Solar module laminating device
By introducing a centering adjustment mechanism into the lamination device, the problem of displacement of perovskite solar modules during the lamination process was solved, ensuring the centering and encapsulation quality of the modules and improving their stability and mechanical strength.
Patent Information
- Application Number
- CN202520391048.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-07
- Publication Date
- 2026-02-17
- Estimated Expiration
- 2035-03-07
AI Technical Summary
Perovskite solar modules are prone to misalignment during the lamination process, resulting in poor encapsulation and affecting the module's processing quality.
A solar module lamination device was designed, comprising a frame, a transport mechanism, a centering adjustment mechanism, and a lamination mechanism. The device is floatingly connected to the frame via an adjustment component, which adjusts the position of the module in real time to ensure that it is centered before lamination.
It effectively prevents the perovskite solar modules from shifting during the lamination process, ensuring the quality and mechanical strength of the laminated modules, and improving the stability and weather resistance of the encapsulation.
Smart Images
Figure CN223928762U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of solar module processing technology, and in particular to a solar module lamination device. Background Technology
[0002] Perovskite solar cells, as representatives of third-generation solar cells, have received widespread attention in both academia and industry in recent years due to their high photoelectric conversion efficiency, low cost, and ease of large-scale fabrication. Compared with traditional silicon-based solar cells, perovskite solar cells have higher absorption coefficients and tunable photoelectric performance, giving them significant advantages in improving photoelectric conversion efficiency and reducing costs. However, perovskite materials are inherently sensitive to air and moisture, posing a serious challenge to their long-term stability and lifespan. Effective encapsulation is crucial to ensure that perovskite solar modules maintain high and stable performance in practical applications. The encapsulation process must not only isolate the perovskite material from air and moisture to prevent degradation but also ensure good mechanical strength and weather resistance during long-term use. Existing perovskite solar module encapsulation technologies mainly employ lamination processes, which involve tightly bonding perovskite cell units with transparent conductive glass and encapsulation materials through heating and pressurization.
[0003] In existing equipment, when encapsulating perovskite solar modules, workers need to place the solar panels with POE film applied inside before lamination and encapsulation. However, the perovskite solar modules being transported into the laminator can shift due to worker placement or natural vibrations during machine transport, resulting in poor lamination and affecting the processing effect.
[0004] Therefore, there is an urgent need to design a solar module lamination device to solve the above problems. Utility Model Content
[0005] The purpose of this invention is to provide a solar module lamination device that ensures the solar module is centered during lamination, thereby ensuring the quality of the laminated solar module.
[0006] To achieve this objective, the present invention adopts the following technical solution:
[0007] Solar module lamination apparatus, including:
[0008] The frame extends along the first direction;
[0009] A transport mechanism, installed on the aforementioned rack, is capable of transporting solar modules along the aforementioned first direction;
[0010] The centering adjustment mechanism includes two adjustment components, which are symmetrically arranged on both sides of the frame to form an adjustment channel. Each adjustment component includes an adjustment member, which is floatingly connected to the corresponding side of the frame and located on the upper side of the transport mechanism. Both sides of the solar panel can respectively abut against the adjustment member.
[0011] A laminating mechanism is provided on the frame and located downstream of the central adjustment mechanism, and the laminating mechanism is configured to press the solar panels on the transport mechanism.
[0012] As an optional solution, the aforementioned adjusting element includes:
[0013] An adjustment section extends along the first direction and is located on the upper side of the transport mechanism, and two opposing adjustment sections form the adjustment channel.
[0014] The machine includes a through-hole and a first limiting part. The through-hole extends along the second direction and passes through the frame. One end of the through-hole is connected to the adjustment part, and the other end is connected to the first limiting part. The first limiting part is located on the outside of the frame, and the first direction is perpendicular to the second direction.
[0015] The aforementioned adjustment assembly also includes a first elastic element, one end of which is connected to the outer side of the frame and the other end of which is connected to the first limiting part.
[0016] As an optional solution, the side wall of the frame is provided with an elongated hole extending along the first direction, the through-hole is provided through the elongated hole, at least two through-holes are provided at intervals along the first direction, and the first limiting part and the first elastic member are provided in one-to-one correspondence with the through-holes.
