CN217426751U - Solar cell composite assembly and photovoltaic system - Google Patents

Abstract

The application is suitable for the technical field of solar cells and provides a solar cell composite assembly and a photovoltaic system. The solar cell composite component comprises the following components in sequence: the solar cell comprises a glass substrate, a thin film battery array, an insulating layer, a crystalline silicon battery array, a packaging adhesive film and packaging glass; the glass substrate is conductive glass, and the thin film battery array comprises a first contact layer, an absorption layer, a second contact layer and a conductive layer which are sequentially arranged on the conductive glass; the thin film battery array is provided with a first groove, a second groove and a third groove, the first groove is formed in the conductive glass and contains the first contact layer, the second groove penetrates through the second contact layer, the absorption layer and the first contact layer, the second groove contains the conductive layer, and the third groove penetrates through the conductive layer, the second contact layer, the absorption layer and the first contact layer. Therefore, the process difficulty and the material cost can be effectively reduced, the short-circuit current of the crystalline silicon cell array is effectively increased, and the photoelectric conversion efficiency of the solar cell composite component is further improved.

Description

Solar cell composite assembly and photovoltaic system

Technical Field

The application belongs to the technical field of solar cells, and particularly relates to a solar cell composite assembly and a photovoltaic system.

Background

Solar cell power generation is a sustainable clean energy source that can convert sunlight into electrical energy using the photovoltaic effect of semiconductor p-n junctions.

In the related art, two cells of the two-end tandem solar cell are in series connection, so the optical properties of the top and bottom cells need to be finely regulated to reach the highest current, and a proper tunneling layer needs to be searched and additionally prepared, so that the process difficulty is high. In the four-terminal laminated solar cell in the related technology, the top cell and the bottom cell are independently packaged, at least four layers of packaging adhesive films and packaging glass are required, metal electrodes are required to be used, and when the size of the module is expanded, the balancing cost of the module and a system is higher, and the power loss is larger.

Therefore, how to reduce the process difficulty and the material cost of the laminated battery assembly becomes a problem to be solved urgently.

SUMMERY OF THE UTILITY MODEL

The application provides a solar cell composite component and a photovoltaic system, and aims to solve the problems of how to reduce the process difficulty and the material cost of a laminated cell component.

The application provides a solar cell composite assembly, including range upon range of in proper order: the solar cell comprises a glass substrate, a thin film battery array, an insulating layer, a crystalline silicon battery array, a packaging adhesive film and packaging glass; the thin film battery array comprises a first contact layer, an absorption layer, a second contact layer and a conductive layer which are sequentially arranged on the conductive glass; the thin film battery array is provided with a first groove, a second groove and a third groove, the first groove is formed in the conductive glass and contains the first contact layer, the second groove penetrates through the second contact layer, the absorption layer and the first contact layer, the second groove contains the conductive layer, and the third groove penetrates through the conductive layer, the second contact layer, the absorption layer and the first contact layer.

Optionally, the conductive glass includes an insulating glass and a conductive film, the conductive film is disposed between the insulating glass and the first contact layer, and the first groove penetrates through the conductive film.

Optionally, the first contact layer includes a first dense contact layer, a first mesoporous contact layer, a first ferroelectric spacer insulating layer, and a first carbon electrode sequentially disposed on the conductive glass.

Optionally, the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, and the first contact end, the second contact end, the third contact end and the fourth contact end are respectively led out from the solar battery composite component.

Optionally, the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the polarities of the first contact end and the third contact end are the same, the polarities of the second contact end and the fourth contact end are the same, the first contact end and the third contact end are connected to form a first leading-out end, and the first leading-out end, the second contact end and the fourth contact end are respectively led out from the solar battery composite component.

Optionally, the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the polarities of the first contact end and the third contact end are the same, the polarities of the second contact end and the fourth contact end are the same, the voltages of the thin film battery array and the crystalline silicon battery array are matched, the first contact end and the third contact end are connected to form a first leading-out end, the second contact end and the fourth contact end are connected to form a second leading-out end, and the first leading-out end and the second leading-out end are respectively led out from the solar battery composite component.

Optionally, the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the polarities of the first contact end and the third contact end are the same, the polarities of the second contact end and the fourth contact end are the same, the currents of the thin film battery array and the crystalline silicon battery array are matched, the second contact end and the third contact end are connected, and the first contact end and the fourth contact end are respectively led out from the solar battery composite component.

