solar cells 4 is not particularly limited, but is usually 0.5 mm or more, and in the case of less than this, the cells when the adjacent solar cells 4 come into contact with each other to be sealed May be damaged. If priority is given to daylighting, the gap 9 is preferably widened, and if priority is given to light utilization efficiency, the gap 9 is preferably narrowed. It is adjusted appropriately according to the usage and design requirements.

  When encapsulating a plurality of solar cells 4, it is preferable that the plurality of solar cells 4 are arranged via a predetermined width and are connected to each other by a conductor 8. At this time, the adjacent solar battery cells 4 are connected to each other by the conductive wire 8 between the light receiving surface 6 and the back surface 7, and a large number of solar battery cells 4 are connected in series. Connection between the light receiving surface 6 or the back surface 7 and the conductive wire 8 is performed using a conductive adhesive such as solder. Further, in order to efficiently collect the generated current, it is also preferable to form a current collection pattern with a conductive paste or the like on the light receiving surface 6 so as to be electrically connected to the conductor 8. Furthermore, there may be a case where non-adjacent cells or conductors 8 located apart from each other are connected, or a hole is formed in the back plate 3 to pull out the conductor 8 to the outside.

  The conductive wire 8 is also called an interconnector, but the material is not particularly limited, and a copper wire or the like is used. Since the light-receiving surface side transparent plate 2 and the back plate 3 are sandwiched and disposed, it is preferable to use a thin ribbon-shaped conductor 8, and the thickness is usually 0.5 mm or less, preferably 0.3 mm. It is as follows. Moreover, it is 0.05 mm or more normally. It is preferable that a conductive adhesive such as solder is applied to the conductive wire 8 in advance because the connection work becomes easy. In the state where the conductive wire 8 is connected, the height from the surface of the solar battery cell 4 to the highest portion of the conductive wire 8 varies depending on the location, but depending on the connection operation, the height is 0.5 mm than the thickness of the conductive wire 8. There are places where it gets thicker.

  The material of the light-receiving surface side transparent plate 2 should just be transparent with respect to sunlight, and polycarbonate resin, an acrylic resin, etc. can also be used besides glass. However, considering durability, hardness, flame retardancy, etc., it is preferable to use glass. Since a structural material having a large area is often formed, a glass plate having a surface compressive stress of 20 MPa or more is preferable from the viewpoint of strength. In addition, when the area is large, thermal cracking due to temperature rise due to sunshine or the like is likely to occur. From this point, it is preferable to use a glass plate having a surface compressive stress of 20 MPa or more. However, since a glass plate having a large surface compressive stress is usually produced by heating and quenching a float plate glass, occurrence of a certain strain is inevitable. Therefore, due to the warp of the glass generated, excessive load is easily applied to some of the solar cells 4 at the time of sealing, and the practical advantage of employing the manufacturing method of the present invention that can prevent cell cracking is great.

  Here, the surface compressive stress of the plate glass is a value measured according to JIS R3222. Specific examples of the glass plate having a surface compressive stress of 20 MPa or more include double strength glass, tempered glass, and super tempered glass. Double-strength glass usually has a surface compressive stress of 20 to 60 MPa, tempered glass usually has a surface compressive stress of 90 to 130 MPa, and super-tempered glass usually has a surface compressive stress of 180 to 250 MPa. As the surface compressive stress is increased, the strength is improved, but warpage tends to increase and the manufacturing cost tends to increase. The double-strength glass is preferable in that it is easy to produce a glass with relatively little warpage and does not fall into a small piece when dropped. The glass plate is selected according to the use and purpose.

  The back plate 3 does not necessarily have to be transparent, but if the lighting is taken into consideration, the back plate 3 should also be transparent to sunlight. Moreover, it is preferable to use glass, especially a glass plate whose surface compressive stress is 20 MPa or more for the same reason as the light-receiving surface side transparent plate 2.

The material of the glass is not particularly limited, and soda lime glass is preferably used. In particular, the light-receiving surface side transparent plate 2 is preferably a highly transmissive glass (so-called white plate glass). High transmission glass is soda lime glass with a low iron content, and has high light transmittance. Further, as the glass of the back plate 3, in addition to using the high transmission glass and soda lime glass (so-called blue plate glass) having a relatively high iron content, use heat ray reflection glass, heat ray absorption glass, or the like. Is also preferred depending on the application. Moreover, the template glass etc. which formed the embossed pattern on the surface can also be used. Although the thickness of a glass plate is not specifically limited, If it uses as a structural material, it is preferable that it is 3 mm or more, and it is more preferable that it is 5 mm or more. Thus, when using a thick glass plate, the influence of its own weight is large, and there is a possibility that the cell may be damaged when the glass plate is stacked on the cell before bonding, and there is an advantage of adopting the manufacturing method of the present invention. large. The thickness of the glass plate is usually 20 mm or less. Moreover, although the area of glass is adjusted with a use, when it is 1 m < ² > or more, the actual profit which employ | adopts the manufacturing method of this invention is large.

  The material of the resin 5 is not particularly limited as long as it is transparent and has adhesiveness and flexibility, and is selected from the group consisting of ethylene-vinyl acetate copolymer (EVA), polyvinyl butyral, and polyurethane. One kind of resin is preferably used. At this time, a crosslinked resin is preferable from the viewpoint of strength and durability. Therefore, the raw material of the resin 5 is preferably a crosslinkable thermoplastic resin, particularly a resin that undergoes a crosslinking reaction when heated. Such a resin is sandwiched between the light-receiving surface side transparent plate 2 and the back plate 3 in the form of a sheet, heated and melted, then subjected to a crosslinking reaction as necessary, and then cooled and solidified to form a solar battery cell 4. Is sealed. By using a material that is crosslinked by heating, it is possible to achieve excellent durability and adhesiveness. The crosslinkable thermoplastic resin is not particularly limited as long as it undergoes a crosslinking reaction when heated, but is a kind selected from the group consisting of ethylene-vinyl acetate copolymer (EVA), polyvinyl butyral, and polyurethane. Resins are preferably used. For example, EVA can be crosslinked by blending and heating a crosslinking agent, and polyurethane can be crosslinked by reacting an isocyanate group and a hydroxyl group.

  In the case of polyurethane, since the crosslinking reaction proceeds at a relatively low temperature, it is suitable when a resin plate having low heat resistance is used for at least one of the light receiving surface side transparent plate and the back plate. In addition, since polyurethane is also excellent in flexibility, it is suitable for use when it is used for the light-receiving surface side transparent plate and the back plate in combination with materials with greatly different coefficients of thermal expansion such as glass and plastic. It is. Furthermore, polyurethane has excellent penetration strength.

  Among the crosslinkable thermoplastic resins, it is preferable to use a thermoplastic resin containing a crosslinking agent. The thermoplastic resin at this time is not particularly limited as long as the crosslinking reaction proceeds when heated together with the crosslinking agent, but an ethylene-vinyl acetate copolymer (EVA) excellent in transparency, flexibility, durability and the like. Is most preferably used.