[0017] As an alternative, the entry end of the aforementioned adjustment unit facing the adjustment channel is arranged in an arc shape.
[0018] As an alternative, the aforementioned transport mechanism is a conveyor belt, on which a follower is protruding, and the aforementioned solar panel is placed on the conveyor belt and can abut against the aforementioned follower.
[0019] As an optional solution, the above lamination mechanism includes:
[0020] The lamination chamber is installed on the aforementioned frame and located above the aforementioned transport mechanism;
[0021] A lifting drive and a laminating component are provided. The lifting drive is installed in the laminating chamber, and the laminating component is floatingly connected to the output end of the lifting drive.
[0022] As an optional embodiment, the lamination mechanism further includes a connecting component, which comprises:
[0023] The limiting member has one end connected to the output end of the lifting drive member, and a floating space is formed inside the limiting member. The other end of the limiting member is constructed as a second limiting part, and a through hole communicating with the floating space is opened on the second limiting part. The cross-sectional size of the through hole is smaller than the cross-sectional size of the floating space.
[0024] A floating component includes a floating part, the floating part including a connected third limiting part and a connecting part, the cross-sectional shape of the third limiting part being consistent with the cross-sectional shape of the floating space and located within the floating space, the cross-sectional shape of the connecting part being consistent with the cross-sectional shape of the perforation and passing through the perforation, and the end of the connecting part away from the third limiting part being connected to the laminate.
[0025] The second elastic element has one end abutting against the aforementioned floating component and the other end abutting against the inner wall of the aforementioned floating space.
[0026] As an optional solution, the floating component further includes a damping element disposed within the floating space, one end of the second elastic element abutting against one side of the damping element, and the other side of the damping element being the third limiting portion.
[0027] As an alternative, the aforementioned laminating chamber has an opening and a lifting space facing the aforementioned transport mechanism. The lifting space extends along a third direction, and the aforementioned laminate can slide within the lifting space along the aforementioned third direction, which is perpendicular to the aforementioned first direction.
[0028] As an alternative, a blower is also included, which is installed in the lamination chamber and located upstream of the lamination member. The blower is configured to blow air onto the solar module to remove dust from the surface of the solar module.
[0029] The beneficial effects of this utility model are as follows:
[0030] This invention provides a solar module lamination device. By setting a centering adjustment mechanism, the solar module is placed on a transport mechanism before lamination. As the transport mechanism moves downstream in a first direction, the solar module enters the adjustment channel. At the same time, the two sides of the solar module abut against the corresponding adjustment components. Since the adjustment components are floatingly connected to the frame, the two symmetrical adjustment components can apply a counterforce to the tilted side of the solar module when it tilts, thereby keeping the solar module in the center position of the transport mechanism in the adjustment channel. After being centered, the solar module is centered when it reaches the lamination mechanism for lamination, thus ensuring the quality of the laminated solar module. Attached Figure Description
[0031] Figure 1 This is a schematic diagram of the structure of the solar module lamination device provided in this embodiment of the utility model;
[0032] Figure 2 This is a schematic diagram of the structure of the adjustment component provided in an embodiment of the present invention;
[0033] Figure 3 This is a cross-sectional view of the lamination mechanism and the blower provided in this embodiment of the utility model;
[0034] Figure 4 yes Figure 3 Enlarged view of point A in the middle.
[0035] In the picture:
[0036] 10. Frame; 11. Side panel; 111. Long strip hole; 12. Base plate;
[0037] 20. Transportation mechanism; 21. Conveyor belt; 22. Follower component;
[0038] 30. Centering adjustment mechanism; 31. Adjustment assembly; 311. Adjustment component; 3111. Adjustment section; 3112. Through section; 3113. First limiting section; 3114. Mounting section; 312. First elastic element; 32. Adjustment channel;
[0039] 40. Lamination mechanism; 41. Lamination chamber; 411. Lifting space; 412. Air blowing channel; 413. Air blowing pipe; 42. Lifting drive component; 43. Lamination component; 44. Connecting assembly; 441. Limiting component; 4411. Floating space; 4412. Second limiting part; 4413. Perforation; 442. Floating assembly; 4421. Damping component; 4422. Floating component; 44221. Third limiting part; 44222. Connecting part; 443. Second elastic component;
[0040] 50. Air blower; 200. Solar panel. Detailed Implementation
[0041] The present invention will now be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present invention and not intended to limit it. Furthermore, it should be noted that, for ease of description, the accompanying drawings show only the parts relevant to the present invention, not the entire structure.