Optionally, the thin film battery array comprises at least one of a ferrous silicon battery, a copper indium gallium selenide battery, a microcrystalline silicon battery, a nanocrystalline silicon battery, an indium phosphide battery, an amorphous silicon battery, a perovskite battery, a gallium arsenide battery, and a cadmium telluride battery.

The photovoltaic system comprises the solar cell composite component.

According to the solar cell composite assembly and the photovoltaic system, the crystalline silicon cell array is arranged on the thin film cell array to form the solar cell composite assembly, and only two layers of packaging glass and packaging adhesive films are needed. When two layers of glass are adopted for packaging, one piece of glass is used as a substrate to prepare the thin film battery array, so that the process difficulty and the material cost can be effectively reduced. Meanwhile, the thin film battery array and the crystalline silicon battery array are isolated by the insulating layer, so that tunneling junctions can be avoided, the short-circuit current of the crystalline silicon battery array can be effectively increased, and the photoelectric conversion efficiency of the solar battery composite assembly is further improved.

Drawings

Fig. 1 is a schematic structural diagram of a solar cell composite module according to an embodiment of the present application;

fig. 2 is a schematic structural diagram of a solar cell composite module according to an embodiment of the present application;

fig. 3 is a schematic structural diagram of a solar cell composite module according to an embodiment of the present application;

fig. 4 is a schematic structural diagram of a solar cell composite module according to an embodiment of the present application.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more apparent, the present application is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.

Example one

Referring to fig. 1, a solar cell composite assembly 100 according to an embodiment of the present disclosure includes: the solar cell comprises a glass substrate 101, a thin film battery array 10, an insulating layer 20, a crystalline silicon battery array 30, a packaging adhesive film 102 and packaging glass 103.

In the solar cell composite module 100 according to the embodiment of the present application, the crystalline silicon cell array 30 is disposed on the thin film cell array 10 to form the solar cell composite module 100, and only two layers of encapsulation glass and an encapsulation adhesive film 103 are required. When two layers of glass are adopted for packaging, one piece of glass is used as a substrate to prepare the thin film battery array 10, so that the process difficulty and the material cost can be effectively reduced. Meanwhile, the insulating layer 20 is used for isolating the thin film battery array 10 and the crystalline silicon battery array 30, so that tunneling junctions can be avoided, the short-circuit current of the crystalline silicon battery array 30 can be effectively increased, and the photoelectric conversion efficiency of the solar battery composite assembly 100 can be further improved.

Specifically, in the present embodiment, the thin film battery array 10 is a top battery array, and the crystalline silicon battery array 30 is a bottom battery array. It is understood that in other embodiments, the thin film battery array 10 may be a bottom battery array and the crystalline silicon battery array 30 may be a top battery array.

Alternatively, the glass substrate 101 is a large-sized glass substrate. The length of the large-size glass substrate is 0.5m-3 m. For example, 0.5m, 0.6m, 0.8m, 1m, 1.5m, 2m, 2.5m, 2.8m, 3 m. The width of the large-size glass substrate is 0.5m-2.5 m. For example, 0.5m, 0.6m, 0.8m, 1m, 1.5m, 2m, 2.5 m. Therefore, a large-size thin film battery array can be manufactured, and the efficiency is higher.

Alternatively, the glass substrate 101 may include a transparent glass substrate. Specifically, the transmittance of the glass substrate 101 may be greater than 90%. For example 90%, 91%, 92%, 93%, 94%, 95%, 96%, 97%, 98%, 99%, 100%. Thus, the glass substrate has high light transmittance, so that more sunlight can enter the solar cell composite assembly 100, which is beneficial to improving the photoelectric conversion efficiency.

Specifically, the glass substrate 101 includes one or more of float glass, patterned glass, tempered glass, antireflection glass, PET, PEN, PEI, PMMA. Thus, the glass substrate 101 is provided in various forms, which are convenient to select according to actual production conditions.

Alternatively, the thin film battery array 10 may be a battery string formed by connecting a plurality of thin film batteries in series, or may be a battery array formed by connecting a plurality of thin film batteries in series in parallel.