  The sealing resin sheet is sandwiched between the light-receiving surface side transparent plate 2 and the back plate 3, melted by heating, and then cooled and solidified to seal the solar cells 4. It is preferable that the sealing resin sheet contains a crosslinking agent in EVA resin. In this case, the resin is heated and melted and then a crosslinking reaction is allowed to proceed, followed by cooling to seal with the crosslinked EVA. Can do. The EVA in the sealing resin sheet preferably has a melting point of 50 to 80 ° C. measured by the DSC method from the viewpoint of the balance between transparency and form retention.

  It is preferable that the sealing resin sheet has an appropriate embossed surface on one or both sides because blocking can be prevented and remaining bubbles are easily suppressed. A suitable embossing depth is 10 to 100 μm, and if it is too deep, there is a possibility that bubbles remain. The sheet thickness is preferably 0.2 to 2 mm, and more preferably 0.3 to 1 mm, and one or a plurality of the sheets can be stacked to adjust the thickness.

  Hereinafter, the sealing operation method according to the production method of the present invention will be described. In the description here, the operation of stacking the light-receiving surface side transparent plate 2 from below is performed, but the back plate 3 may be stacked in reverse order from the bottom first.

  First, the configuration of the first invention will be described with reference to the drawings. A feature of the first invention is that a plurality of solar cells 4 are arranged at a narrow interval of 5 mm or less, and the total thickness of the solar cells 4 is larger than the thickness of the solar cells 4 in the blank portion 10 outside the solar cells 4. It is sealing after arrange | positioning the thick sealing resin sheet piece 40,41,42,43. FIG. 2 is a schematic cross-sectional view of an example of the laminated body 60 before the sealing operation, and shows a cross section cut in parallel to the direction in which the plurality of solar battery cells 4 are connected in series.

  First, the 1st sealing resin sheet 20 is accumulated on the light-receiving surface side transparent plate 2 so that the whole surface may be covered substantially. At this time, the light-receiving surface side transparent plate 2 is preferably a glass plate, particularly a glass plate having a warped surface compressive stress of 20 MPa or more. And in the light-receiving surface side transparent plate 2, it is preferable to overlap the 1st sealing resin sheet 20 on it so that the inner side of curvature, ie, a concave surface side may become upper. At this time, the warp of the light-receiving surface side transparent plate 2 (value measured in accordance with JIS R3206) is preferably 0.05 to 0.5%. If the warpage is too large, there is a possibility that a force for peeling off inside the module after sealing may remain, more preferably 0.4% or less, and further preferably 0.3% or less. On the other hand, when the warpage is too small, there is a possibility that a cell crack may occur due to the load of the back plate 3 being applied to the solar cell 4 near the center of the module during the sealing operation, and more preferably 0.1%. % Or more, and more preferably 0.15% or more.

  The thickness of the first sealing resin sheet 20 is preferably 0.5 mm or more, and more preferably 1 mm or more. Also, it is usually 5 mm or less, preferably 3 mm or less. By setting the thickness to a certain value or more, the impact can be efficiently absorbed and the solar battery cell 4 can be effectively protected. The first sealing resin sheet 20 is preferably configured by laminating a plurality of sealing resin sheets. This is because it becomes easy to adjust the thickness of the first sealing resin sheet 20 according to the application and required performance. In the example of FIG. 2, the first sealing resin sheet 20 is configured by stacking three sealing resin sheets 21, 22, and 23. The first sealing resin sheet 20 only needs to cover substantially the entire surface of the light-receiving surface-side transparent plate 2, and a part of the first sealing resin sheet 20 may be missing due to the arrangement of the conductive wires. You may be comprised from the several sealing resin sheet arrange | positioned.

  On the 1st sealing resin sheet 20, the photovoltaic cell 4 is mounted. At this time, it is preferable to place a plurality of solar cells 4 connected to each other in the manner described above, and arrange them vertically and horizontally as necessary. In this case, the solar cells 4 that are connected in advance may be placed, may be connected on the first sealing resin sheet 20, or after the part that has been partially connected is placed, You may connect.

  In 1st invention, the width | variety of the clearance gap 9 between the adjacent photovoltaic cells 4 is 5 mm or less, Preferably it is 4 mm or less, More preferably, it is 3 mm or less. Further, the width of the gap 9 is usually 0.5 mm or more, and preferably 1 mm or more. Thus, the utilization efficiency of light can be improved by arranging the photovoltaic cells 4 at a narrow interval. However, when the gap 9 is narrow, it is difficult to dispose the sealing resin sheet piece in the gap between the adjacent solar cells 4 in order to prevent cell cracking. It is necessary to arrange the sealing resin sheet pieces 40, 41, 42, and 43 whose total thickness is larger than the thickness of the solar battery cell 4 in the portion 10.

  When the internal resin is depressurized by disposing the sealing resin sheet pieces 40, 41, 42, 43 having a total thickness larger than the thickness of the solar battery cell 4 in the margin 10 on the outer side of the solar battery cell 4, A load due to atmospheric pressure from both the front and back surfaces is not directly applied to the solar battery cell 4, and the sealing resin sheet pieces 40, 41, 42, and 43 receive the load. Therefore, the load of the back plate 3 can be prevented from being directly applied to the solar cells 4 arranged in the module. And as the temperature rises, the resin softens and the thickness of the encapsulating resin sheet pieces 40, 41, 42, 43 applied with a load decreases, the cell or the portion of the conductive wire 8 connected to the cell, The upper and lower sealing resin sheets come into contact with each other. At that time, the entire resin sheet is softened so that no local load is applied, and the cell or the conductive wire 8 connected to the cell is softened. It can be closely attached so as to be embedded in the resin sheet. Thereby, cell cracking in the decompression step can be prevented. In particular, as the number of solar cells 4 enclosed in one solar cell module 1 increases, the defective product rate resulting from the damage of the solar cells 4 increases. Therefore, the sealing resin sheet pieces 40, 41, The actual benefit of arranging 42 and 43 is great.

  The total thickness of the sealing resin sheet pieces 40, 41, 42, and 43 disposed in the margin 10 on the outer side of the solar battery cell 4 needs to be larger than the thickness of the solar battery cell 4. Here, the total thickness means the total thickness when a plurality of sealing resin sheet pieces 40, 41, 42, 43 are used in an overlapping manner. For example, not only when the sealing resin sheet piece is disposed only between the first sealing resin sheet 20 and the second sealing resin sheet 30, but also the first sealing resin sheet 20 or the second sealing resin sheet 30. The case where it arrange | positions so that it may be pinched | interposed between the some sealing resin sheets which comprise is also included. In the example of FIG. 2, the two sealing resin sheet pieces 40 and 41 arranged between the first sealing resin sheet 20 and the second sealing resin sheet 30 and the second sealing resin sheet 30 are configured. That is, the total thickness (four) of the two sealing resin sheet pieces 42 and 43 sandwiched between the two sealing resin sheets 31, 32, 33 and 34.