[0042] In the description of this utility model, unless otherwise explicitly specified and limited, the terms "connected," "linked," and "fixed" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral part; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.
[0043] In this invention, unless otherwise explicitly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.
[0044] In the description of this embodiment, the terms "upper," "lower," "left," and "right," etc., refer to the orientation or positional relationship shown in the accompanying drawings. They are used only for ease of description and simplification of operation, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first" and "second" are only used for distinction in description and have no special meaning.
[0045] This embodiment provides a solar module lamination device that ensures the solar module 200 is centered during lamination, thereby ensuring the quality of the laminated solar module 200. Figure 1 and Figure 2 As shown, the solar module laminating device includes a frame 10, a transport mechanism 20, a centering adjustment mechanism 30, and a laminating mechanism 40. The frame 10 extends along a first direction (X direction in the figure). The transport mechanism 20 is installed on the frame 10 and can transport solar modules 200 along the first direction. The centering adjustment mechanism 30 includes two adjustment components 31, which are symmetrically arranged on both sides of the frame 10 to form an adjustment channel 32. Each adjustment component 31 includes an adjustment element 311, which is floatingly connected to the corresponding side of the frame 10 and located on the upper side of the transport mechanism 20. Both sides of the solar module 200 can abut against the adjustment element 311 respectively. The laminating mechanism 40 is disposed on the frame 10 and located downstream of the centering adjustment mechanism 30. The laminating mechanism 40 is configured to press the solar modules 200 on the transport mechanism 20.
[0046] The aforementioned solar module laminating device, by setting a centering adjustment mechanism 30, places the solar module 200 onto the transport mechanism 20 before lamination by the laminating mechanism 40. As the transport mechanism 20 moves downstream in the first direction, the solar module 200 enters the adjustment channel 32. At the same time, the two sides of the solar module 200 abut against the corresponding adjustment members 311. Since the adjustment members 311 are floatingly connected to the frame 10, the two symmetrical adjustment members 31 can apply a reverse force to the tilted side of the solar module 200 when it tilts, thereby making the solar module 200 in the adjustment channel 32 in the center position of the transport mechanism 20. After being centered, when the solar module 200 reaches the laminating mechanism 40 for lamination, it is in the center position, thereby ensuring the quality of the laminated solar module 200.
[0047] The frame 10 is U-shaped and includes a base plate 12 and two side plates 11. The two side plates 11 are connected to the two sides of the base plate 12 at intervals along a second direction (Y direction in the figure, which is perpendicular to the X direction). The transport mechanism 20 is located between the two side plates 11.
[0048] Optionally, such as Figure 2 As shown, the adjusting member 311 includes an adjusting part 3111, a through part 3112, and a first limiting part 3113. The adjusting part 3111 extends along a first direction and is located on the upper side of the transport mechanism 20. Two opposing adjusting parts 3111 form an adjusting channel 32. The through part 3112 extends along a second direction and is disposed through the frame 10. One end of the through part 3112 is connected to the adjusting part 3111, and the other end is connected to the first limiting part 3113. The first limiting part 3113 is located on the outside of the frame 10. The adjusting assembly 31 also includes a first elastic member 312. One end of the first elastic member 312 is connected to the outside of the frame 10, and the other end is connected to the first limiting part 3113. Understandably, before the solar module 200 enters the adjustment channel 32, the first elastic member 312 is not subjected to external force, and the distance between the two adjustment members 311 is slightly smaller than the width of the solar module 200. When the solar module 200 enters the adjustment channel 32, the adjustment part 3111 receives a squeezing force and moves in the direction away from the adjustment channel 32, thereby driving the through part 3112 and the first limiting part 3113 to move outward at the same time. The outward movement of the first limiting part 3113 causes one end of the first elastic member 312 to be stretched outward. Thus, when the solar module 200 squeezes the adjustment part 3111, the first elastic member 312 also has a squeezing and adjusting effect on the solar module 200. Since the specifications of the first elastic members 312 on both sides are the same, when the solar module 200 is offset, the reaction force of the first elastic member 312 on the offset side will be greater, forcing the solar module 200 to move to the other side until the elastic force of the first elastic members 312 on both sides is balanced, thereby achieving the centering adjustment of the solar module 200.