Specifically, the plurality of thin-film cells in the thin-film cell array 10 may be arranged in a grid. Further, the thin film battery array 10 includes a plurality of rows of thin film batteries parallel to each other and a plurality of columns of thin film batteries parallel to each other, where each row of thin film batteries is perpendicular to each column of thin film batteries. It is understood that in other embodiments, the thin film battery array 10 includes a plurality of rows of thin film batteries parallel to each other and a plurality of columns of thin film batteries parallel to each other, each row of thin film batteries being at an acute angle to each column of thin film batteries; the thin film battery array 10 comprises a plurality of rows of thin film batteries and a plurality of columns of thin film batteries, wherein the thin film batteries in partial rows are parallel to each other; the thin film battery array 10 includes a plurality of rows of thin film batteries and a plurality of columns of thin film batteries, some of the columns of thin film batteries being parallel to each other. The specific arrangement of the plurality of thin-film cells in the thin-film cell array 10 is not limited herein.

Optionally, the thin film battery comprises a ferrous silicon battery, a copper indium gallium selenide battery, a microcrystalline silicon battery, a nanocrystalline silicon battery, an indium phosphide battery, an amorphous silicon battery, a perovskite battery, a gallium arsenide battery, and a cadmium telluride battery. It is understood that the plurality of thin film batteries in the thin film battery array 10 may be the same kind of thin film battery or different kinds of thin film batteries. In other words, the thin-film battery array 10 includes at least one of a ferrous-silicon battery, a copper indium gallium selenium battery, a microcrystalline-silicon battery, a nanocrystalline-silicon battery, an indium phosphide battery, an amorphous-silicon battery, a perovskite battery, a gallium arsenide battery, and a cadmium telluride battery.

Note that, for convenience of explanation, the thin film batteries in the thin film battery array 10 are all perovskite batteries, but this does not represent a limitation to the thin film battery array 10.

Optionally, the insulating layer 20 is a transparent insulating layer 20. Therefore, the insulating layer 20 can transmit sunlight, so that the sunlight is prevented from being shielded by the insulating layer 20, and the photoelectric conversion efficiency of the double-sided light receiving solar cell composite component 100 is improved. It will be appreciated that sunlight incident from a side of one cell array facing away from the opposite cell array, after being transmitted through the insulating layer 20, may be incident on the opposite cell array and thus be utilized by the opposite cell array.

Specifically, the light transmittance of the insulating layer 20 ranges over more than 80%. For example, 80%, 82%, 85%, 87%, 89%, 90%, 92%, 95%, 97%, 99%, 100%.

Thus, the light transmittance of the insulating layer 20 is in a proper range, and the phenomenon that sunlight is difficult to transmit due to the fact that the light transmittance is small is avoided, so that the phenomenon that the photoelectric conversion efficiency is low due to shielding of the insulating layer 20 is avoided.

Optionally, the insulating layer 20 includes at least one of glass, EVA glue, silicone, POE.

Alternatively, the insulating layer 20 may be continuously provided on the thin film battery array 10, as shown in fig. 1, and the insulating layer 20 may be provided on the entire surface of the thin film battery array 10. It is understood that in other embodiments, the insulating layer 20 may be intermittently disposed on the thin film battery array 10, in other words, the insulating layer 20 is disposed on the contact surface between the thin film battery array 10 and the crystalline silicon battery array 30, and the insulating layer 20 is not disposed on the non-contact surface between the thin film battery array 10 and the crystalline silicon battery array 30. The specific arrangement of the insulating layer 20 is not limited as long as the thin film cell array 10 and the crystalline silicon cell array 30 can be insulated.

Alternatively, the crystalline silicon battery array 30 may be a battery string formed by connecting a plurality of crystalline silicon batteries in series, or may be a battery array formed by connecting a plurality of crystalline silicon batteries in series in parallel.

It is to be understood that the specific arrangement of the plurality of crystalline silicon cells in the crystalline silicon cell array 30 can refer to the foregoing, and for the sake of avoiding easy description, the detailed description is omitted here.

Alternatively, the crystalline silicon Cell includes an Interdigitated Back Contact (IBC), an HJT Cell (Heterojunction Cell) with Intrinsic Thin film, a TOPCon Cell (Tunnel Oxide Passivated Contact Cell), an MWT Cell (Metallization wrap-through) or a percc Cell (Passivated Emitter back solar Cell). It is understood that the plurality of crystalline silicon cells in the crystalline silicon cell array 30 may be the same type of crystalline silicon cell, or may be different types of crystalline silicon cells.

It should be noted that, for convenience of explanation, the silicon-crystal cells in the silicon-crystal cell array 30 are all interdigital back contact cells, but this does not represent a limitation to the silicon-crystal cell array 30. It is understood that when the crystalline silicon cell array 30 includes double-sided contact cells, the structure and wiring connection of the crystalline silicon cells in the drawings can be modified adaptively, and the relevant drawings of the double-sided contact cells are not shown to avoid redundancy.