  The total thickness of the sealing resin sheet pieces 40, 41, 42, 43 is preferably thicker than the total value of the thickness of the solar battery cell 4 and the thickness of the conductive wire 8, and is 0.2 mm or more thicker than the total value. It is more preferable. Moreover, it is preferable that the total thickness of the sealing resin sheet pieces 40, 41, 42, and 43 is 0.3 mm or more thicker than the thickness of the solar battery cell 4, and more preferably 0.6 mm or more. Specifically, it is preferable that the total thickness of the sealing resin sheet pieces 40, 41, 42, and 43 is 1 to 5 mm. The total thickness of the sealing resin sheet pieces 40, 41, 42, 43 is more preferably 1.5 mm or more, and even more preferably 2 mm or more. Further, it is more preferably 4 mm or less, and further preferably 3 mm or less.

  It is preferable that the sealing resin sheet pieces 40, 41, 42 and 43 are arranged at intervals in the horizontal direction so that the internal air can be discharged therefrom. By securing a passage for positively discharging the internal air, it is possible to suppress the remaining of bubbles, and it is possible to manufacture the solar cell module 1 having a good appearance. At this time, in the case where the sealing resin sheet pieces are directly stacked, it is sufficient that at least one of the sealing resin sheet pieces has a horizontal space between the resin sheet pieces and the internal air can be discharged therefrom. .

  In the example of FIG. 2, the sealing resin sheet piece disposed substantially continuously over the entire periphery of the blank portion 10 on the first sealing resin sheet 20 in the blank portion 10 outside the solar battery cell 4. 40 and a sealing resin sheet piece 41 which is overlapped with each other and arranged with a space therebetween are disposed, and the second sealing resin sheet 30 is superimposed thereon. By disposing the sealing resin sheet pieces 40 continuously at the same height as the solar cells 4 over the entire circumference, it is possible to uniformly fill the molten resin and prevent the generation of bubbles. The sealing resin sheet piece 40 preferably has a width of 50% or more of the blank portion 10 and more preferably has a width of 70% or more. The sealing resin sheet piece 40 may be composed of a plurality of sheet pieces arranged in parallel. It is preferable that the sealing resin sheet piece 41 is disposed on the sealing resin sheet piece 40 so as to be spaced apart from each other, whereby the internal air can be discharged smoothly.

  The solar battery cell 4 is placed on the first sealing resin sheet 20, the sealing resin sheet piece 40 is placed on the outer margin 10 of the solar battery cell 4, and the sealing resin sheet piece 40 is placed on the sealing resin sheet piece 40. After the sealing resin sheet piece 41 is placed, the whole is covered with the sealing resin sheet 31 constituting the second sealing resin sheet 30. Subsequently, the sealing resin sheet piece 42 is intermittently placed on the blank portion 10, covered with the two sealing resin sheets 32 and 33, and the sealing resin sheet piece 43 is intermittently provided on the blank portion 10. It is placed and covered with the sealing resin sheet 34. As a result, the second sealing resin sheet 30 is constituted by the four sealing resin sheets 31, 32, 33, and 34. The suitable thickness of the 2nd sealing resin sheet 30 is the same as the case of the 1st sealing resin sheet 20 already demonstrated. In addition, a total of four sealing resin sheet pieces 40, 41 are also provided, including two sealing resin sheet pieces 42, 43 present in a form sandwiched between four sealing resin sheets 31, 32, 33, 34. , 42 and 43 are overlapped and exist in the margin 10. Here, the second sealing resin sheet 30 only needs to cover substantially the entire surface of the back plate 3, and a part of the second sealing resin sheet 30 may be missing due to the arrangement of the conductive wires. You may be comprised from the several sealing resin sheet arrange | positioned.

  Finally, the back plate 3 is placed on the second sealing resin sheet 30. At this time, the back plate 3 is preferably a glass plate, particularly a glass plate having a warped surface compressive stress of 20 MPa or more. And in the back surface board 3, it is preferable to mount on the 2nd sealing resin sheet 30 so that the inner side of a curvature, ie, a concave surface side may become down. The warpage of the back plate 3 at this time (value measured according to JIS R3206) is preferably 0.05 to 0.5%. If the warpage is too large, there is a possibility that a force for peeling off inside the module after sealing may remain, more preferably 0.4% or less, and further preferably 0.3% or less. On the other hand, when the warpage is too small, there is a possibility that a cell crack may occur due to the load of the back plate 3 being applied to the solar cell 4 near the center of the module during the sealing operation, and more preferably 0.1%. % Or more, and more preferably 0.15% or more.

  Thus, as the light-receiving surface side transparent plate 2 and the back plate 3, a glass plate having a certain warp is used, and the sealing is performed by performing a sealing operation with the concave surfaces facing each other. Can be prevented from being damaged. In 1st invention, the width | variety of the gap | interval part 9 between the adjacent photovoltaic cells 4 is 5 mm or less, and it is difficult to arrange | position a sealing resin sheet piece in the gap | interval part 9. FIG. Therefore, in order to prevent damage to a large number of solar cells 4 to be sealed, it is necessary to arrange the sealing resin sheet pieces 40, 41, 42, and 43 only in the margin 10 outside the solar cells 4. . However, when a large-sized plate glass is supported only by the peripheral portion, the bending due to the weight of the plate glass cannot be ignored. For example, the weight of the 2810 mm × 1795 mm × 12 mm plate glass used as the back plate 3 in Example 1 described later is 151 kg. Then, even if the center part of the back surface plate 3 bends and falls downward by its own weight, the light receiving surface side transparent plate 2 and the back surface plate 3 are not directly loaded with the load on the back surface plate 3. The concave surfaces are sealed facing each other. Normally, when manufacturing laminated glass that does not seal anything inside, it is often pasted after aligning the direction of warpage of the two glass plates, whereas in the present invention, a different method is adopted. To do.

  Next, the configuration of the second invention will be described with reference to the drawings. A feature of the second invention is that a part of the electric wiring is arranged in an overlapping position without coming into contact with the solar battery cell 4, and one sealing is performed in the first sealing resin sheet 20 or the second sealing resin sheet 30. The sealing resin sheet 33 is sealed after being arranged so as to be missing at the electric wiring portion. FIG. 3 is a schematic cross-sectional view of an example of the laminated body 60 before the sealing operation, and shows a cross section cut perpendicularly to the direction in which the plurality of solar battery cells 4 are connected in series.

  The first sealing resin sheet 20 is overlaid on the light-receiving surface side transparent plate 2, and the solar cell 4 is placed thereon. This is substantially the same as in the first invention. In the first invention, the width of the gap 9 between the adjacent solar cells 4 is 5 mm or less, but in the second invention, the gap 9 may be wider. When the width of the gap 9 exceeds 5 mm, it is possible to dispose a sealing resin sheet piece in the gap 9. In this case, it is not necessary to support the plate glass only at the peripheral portion, and the light receiving surface side Even when a glass plate having a certain warp is used as the transparent plate 2 and the back plate 3, the necessity of facing the concave surfaces to each other is low.