[0049] In this embodiment, one end of the first elastic member 312 is welded to the corresponding side plate 11, and the other end is welded to the corresponding first limiting part 3113. In other embodiments, the connection of the first elastic member 312 can also be achieved by bonding, riveting, etc., which is not limited here. In addition, in order to facilitate the installation of the adjusting part 311, the first limiting part 3113 and the through part 3112 are detachably provided, or the adjusting part 3111 and the through part 3112 are detachably provided, to prevent interference with the side plate 11 during installation.
[0050] Optionally, such as Figure 1 and Figure 2 As shown, the side wall of the frame 10 has an elongated hole 111 extending along a first direction. A through-hole 3112 is disposed through the elongated hole 111, and at least two through-holes 3112 are spaced apart along the first direction. A first limiting part 3113 and a first elastic member 312 are disposed corresponding to each through-hole 3112. This arrangement ensures that the reaction force of the first elastic member 312 acting on the adjusting part 3111 in the first direction is balanced. In this embodiment, three through-holes 3112 are provided. In other embodiments, the number of through-holes 3112 can be two, four, or more, and is not limited here.
[0051] Optionally, the entry end of the adjusting part 3111 facing the adjusting channel 32 is arranged in an arc shape. This can prevent the solar module 200 from colliding with the end of the adjusting part 3111 when it enters the adjusting channel 32, and at the same time, it can gradually guide the solar module 200 into the adjusting channel 32.
[0052] Optionally, the adjusting member 311 further includes a mounting portion 3114, which is located inside the frame 10. The adjusting portion 3111 is mounted on one side of the mounting portion 3114, and the through portion 3112 is connected to the other side of the adjusting portion 3111. This arrangement prevents the connecting portion 44222 from being directly connected to the adjusting portion 3111, ensuring the integrity of the adjusting portion 3111 and its structural strength.
[0053] Optionally, such as Figure 1 As shown, the transport mechanism 20 is a conveyor belt 21, and a follower 22 is protruding from the conveyor belt 21. The solar panel 200 is placed on the conveyor belt 21 and can abut against the follower 22. With the above arrangement, when the solar panel 200 moves downstream with the conveyor belt 21, its movement in the first direction is restricted by the follower 22, further preventing the solar panel 200 from shifting.
[0054] The conveyor rollers and conveyor motors that are matched with the conveyor belt 21 are existing technologies and will not be described in detail here.
[0055] Optionally, such as Figure 1 and Figure 3 As shown, the lamination mechanism 40 includes a lamination chamber 41, a lifting drive 42, and a laminating component 43. The lamination chamber 41 is mounted on the frame 10 and located above the transport mechanism 20. The lifting drive 42 is mounted on the lamination chamber 41, and the laminating component 43 is floatingly connected to the output end of the lifting drive 42. This design prevents excessive instantaneous impact on the solar module 200 when the laminating component 43 is pressed down, thus preventing damage to the solar module 200.
[0056] Optionally, such as Figure 3 As shown, the laminate 43 has a heating function, which can increase the lamination speed. This part is prior art and will not be described in detail here.