In this embodiment, the interdigital electrode of the interdigital back contact cell array is located on a side of the interdigital back contact cell, which faces away from the thin film cell array. It is understood that in other embodiments, the interdigital electrodes of the interdigital back contact cell array can also be located on the side of the interdigital back contact cell facing the thin film cell array.

Alternatively, the encapsulant film 102 includes, but is not limited to, Ethylene Vinyl Acetate Copolymer (EVA), polyethylene octene co-elastomer (POE).

Alternatively, the packaging adhesive film 102 may be continuously disposed on the crystalline silicon cell array 30. Further, the whole surface of the crystalline silicon battery array 30 may be provided with the packaging adhesive film 102. Thus, the stability of the package is ensured. In other embodiments, the packaging adhesive film 102 may be intermittently disposed on the crystalline silicon battery array 30. Therefore, the material can be further saved, and the cost can be reduced.

Please note that, the related explanation and description of the package glass 103 can refer to the parts related to the glass substrate 101, and are not described herein again to avoid redundancy.

Alternatively, the encapsulation glass 103 may be provided on the whole surface of the crystalline silicon cell array 30. Thus, moisture and dust are prevented from entering from the gap, and the reliability of the solar cell composite assembly 100 can be improved.

Alternatively, the light trapping structure can be fabricated on the glass substrate 101. In other words, the glass substrate 101 is provided with a light trapping structure. Therefore, the loss of sunlight can be reduced, and the photoelectric conversion efficiency can be improved. Further, the light trapping structure may be prepared on a side of the glass substrate 101 facing away from the thin film cell array 10. In other words, the side of the glass substrate 101 facing away from the thin film cell array 10 is provided with a light trapping structure. In this way, the light trapping structure is prevented from interfering with the preparation of the thin film cell array 10.

Alternatively, the number of thin film cells in the thin film cell array 10 may be the same as or different from the number of crystalline silicon cells in the crystalline silicon cell array 30. Alternatively, the thin film cells in the thin film cell array 10 and the crystalline silicon cells in the crystalline silicon cell array 30 may be disposed in a thickness direction, or may be disposed in a staggered manner. Specifically, the offset arrangement means that the center line of the thin film battery is offset from the center line of the crystalline silicon battery in the thickness direction. Alternatively, the projection of the thin film cell in the thin film cell array 10 on the packaging glass 103 may be completely overlapped, partially overlapped or completely staggered with the projection of the crystalline silicon cell in the crystalline silicon cell array 30 on the packaging glass 103; the projection of the thin film battery on the packaging glass 103 can cover and exceed the projection of the crystalline silicon battery on the packaging glass 103; the projection of the crystalline silicon cell on the encapsulation glass 103 also covers and exceeds the projection of the thin film cell on the encapsulation glass 103. The positional relationship between the thin film cell and the crystalline silicon cell is not limited herein.

Referring to fig. 1, optionally, the glass substrate 101 is conductive glass, and the thin film battery array 10 includes a first contact layer 12, an absorption layer 13, a second contact layer 14, and a conductive layer 15, which are sequentially disposed on the conductive glass; the thin film battery array 10 is provided with a first groove 191, a second groove 192 and a third groove 193, the first groove 191 is provided in the conductive glass and accommodates the first contact layer 12, the second groove 192 penetrates through the second contact layer 14, the absorption layer 13 and the first contact layer 12, the second groove 192 accommodates the conductive layer 15, and the third groove 193 penetrates through the conductive layer 15, the second contact layer 14, the absorption layer 13 and the first contact layer 12.

In this way, the thin film battery array 10 is formed by dividing the large-area thin film battery by the grooves. Moreover, the scribing is carried out first and then the deposition is carried out, so that the process is simple and the efficiency is high. It can be understood that the battery array formed by connecting the series thin film batteries in series and parallel can be scribed according to actual conditions, and details are not described herein.

Specifically, the first groove may be made by scribing with a laser. Therefore, the scribing precision and speed are high, the process is simple, and the efficiency is improved. Further, scribing may be performed using a laser having a wavelength of 1064 nm. Similarly, the second groove and the third groove may be scribed by a laser.

It is understood that the recess may also be formed by mask blanket redeposition; chemical etching can also be utilized to form the grooves; mechanical engraving may also be used to form the grooves. The specific manner of forming the grooves is not limited herein.