  In the example of FIG. 3, the conductive wire 50 is arranged at a position where it does not contact the solar battery cell 4 in addition to the conductive wire 8 that connects adjacent solar battery cells 4. The conducting wire 50 is arranged in parallel to the direction in which the plurality of solar cells 4 are connected in series, and FIG. 3 shows a cross section thereof. This is for electrically connecting the conductor 8 existing at one end of the group of solar cells 4 connected in series to the conductor 8 existing at the other end to form a bypass circuit. Since the conducting wire 50 is disposed at a position overlapping the solar battery cell 4 in the vertical direction, when a load is applied from above and below, an excessive load is applied to the overlapped portion and cell cracking is likely to occur. In the example of FIG. 3, there are two sealing resin sheets that are much thicker than the conductor 50 between the conductor 50 and the solar battery cell 4. However, it is difficult to completely prevent cell cracking. In addition to such an example, when the electric wiring connected to the outside from the solar cell module 1 is pulled out from the hole opened in the back plate 3, the electric wiring overlaps without contacting the solar cell 4. May be placed in position. Various design methods are conceivable depending on the use of the solar cell module 1, and there are various cases in which the electric wiring and the solar cell 4 are arranged to overlap each other.

  The solar battery cell 4 is placed on the first sealing resin sheet 20, the sealing resin sheet piece 40 is placed on the outer margin 10 of the solar battery cell 4, and the sealing resin sheet piece 40 is placed on the sealing resin sheet piece 40. After the sealing resin sheet piece 41 is placed, the whole is covered with the sealing resin sheet 31 constituting the second sealing resin sheet 30. This operation is the same as in the example of FIG. An insulating film 55 is disposed on the sealing resin sheet 31. The insulating film 55 is for ensuring insulation between the conducting wire 50 and the solar battery cell 4, and is arranged so that the tape-like insulating film 55 overlaps the conducting wire 50. At the same time, the sealing resin sheet piece 42 is intermittently placed on the blank portion 10 on the sealing resin sheet 31. And by covering the whole with the sealing resin sheet 32, the insulating film 55 is laminated | stacked via the sealing resin sheets 31 and 32 with the photovoltaic cell 4 and the conducting wire 50, respectively. At this time, in order to connect the conducting wire 50 and the conducting wire 8, the sealing resin sheets 31 and 32 may be appropriately provided with holes or notches. Alternatively, the sealing resin sheets 31 and 32 may be configured by a plurality of sealing resin sheets arranged side by side, and the lead wires 50 may be drawn from the gaps.

  A conducting wire 50 is disposed on the sealing resin sheet 32. As the conducting wire 50, the same thing as the conducting wire 8 can be used. Subsequently, the sealing resin sheet 33 is arranged so as to be missing at the portion of the conducting wire 50. Here, the sealing resin sheet 33 divided into a plurality of sheets is arranged with a gap so that the portion of the conductive wire 50 is not covered with the sealing resin sheet 33 so as to cover the entire surface of the laminate. In this way, by placing the single sealing resin sheet 33 constituting the second sealing resin sheet 30 so as to be missing at the portion of the conducting wire 50, a local load is applied at the portion of the conducting wire 50 in the sealing operation. Is not applied to the solar battery cell 4 and cell cracking can be prevented. The width at which the sealing resin sheet 33 is removed at the portion of the conducting wire 50 only needs to be wider than the width of the conducting wire 50.

  At this time, it is preferable to arrange a sealing resin sheet piece 44 thinner than the sealing resin sheet 33 so as to overlap the conductive wire 50 in a portion where the sealing resin sheet 33 is omitted. As a result, it is possible to prevent bubbles from remaining in the vicinity of the conductor 50. The thickness of the sealing resin sheet piece 44 is preferably 0.1 mm or more thinner than the sealing resin sheet 33. The width of the sealing resin sheet piece 44 may be the same as or narrower than the width of the missing portion, but it should not overlap the sealing resin sheet 33. If they overlap, there is a risk of cell cracking at that portion. Considering the balance between workability and the effect of preventing the generation of bubbles, it is preferable that the width is about 0.5 to 10 mm narrower than the width of the missing portion.

  After the sealing resin sheet 33 and the sealing resin sheet piece 44 are arranged, the sealing resin sheet piece 43 is intermittently placed on the blank portion 10. And after covering the whole with the sealing resin sheet 34, the back surface board 3 is mounted on it.

  In the above, the laminated structure of 1st invention and 2nd invention was demonstrated. Subsequently, the air between the light-receiving surface side transparent plate 2 and the back plate 3 is discharged, heated to melt the resin, and then cooled and sealed. At this time, it is preferable to heat and melt the resin to advance the crosslinking reaction and then cool and seal. The apparatus used for sealing is not particularly limited as long as it can perform an air discharging operation and a heating operation. It is preferable to use a container having a sealing treatment container that accommodates the laminated body 60 and capable of discharging air and heating. At this time, it is preferable that a part or all of the sealing treatment container is made of a gas non-permeable flexible film. A so-called single-vacuum system in which the outside of the sealing treatment container made of a gas non-permeable flexible membrane is kept at atmospheric pressure can be adopted, and two chambers separated by a partition made of a gas non-permeable flexible membrane A so-called double vacuum system that can adjust the degree of vacuum on both sides can also be adopted. The single vacuum method is preferable from the viewpoint of simple equipment. According to the manufacturing method of the present invention, cell cracking can be prevented even in the single vacuum method in which a load is applied from above and below the laminated body 60 before the sealing resin melts. The material of the membrane may be a gas-impermeable flexible membrane, and has a certain degree of flexibility and strength, and when the inside of the membrane is evacuated, the external pressure is uniformly applied to the entire laminate. If it becomes, it will not specifically limit, The sheet | seat and film of rubber | gum and resin can be used.

  The single vacuum type sealing treatment container may be integrated with the heater, or only a part thereof may be made of a gas non-permeable flexible film, but the whole is gas. It is preferable to use a bag 61 made of a non-permeable flexible membrane. In this case, since the sealing treatment container is simply the bag 61, it is possible to flexibly cope with the production of solar cell modules having various shapes and dimensions, and products having various dimensions such as building materials can be used. It is particularly suitable for applications that require manufacturing. When the laminated body 60 is introduced into the bag 61, the entire circumference of the end surface of the laminated body 60 is covered with a bleeder 62 made of a breathable material to prevent the molten resin inside the laminated body 60 from flowing out, It is preferable to secure a discharge route for air from inside the laminate 60. As a material used for the bleeder 62, fabrics such as a woven fabric, a knitted fabric, and a non-woven fabric can be used.

  Thus, when using the bag 61 which consists of a flexible film | membrane with a gas impermeable whole, multiple bags 61 in which the laminated body 60 was introduce | transduced can be arrange | positioned in a heating apparatus. Each bag 61 is connected to a pipe 63 that can be evacuated and connected to a vacuum pump 65 via a pressure regulating valve 64. By such a method, a plurality of pasting operations can be performed together with a simple apparatus.