[0057] Optionally, such as Figure 3 and Figure 4 As shown, the lamination mechanism 40 also includes a connecting component 44, which includes a limiting member 441, a floating component 442, and a second elastic member 443. One end of the limiting member 441 is connected to the output end of the lifting drive member 42, and a floating space 4411 is formed inside the limiting member 441. The other end of the limiting member 441 is constructed as a second limiting part 4412, and a through hole 4413 communicating with the floating space 4411 is opened on the second limiting part 4412. The cross-sectional dimension of the through hole 4413 is smaller than the cross-sectional dimension of the floating space 4411. The floating component 442 includes a floating member 441. 422, the floating member 4422 includes a connected third limiting part 44221 and a connecting part 44222. The cross-sectional shape of the third limiting part 44221 is consistent with the cross-sectional shape of the floating space 4411 and is located within the floating space 4411. The cross-sectional shape of the connecting part 44222 is consistent with the cross-sectional shape of the perforation 4413 and is provided through the perforation 4413. One end of the connecting part 44222 away from the third limiting part 44221 is connected to the laminate 43. One end of the second elastic member 443 abuts against the floating assembly 442, and the other end abuts against the inner wall of the floating space 4411. With the above settings, when the laminate 43 is not pressed against the solar module 200, the third limiting part 44221 abuts against the second limiting part 4412 due to the action of the second elastic member 443. When the laminate 43 is pressed down, the second elastic member 443 is compressed, and the third limiting part 44221 moves upward in the floating space 4411, thereby realizing the floating connection between the laminate 43 and the output end of the lifting drive member 42.
[0058] In this embodiment, the lifting drive component 42 is a cylinder, which has the advantage of fast response. In other embodiments, the lifting drive component 42 can also be a linear motor, etc., which is not limited here.
[0059] Optionally, such as Figure 4As shown, the floating assembly 442 also includes a damping element 4421, which is disposed within the floating space 4411. One end of the elastic element abuts against one side of the damping element 4421, and the other side of the damping element 4421 is a third limiting part 44221. Through this arrangement, the compression speed of the second elastic element 443 can be further reduced, thereby reducing the impact force on the solar module 200 when the laminate 43 is pressed down.
[0060] In other embodiments, if the damping member 4421 is not provided, the second elastic member 443 can abut against the third limiting part 44221.
[0061] Optionally, such as Figure 3 As shown, the laminating chamber 41 has an opening facing the transport mechanism 20, and a lifting space 411 extends along a third direction (Z direction in the figure, which is perpendicular to both the X and Y directions). The laminating component 43 can slide within the lifting space 411 along this third direction. This design ensures that the laminating component 43 extends precisely along the third direction when pressed down, preventing skewness caused by excessive distance between the laminating component 43 and the output end of the lifting drive component 42 when it is fully depressed, thus ensuring accurate lamination positioning.
[0062] Optionally, such as Figure 1 and Figure 3 As shown, the solar module lamination device also includes a blower 50, which is installed in the lamination chamber 41 and located upstream of the laminator 43. The blower 50 is configured to blow air onto the solar module 200 to remove dust from its surface. Through this arrangement, impurities and dust are blown away from the surface of the solar module 200 between laminations, preventing dust from affecting its performance after encapsulation.
[0063] Optionally, such as Figure 3 As shown, the lamination chamber 41 has an air blowing pipe 413 and an air blowing groove 412 sequentially opened on the lower side of the air blowing component 50. The air blowing pipe 413 can increase the wind speed, and the air blowing groove 412 is adapted to the shape of the solar module 200.
[0064] Obviously, the above embodiments of this utility model are merely examples for clearly illustrating the present utility model, and are not intended to limit the implementation of the present utility model. Those skilled in the art can make various obvious changes, readjustments, and substitutions without departing from the protection scope of this utility model. It is neither necessary nor possible to exhaustively describe all embodiments here. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of this utility model should be included within the protection scope of the claims of this utility model.
Claims
1. A solar module lamination device, characterized in that, include: The frame (10) extends along the first direction; A transport mechanism (20) is installed on the frame (10), and the transport mechanism (20) is capable of transporting solar modules (200) along the first direction; The centering adjustment mechanism (30) includes two adjustment components (31). The two adjustment components (31) are symmetrically arranged on both sides of the frame (10) and form an adjustment channel (32). Each adjustment component (31) includes an adjustment element (311). The adjustment element (311) is floatingly connected to the corresponding side of the frame (10) and located on the upper side of the transport mechanism (20). Both sides of the solar panel (200) can respectively abut against the adjustment element (311). A laminating mechanism (40) is disposed on the frame (10) and located downstream of the centering adjustment mechanism (30), the laminating mechanism (40) being configured to press the solar panel (200) on the transport mechanism (20).
2. The solar module laminating apparatus according to claim 1, characterized in that, The adjusting member (311) includes: An adjustment section (3111) extends along the first direction and is located on the upper side of the transport mechanism (20), and two opposing adjustment sections (3111) form the adjustment channel (32); The frame (10) includes a through-hole (3112) and a first limiting part (3113). The through-hole (3112) extends along the second direction and passes through the frame (10). One end of the through-hole (3112) is connected to the adjusting part (3111), and the other end is connected to the first limiting part (3113). The first limiting part (3113) is located on the outside of the frame (10), and the first direction is perpendicular to the second direction. The adjustment assembly (31) further includes a first elastic element (312), one end of which is connected to the outside of the frame (10), and the other end is connected to the first limiting part (3113).
3. The solar module laminating apparatus according to claim 2, characterized in that, The frame (10) has an elongated hole (111) extending along the first direction on its side wall. The through-hole (3112) is disposed through the elongated hole (111). At least two through-holes (3112) are disposed at intervals along the first direction. The first limiting part (3113) and the first elastic member (312) are disposed in a one-to-one correspondence with the through-holes (3112).
4. The solar module laminating apparatus according to claim 2, characterized in that, The adjustment part (3111) is arranged in an arc shape at the entry end facing the adjustment channel (32).
5. The solar module laminating apparatus according to any one of claims 1-4, characterized in that, The transport mechanism (20) is a conveyor belt (21), and a follower (22) is protruding on the conveyor belt (21). The solar panel (200) is placed on the conveyor belt (21) and can abut against the follower (22).
6. The solar module lamination apparatus according to any one of claims 1-4, characterized in that, The lamination mechanism (40) includes: A laminating chamber (41) is installed on the frame (10) and located above the transport mechanism (20); A lifting drive (42) and a laminating component (43) are provided. The lifting drive (42) is installed in the laminating chamber (41), and the laminating component (43) is floatingly connected to the output end of the lifting drive (42).
7. The solar module laminating apparatus according to claim 6, characterized in that, The lamination mechanism (40) further includes a connecting component (44), the connecting component (44) comprising: A limiting member (441) is connected at one end to the output end of the lifting drive member (42). A floating space (4411) is formed inside the limiting member (441). The other end of the limiting member (441) is constructed as a second limiting part (4412). A through hole (4413) communicating with the floating space (4411) is opened on the second limiting part (4412). The cross-sectional dimension of the through hole (4413) is smaller than the cross-sectional dimension of the floating space (4411). A floating component (442) includes a floating element (4422), the floating element (4422) including a connected third limiting part (44221) and a connecting part (44222), the cross-sectional shape of the third limiting part (44221) is consistent with the cross-sectional shape of the floating space (4411) and is located within the floating space (4411), the cross-sectional shape of the connecting part (44222) is consistent with the cross-sectional shape of the perforation (4413) and is disposed through the perforation (4413), and one end of the connecting part (44222) opposite to the third limiting part (44221) is connected to the laminate (43); The second elastic element (443) abuts against the floating component (442) at one end and against the inner wall of the floating space (4411) at the other end.
8. The solar module laminating apparatus according to claim 7, characterized in that, The floating component (442) further includes a damping element (4421), which is disposed within the floating space (4411). One end of the second elastic element (443) abuts against one side of the damping element (4421), and the other side of the damping element (4421) is the third limiting part (44221).
9. The solar module laminating apparatus according to claim 6, characterized in that, The laminating chamber (41) has an opening and a lifting space (411) facing the transport mechanism (20). The lifting space (411) extends along a third direction, and the laminating member (43) can slide within the lifting space (411) along the third direction, which is perpendicular to the first direction.
10. The solar module laminating apparatus according to claim 6, characterized in that, It also includes a blower (50) mounted on the laminating chamber (41) and located upstream of the laminating member (43), the blower (50) being configured to blow air onto the solar module (200) to remove dust from the surface of the solar module (200).