  When arranged as described above, the air between the light receiving surface side transparent plate 2 and the back plate 3 is discharged, heated to melt the resin, and then cooled and sealed. The temperature condition at this time is not particularly limited, and may be increased to a temperature at which the resin can be melted. If the resin is a crystalline resin, it may be heated to the melting point of the resin or higher. Further, if the sealing resin is a crosslinkable thermoplastic resin, the sealing resin is raised to a crosslinkable temperature and maintained at a crosslinkable temperature for a predetermined time. The pressure is not particularly limited as long as the pressure in the stacked body 60 can be reduced to a pressure that can discharge the air in the stacked body 60 and reduce the remaining bubbles.

  In particular, when sealing in the sealing treatment container, the step of heating the sealing resin while maintaining the pressure in the sealing treatment container at 0.05 MPa or more (step 1), at a temperature below the melting point of the sealing resin A step of reducing the pressure inside the sealing treatment container to a pressure of 0.01 MPa or less (step 2), a step of raising the temperature to a temperature equal to or higher than the melting point of the sealing resin while keeping the pressure reduced (step 3), It is preferable to perform a sealing operation including the steps of increasing the pressure (step 4) and cooling (step 6). Although it is preferable to seal the laminate having the structure of the first invention or the second invention using this method, the present invention is not limited to this.

  The step 1 is a step of heating the sealing resin while maintaining the pressure in the sealing treatment container at 0.05 MPa or more. By maintaining the pressure in the sealing treatment container at 0.05 MPa or more, it is possible to prevent a large load from being applied to the cell from the vertical direction of the laminate 60. More preferably, the pressure is 0.06 MPa or more. Although the pressure in the sealing process container at this time may be atmospheric pressure (0.1 MPa), for example, the leakage of the sealing process container can be checked by reducing the pressure to 0.09 MPa or less. In step 1, since the sealing resin is not yet melted, if there is a leak in the sealing processing container, it can be repaired at this stage. In particular, when a flexible bag is used as the sealing container, it is preferable to reduce the pressure slightly as described above because the bag is easily damaged. When the pressure is reduced from atmospheric pressure to a predetermined pressure of 0.05 MPa or more, it is preferable that the time required for the pressure reducing operation is 10 minutes or more. This is because although a large load is not applied, a rapid decompression operation may cause cell cracking.

  As described above, the sealing resin is softened in advance by heating the sealing resin in a state where the pressure in the sealing processing container is high. The temperature reached by heating at this time is a temperature at which the elastic modulus is lowered while the sealing resin is not melted. Here, the temperature at which the sealing resin does not melt is usually a temperature lower than the melting point (Tm), preferably (Tm-5) ° C. or less, and more preferably (Tm-10). It is below ℃. When the sealing resin does not have a melting point, the melting point referred to here may be replaced with a glass transition point or a softening point. In many sealing resins, a suitable temperature is 65 ° C. or lower, and a more preferable temperature is 60 ° C. or lower. If the temperature is too high, the flow of the resin starts before the pressure in the sealing treatment container drops to 0.01 MPa or less in Step 2, and the passage for discharging the air inside the laminate 60 is blocked. There is a risk that bubbles will be removed and bubbles will remain. The temperature reached by the heating is preferably (Tm-30) ° C. or higher, and more preferably (Tm-20) ° C. or higher. In many sealing resins, a suitable temperature is 40 ° C. or higher, and a more preferable temperature is 45 ° C. or higher. When the said temperature is too low, the fall of the elasticity modulus of sealing resin is inadequate, and when the pressure in a sealing process container is reduced in process 2, there exists a possibility that a cell crack may generate | occur | produce. It is preferable to start the pressure reduction operation in Step 2 after maintaining the temperature in such a temperature range for 5 minutes or more.

  Step 2 is a step of depressurizing the inside of the sealing treatment container to a pressure of 0.01 MPa or less at a temperature lower than the melting point of the sealing resin. By reducing the pressure at a temperature lower than the melting point of the sealing resin, a passage through which the air inside the laminate 60 is discharged is secured. At this time, the pressure in the sealing treatment container is preferably reduced to 0.005 MPa or less. By sufficiently reducing the pressure, the remaining bubbles after sealing can be effectively suppressed. It is preferable that the temperature during pressure reduction from 0.05 MPa to 0.01 MPa in Step 2 is maintained in the same temperature range as the temperature reached by the heating described in Step 1. Further, in order to prevent cell cracking due to an abrupt depressurization operation, it is preferable to slowly depressurize from 0.05 MPa to 0.01 MPa over 5 minutes or more.

  Step 3 is a step of raising the temperature to a temperature equal to or higher than the melting point of the sealing resin while reducing the pressure, and is a step performed subsequent to Step 2. When the temperature of the encapsulating resin is raised, the elastic modulus is greatly lowered near the melting point and changes to a highly viscous liquid. Step 3 is a step in which the pressure is kept reduced until such temperature is reached. If the pressure is increased by lowering the degree of decompression while the elastic modulus is high, air flows into the laminated body 60, and bubbles may remain in the sealing resin. Here, the lower limit value of the temperature reached by the temperature raising operation in Step 3 is preferably (Tm + 10) ° C. or more, and more preferably (Tm + 20) ° C. or more. In many sealing resins, a suitable lower limit is 80 ° C. or higher, and more preferably 85 ° C. or higher. Moreover, an upper limit is 200 degrees C or less normally.

  The rate of temperature increase in step 3 is preferably slow, the time taken to increase the temperature from room temperature to the above temperature is preferably 15 minutes or more, more preferably 30 minutes or more, and more preferably 1 hour or more More preferably. By slowly raising the temperature, a sudden load is not applied and cell cracking can be efficiently prevented. At this time, the temperature increase rate may be changed in the middle, or a balancing operation may be performed to stop the temperature increase and eliminate the temperature distribution inside the laminate 60. From the viewpoint of productivity, the temperature raising time is usually 20 hours or less.

  Step 4 is a step of increasing the pressure in the sealing treatment container, and step 6 is a step of cooling, both of which are performed subsequent to step 3. Either step 4 or step 6 may be performed first, or both steps may be performed simultaneously. In the cooling step of Step 6, the glass is usually cooled to around room temperature. However, if the cooling rate is too fast, the glass may break, and thus cooling is preferably performed for 10 minutes or more, and more preferably for 30 minutes or more.

  In step 4, the pressure is preferably increased slowly, and the time for the pressure increase is preferably 5 minutes or more, more preferably 10 minutes or more, and further preferably 20 minutes or more. From the viewpoint of productivity, the pressurization time is usually 5 hours or less, and preferably 2 hours or less. The pressure after the pressure increase is preferably 0.05 MPa or more, more preferably 0.07 MPa or more, and the pressure can be increased to the same pressure (0.1 MPa) as the atmospheric pressure. At this time, the voltage may be increased stepwise. In step 4, when the temperature at which the pressure is increased is too high, the molten resin may flow unnecessarily, and the cell may move. It is usually 120 ° C. or lower, preferably 100 ° C. or lower.

  In step 4, it is preferable to have a process of simultaneously raising the temperature while increasing the pressure in the sealing treatment container. In this way, in the process of gradually increasing the fluidity, the pressure applied to the laminate 60 can be gradually released, and the molten resin flows unnecessarily while suppressing the generation of residual bubbles. It is effective to suppress. In this case, the temperature at the start of boosting is (Tm-10) ° C. to (Tm + 20) ° C., more preferably (Tm−5) ° C. to (Tm + 15) ° C., and then 3 to 30 ° C., more preferably It is desirable to increase the pressure while raising the temperature from 5 to 20 ° C. The ratio of the pressure increase rate (MPa / min) to the temperature increase rate (° C / min) is preferably 0.001 to 0.1 (MPa / ° C), 0.002 to 0.05 (MPa / ° C). It is more preferable that

  When a crosslinkable thermoplastic resin is used as the sealing resin, after the step of raising the temperature to near the melting point of the sealing resin while reducing the pressure (step 3), the pressure in the sealing treatment container is increased. It is preferable to have a step of raising the temperature to a temperature range where the crosslinking reaction proceeds (step 5) through a step of raising (step 4) (step 5) and a step of cooling (step 6).

  In this case, it is also preferable to raise the pressure in the sealing treatment container in Step 4 and then cool it to a temperature below the melting point and then raise the temperature to a temperature range in which the crosslinking reaction proceeds in Step 5. After raising the pressure, it is possible to raise the temperature to the temperature range where the crosslinking reaction proceeds as it is, but by cooling it once, it is possible to secure a time for the residual stress to relax, and the melted resin can overflow and sink. (The portion where the resin is missing at the end), the movement of the cell can be more effectively suppressed. At this time, it is preferable to cool until the resin sufficiently loses fluidity, and it is preferable to cool to (Tm-10) ° C. or lower, more preferably to (Tm-20) ° C. or lower.

  As described above, after increasing the pressure in the sealing treatment container, the temperature is raised to a temperature range where the crosslinking reaction proceeds in Step 5 to advance the crosslinking reaction. Usually, the crosslinking reaction proceeds by heating to 100 ° C or higher, preferably 120 ° C or higher, more preferably 130 ° C or higher, and even more preferably 140 ° C or higher. In order to prevent deterioration of the resin, a crosslinking temperature of 200 ° C. or lower is usually employed. The time for maintaining the temperature range in which the crosslinking reaction proceeds varies depending on the desired degree of crosslinking and the like, but is usually 5 minutes to 2 hours, preferably 10 minutes to 1 hour.

  The pressure in the sealing treatment container when the crosslinking reaction is advanced in step 5 is preferably 0.05 MPa or more, and more preferably 0.06 MPa or more. By increasing the pressure in the sealing processing container, the pressure applied from above and below can be reduced. Since the crosslinking reaction proceeds at a high temperature, the melt viscosity of the sealing resin at that time is considerably lower than the vicinity of the melting point. Therefore, at this time, it is important not to apply unnecessary pressure from above and below, but to suppress the movement of the cell and the protrusion of the resin. However, when the pressure is increased to the same pressure as the atmospheric pressure, sinking may occur depending on the configuration of the laminated body. In such a case, it is preferable to set the pressure lower than the atmospheric pressure. In addition, if the pressure is increased to the same pressure as the atmospheric pressure, the bleeder may be difficult to press around the laminate and the resin may protrude, so in such a case, the pressure should be set lower than the atmospheric pressure. Is preferred. In that case, the pressure is preferably 0.001 MPa or more lower than atmospheric pressure, and preferably 0.01 MPa or more (in this case, 0.09 MPa or less). The atmospheric pressure as used in the present invention refers to a state in which no positive pressure or depressurization operation is performed. For example, hot air is forcibly blown into the hot air furnace by a fan, so that the atmospheric pressure is slightly higher than atmospheric pressure. Even in such a case, it is substantially the same as the atmospheric pressure.

  After the crosslinking reaction has proceeded in step 5, it is subjected to the cooling step in step 6. Step 6 is as described above.

  The solar cell modules obtained in this way are regularly arranged without damaging a plurality of solar cells. Since a large number of solar battery cells can be sealed with resin without being damaged, a large-sized solar battery module can be provided. In addition, the remaining of bubbles is suppressed, the protrusion of the resin from the end portion is also suppressed, and the resin is properly aligned and has a beautiful appearance. Therefore, it is suitably used for the outer walls, roofs, windows, etc. of various buildings.

  Hereinafter, the present invention will be described in more detail using examples.

Example FIG. 4 shows the outer shape of the solar cell module 1 and the solar cells 4 arranged therein. As the solar cell 4, 416 single-crystal silicon solar cells of 100 mm × 100 mm × 0.3 mm square were used. The four corners are chamfered about several mm. As the conducting wire 8, a solder dip copper ribbon wire manufactured by Hitachi Cable, Ltd. was used. The ribbon wire has a width of 1.5 mm and a thickness of 0.15 mm. Solder is printed in advance on a portion where the light receiving surface 6 of the solar battery cell 4 and the conductive wire 8 on the back surface 7 are bonded. One end of the conductor 8 was overlapped and soldered to the solder printing portion of the light receiving surface 6 of the solar battery cell 4, and the other end was overlapped and soldered to the solder printing portion of the back surface 7 of the adjacent solar battery cell 4. Adjacent cells were connected by two conducting wires 8 so that the distance between them was 2 mm. That is, the width of the gap 9 is 2 mm.

  As the light-receiving surface side transparent plate 2, float plate tempered glass (white plate glass) of 2810 mm × 1795 mm × 12 mm was used. The surface compressive stress of the tempered glass was 100 MPa, and the warpage measured in accordance with JIS R3206 was 0.25%. As the sealing resin sheet, unless otherwise specified, a 0.6 mm thick sheet of “Solar Eva SC36” manufactured by Hisheet Kogyo Co., Ltd. was used. The sealing resin sheet is obtained by blending an ethylene-vinyl acetate copolymer (EVA) with a crosslinking agent, a silane coupling agent, a stabilizer and the like, and the melting point measured by the DSC method of the resin before crosslinking is 71 ° C. It is. A shallow embossed pattern (pear texture) is formed on one side of the sealing resin sheet, and the depth is about 45 μm. Three sealing resin sheets 21, 22, and 23 having a size of 2810 mm × 1795 mm were stacked thereon so that the warped concave surface of the light-receiving surface side transparent plate 2 was on top. The three sealing resin sheets 21, 22, and 23 constitute a first sealing resin sheet 20 having a thickness of 1.8 mm.

  5 to 10 are enlarged views of an upper left portion and an upper right portion (portion surrounded by a one-dot chain line) in FIG. As shown in FIG. 5, 16 sets of 26 solar cells 4 connected in series in the longitudinal direction are arranged in parallel at intervals of 2 mm, and a total of 416 cells are placed on the first sealing resin sheet 20. Arranged. The width of the gap 9 between the adjacent solar battery cells 4 is 2 mm both vertically and horizontally. In the edge part of the photovoltaic cell 4 arrange | positioned in series, the conducting wires 8 connected to the photovoltaic cell 4 were connected with the conducting wire 51 of the position 5 mm away. The distance from the end of the solar battery cell 4 to the end of the light-receiving surface side transparent plate 2, that is, the width of the margin 10 was 80 mm at the left and right ends and 82.5 mm at the upper and lower ends in FIG. In the margin portion 10 on the left side of the figure, the conducting wires 51 are connected by a conducting wire 52. As the conducting wires 51 and 52, solder dip copper ribbon wires having a width of 4.0 mm and a thickness of 0.25 mm were used.

  Subsequently, as illustrated in FIG. 6, the sealing resin sheet piece 40 is disposed in the blank portion 10. The sealing resin sheet piece 40 was disposed along the end of the light-receiving surface side transparent plate 2 over the entire circumference of the blank portion 10. In the left and right margin portions 10 (width is 80 mm), the width of the sealing resin sheet piece 40 is 49 mm, and in the upper and lower margin portions 10 (width is 82.5 mm), the width of the sealing resin sheet piece 40 is 51. 5 mm. Inside the sealing resin sheet piece 40, a sealing resin sheet piece 45 having a width of 15 mm was arranged in parallel to the sealing resin sheet piece 40 with an interval of about 8 mm. The distance between the sealing resin sheet piece 45 and the end of the solar battery cell 4 is about 8 mm. At this time, the left margin 10 was shifted slightly outward from the other margins 10 so that the sealing resin sheet piece 45 did not overlap the conductor 52. By disposing the sealing resin sheet piece 45 narrower than the sealing resin sheet piece 40 inside, when the sealing resin sheet piece 40 is melted by heating, it becomes non-uniform in the direction of the solar cells 4. Inflow can be prevented. Thereby, a movement of the photovoltaic cell 4 and generation | occurrence | production of a bubble can be prevented. Thereafter, a sealing resin sheet piece 41 having a length of 100 mm and a width of 10 mm was intermittently disposed along the end of the light-receiving surface side transparent plate 2. Thereby, a gap can be provided between the sealing resin sheet 31 and the sealing resin sheet piece 40 that are subsequently laminated, and the air in the space formed between the sealing resin sheet 23 and the sealing resin sheet 31. Can be discharged smoothly.

  Subsequently, as shown in FIG. 7, a gap 36 having a width of 5 mm is formed in each of the portion of the conducting wire 51 existing in the right margin portion 10 and the portion of the conducting wire 52 existing in the left margin portion 10 so that almost the entire surface is 3 It was covered with a sealing resin sheet 31 composed of a single sheet. It is possible to connect the conductor 50 to the conductors 51 and 52 through the gap 36. Next, the sealing resin sheet piece 42 having a length of 100 mm and a width of 10 mm was intermittently disposed along the end of the light-receiving surface side transparent plate 2. In addition, an insulating film 55 having a width of 10 mm and a thickness of 0.1 mm was disposed at a position overlapping the lower side of the conductive wire 50 disposed later. Further, an insulating film 56 having a width of 30 mm, a length of 100 mm, and a thickness of 0.1 mm was also disposed at a position overlapping the lower side of the conductive wires 53 and 54 to be disposed later.

  Next, as shown in FIG. 8, a gap 36 having a width of 5 mm is provided in each of the portion of the conducting wire 51 existing in the right margin portion 10 and the portion of the conducting wire 52 existing in the left margin portion 10, so that almost the entire surface is formed. It was covered with a sealing resin sheet 32 composed of three sheets. Next, the lead wire 51 existing in the right margin 10 and the lead wire 52 present in the left margin 10 were connected by the lead 50, and the lead 50 was placed on the sealing resin sheet 32. As the lead wire 50, a solder dip copper ribbon wire having a width of 6 mm and a thickness of 0.1 mm was used. In addition, two conductive wires 53 and 54 led out to the terminal box were connected to an electrical wiring (not shown) existing in the left margin 10. The conducting wires 53 and 54 are the same as the conducting wire 50. An element such as a diode may be incorporated in the electrical wiring (not shown) or the conducting wire 52 present in the left margin 10 according to the module specifications.

  Subsequently, as shown in FIG. 9, the portion of the conductive wire 50 is missing with a width of about 20 mm, the portions of the conductive wires 53 and 54 are covered with the missing sealing resin sheet 33 with a size of 40 × 130 mm, On the conducting wire 50, a sealing resin sheet piece 44 having a width of 15 mm made of “Solar EVA SC36” manufactured by Hisheet Kogyo Co., Ltd. and having a thickness of 0.4 mm was disposed. Further, a sealing resin sheet piece 46 having a thickness of 0.4 mm was disposed on the missing portions of the conducting wires 53 and 54 so as to cover substantially the entire missing range. Next, a sealing resin sheet piece 43 having a length of 100 mm and a width of 10 mm was intermittently disposed along the end of the light-receiving surface side transparent plate 2.

  Subsequently, the entire surface was covered with a sealing resin sheet 34. As shown in FIG. 10, the encapsulating resin sheet 34 is provided with a notch 37 having a length of 300 mm, and the two lead wires 53 and 54 drawn out to the terminal box are drawn out from the notch. Thereafter, the back plate 3 was stacked. As the back plate 3, float plate tempered glass (blue plate glass) of 2810 mm × 1795 mm × 12 mm was used. The surface compressive stress of the tempered glass was 100 MPa, and the warpage measured in accordance with JIS R3206 was 0.25%. Further, the back plate 3 is provided with a 20 mm diameter circular opening through which the two conducting wires 53 and 54 drawn out to the terminal box are passed. Two conductive wires 53 and 54 were drawn out from the opening provided in the back plate 3 and overlapped with the back plate 3 with the concave surface down.

  As described above, a laminate 60 for use in the sealing operation was obtained. Here, the 1st sealing resin sheet 20 consists of three sealing resin sheets, and the total thickness is 1.8 mm. Moreover, the 2nd sealing resin sheet 30 consists of four sealing resin sheets, and the total thickness is 2.4 mm. Moreover, the total thickness of the sealing resin sheet pieces 40, 41, 42, and 43 disposed in the blank portion 10 was 2.4 mm.

  The entire periphery of the end face of the laminate 60 obtained in this way was covered with a bleeder 62, and put into a rubber bag 61 as a sealing treatment container, and the bag 61 was sealed. The reason why the end surface of the laminated body 60 is covered with the bleeder 62 is to prevent the molten resin inside the laminated body 60 from flowing out and to secure a discharge route for air from the inside of the laminated body 60.

  A plurality of sets of the rubber bags 61 are arranged on a shelf 67 provided in a hot stove 66. Each rubber bag 61 is connected to an evacuable pipe 63, which is connected to a vacuum pump 65 via a pressure regulating valve 64. A schematic diagram of the sealing processing apparatus is shown in FIG.

  After setting as described above, the sealing processing operations of the following steps 1 to 6 were performed. The temperature and pressure at this time were controlled as shown in Table 1 and FIG. At this time, the temperature is the temperature in the hot stove 66 and the pressure is the pressure set by the pressure regulating valve 64.

Step 1: “Step of heating the sealing resin while maintaining the pressure in the sealing treatment container at 0.05 MPa or more”
While starting the temperature rise in the hot stove 66, the pressure reduction in the sealing process container was started. The pressure was slowly reduced from atmospheric pressure (0.1 MPa) to 0.07 MPa over 45 minutes, during which time the temperature was slowly increased from room temperature (30 ° C.) to 50 ° C.

Step 2: “Step of reducing the pressure in the sealing treatment container to a pressure of 0.01 MPa or less at a temperature lower than the melting point of the sealing resin”
The temperature in the hot stove 66 was maintained at 50 ° C. for 30 minutes, during which time the pressure in the sealing treatment vessel was slowly reduced from 0.07 MPa to less than 0.005 MPa.

Step 3: “Step of raising the temperature to a temperature equal to or higher than the melting point of the sealing resin with reduced pressure”
The temperature in the hot stove 66 is raised from 50 ° C. to 60 ° C. over 120 minutes, raised from 60 ° C. to 71 ° C. (melting point of the sealing resin) over 150 minutes, and maintained at 71 ° C. for 10 minutes. Then, the temperature was raised from 71 ° C. to 78 ° C. over 45 minutes. During this time, the pressure in the sealing treatment container was maintained at less than 0.005 MPa.

Step 4: “Step of increasing the pressure in the sealing treatment container”
In step 3, the pressure increase was started when the temperature in the hot stove 66 reached 78 ° C., and the pressure in the sealing treatment vessel was slowly increased from less than 0.005 MPa to 0.07 MPa over 70 minutes. During this time, the temperature was slowly increased from 78 ° C. to 90 ° C. over 75 minutes. The ratio of the pressure increase rate (MPa / min) to the temperature increase rate (° C./min) at this time was 0.0063 (MPa / ° C.). Thereafter, the temperature was maintained at 90 ° C. for 30 minutes, cooled to 30 ° C. over 30 minutes, maintained at 30 ° C. for 5 minutes, and a pressure of 0.07 MPa was maintained during that time.

Step 5: “Step of raising the temperature to a temperature range where the crosslinking reaction proceeds to advance the crosslinking reaction”
Subsequently, the temperature was raised from 30 ° C. to 155 ° C. over 90 minutes and maintained at 155 ° C. for 36 minutes to proceed the crosslinking reaction. Meanwhile, a pressure of 0.07 MPa was maintained.

Process 6: “Cooling process”
Subsequently, the pressure was decreased from 155 ° C. to 30 ° C. over 60 minutes while maintaining the pressure of 0.07 MPa. When the temperature reached 30 ° C., the pressure in the sealing treatment container was increased to 0.1 MPa (large) over about 1 minute. The pressure was raised to (atmospheric pressure) and removed from the hot stove 66.

  In the obtained solar cell module, there were no cell cracks or chipping, no wire breakage, no bubble residue was observed, and no protrusion or sink of the sealing resin at the periphery was observed. Moreover, the photovoltaic cells were regularly arranged and sealed.

It is a cross-sectional schematic diagram of an example of the solar cell module after sealing operation. It is a cross-sectional schematic diagram of an example of the laminated body before sealing operation. It is a cross-sectional schematic diagram of another example of the laminated body before sealing operation. It is the schematic diagram which showed the external shape of the solar cell module manufactured in the Example, and the photovoltaic cell arranged in it. It is the figure (the 1) which showed the manufacturing process of the laminated body in an Example. It is the figure (the 2) which showed the manufacturing process of the laminated body in an Example. It is the figure (the 3) which showed the manufacturing process of the laminated body in an Example. It is the figure (the 4) which showed the manufacturing process of the laminated body in an Example. It is the figure (the 5) which showed the manufacturing process of the laminated body in an Example. It is the figure (the 6) which showed the manufacturing process of the laminated body in an Example. It is the schematic of a sealing processing apparatus. It is the figure which showed the temperature and pressure at the time of the sealing process in an Example.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Solar cell module 2 Light-receiving surface side transparent plate 3 Back surface plate 4 Solar cell 5 Resin 8 Conductor 9 Gap part 10 Blank part 20 1st sealing resin sheet 30 2nd sealing resin sheet 40-46 Sealing resin sheet piece 50 ~ 54 Conductor 55,56 Insulation film 60 Laminate 61 Bag 66 Hot stove

Claims (5)

In a method for manufacturing a solar cell module in which a plurality of solar cells are sealed with a resin between a light-receiving surface side transparent plate and a back plate, a plurality of solar cells are arranged with a space between each other and lead wires are used. connect, the first sealing resin sheet covering substantially the entire surface of the light receiving side transparent plate between the light-receiving surface side transparent board and the solar battery cell made of a glass plate is placed, the back surface plate and the sun made of a glass plate By disposing a second sealing resin sheet covering substantially the entire surface of the back plate between the battery cells and laminating a plurality of sealing resin sheets on the first sealing resin sheet or the second sealing resin sheet configured, the electrical wiring portion and arranged parallel to the solar cells to vertically overlap position without contacting the solar cell, a plurality in the first sealing resin sheet or the second sealing resin in the sheet one of the sealing resin sheet of the sealing resin sheet The arranged such that lost wider than the width of the electrical wiring portion of the electric wiring, while allowing the local loads in the portion of electrical wiring not be applied to the solar cell in the sealing operation, the light receiving surface A method for producing a solar cell module, comprising: discharging air between a side transparent plate and a back plate, heating and melting the resin, and then cooling and sealing.   The method for manufacturing a solar cell module according to claim 1, wherein a sealing resin sheet thinner than the missing sealing resin sheet is filled in a portion where the sealing resin sheet is missing in the electrical wiring portion.   The sun according to claim 1 or 2, wherein an insulating film is disposed between the electric wiring and the solar battery cell, and the insulating film is laminated to the solar battery cell and the electric wiring via a sealing resin sheet, respectively. Manufacturing method of battery module.   When sealing in the sealing treatment container, the step of heating the sealing resin while maintaining the pressure in the sealing treatment container at 0.05 MPa or more (step 1), the sealing treatment at a temperature below the melting point of the sealing resin A step of depressurizing the inside of the container to a pressure of 0.01 MPa or less (step 2), a step of raising the temperature to a temperature equal to or higher than the melting point of the sealing resin with the pressure reduced (step 3), and increasing the pressure in the sealing treatment vessel The manufacturing method of the solar cell module in any one of Claims 1-3 which perform sealing operation which consists of each process of the process to perform (process 4) and the process to cool (process 6). The method for manufacturing a solar cell module according to any one of claims 1 to 4, wherein the sealing resin is made of a kind of resin selected from the group consisting of an ethylene-vinyl acetate copolymer, polyvinyl butyral, and polyurethane.

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