Specifically, one of the first contact layer 12 and the second contact layer 14 is an electron transport layer, and the other is a hole transport layer. In this embodiment, the first contact layer 12 is an electron transport layer, and the second contact layer 14 is a hole transport layer. It is understood that in other embodiments, the first contact layer 12 can be a hole transport layer and the second contact layer 14 can be an electron transport layer.

Specifically, the absorption layer 13 includes one or more layers of a silicon ferrocyanide layer, a copper indium gallium selenide layer, a microcrystalline silicon layer, a nanocrystalline silicon layer, an indium phosphide layer, an amorphous silicon layer, a perovskite layer, a gallium arsenide layer, and a cadmium telluride layer. In this way, various forms of the absorbent layer 13 are provided, which can be selected during the production process according to the actual situation.

Specifically, the Conductive layer 15 is a Transparent Conductive Oxide (TCO). Therefore, the TC O can effectively collect the current of the thin film battery array 10, and the normal work of the thin film battery array 10 is ensured. Moreover, the TCO has high permeability and can reflect light, so that the loss of sunlight can be reduced. Thus, the photoelectric conversion efficiency is advantageously improved.

It is understood that in other embodiments, the transparent conductive film may be a metal film system, a compound film system, a polymer film system, a composite film system, or the like, other than the oxide film system. Such as PEDOT (polymer of EDOT (3, 4-ethylenedioxythiophene monomer), metal grids, carbon nanorod conductive Films (CNB Films), Silver Nanowires (SNW), Graphene (Graphene), and the like. The specific form of the transparent conductive film is not limited herein.

Further, TCOs include, but are not limited to, Indium Tin Oxide (ITO), fluorine-doped Tin Oxide (FTO), Aluminum-doped Zinc Oxide (AZO), cerium-doped Zinc Oxide (CZO). The specific type of TCO is not limited herein.

Specifically, the conductive glass may be cleaned. Thus, impurities are prevented from affecting subsequent preparation, and the quality of the thin film battery array 10 can be improved.

Furthermore, the surface of the conductive glass can be wiped by dipping ethanol in the dust-free paper; conducting ultrasonic cleaning on the conductive glass; and drying the conductive glass. Therefore, the cleaning effect is better, and the subsequent preparation is convenient.

Alternatively, the glass substrate 101 is insulating glass, the thin-film battery array 10 includes a conductive film 11 provided between the insulating glass and the first contact layer 12, and the first groove 191 penetrates the conductive film 11.

In this manner, in the case where the glass substrate 101 is an insulating glass, by forming a conductive glass by preparing the conductive film 11 on the insulating glass, it is possible to adapt to more production scenarios.

Please note that, the related explanation and description of the conductive film 11 can refer to the parts related to the conductive layer 15, and are not described herein again for avoiding redundancy.

Optionally, the first contact layer 12 includes a first dense contact layer, a first mesoporous contact layer, a first ferroelectric spacer insulating layer, and a first carbon electrode sequentially disposed on the conductive glass. Thus, the first contact layer 12 is prepared on the scribed conductive glass, the open-circuit voltage and the photoelectric conversion efficiency of the thin film cell array 10 can be improved, and the power of the assembly can be improved.

Specifically, a ferroelectric polarization field directed from the first contact layer 12 toward the absorption layer 13 may be applied to the first ferroelectric spacer insulating layer with a strength greater than the ferroelectric coercive field of the first ferroelectric spacer insulating layer.

Note that "directed from the first contact layer 12 to the absorption layer 13" means a polarization direction directed from the positive electrode to the negative electrode.

It can be understood that, by preparing the first ferroelectric spacer insulating layer by using the inorganic ferroelectric and applying the ferroelectric polarization field to the first ferroelectric spacer insulating layer, ferroelectric domains inside the first ferroelectric spacer insulating layer are aligned in an oriented manner, so that an oriented polarization electric field is formed inside the first ferroelectric spacer insulating layer, and the perovskite is field-passivated by the ferroelectric polarization to enhance the perovskite built-in field. The split of quasi-Fermi energy levels of electrons and holes in the pin junction of the perovskite is aggravated by the enhanced built-in field of the perovskite material, so that the open-circuit voltage of the battery is further improved. Moreover, the enhanced built-in field of the perovskite material causes the energy band of a heterojunction interface formed by the perovskite absorption layer and the compact electron transport layer to be bent, so that the separation and extraction of photon-generated carriers at the heterojunction interface are promoted. Thus, the open circuit voltage and the photoelectric conversion efficiency of the perovskite cell are improved.

Specifically, the first intimate contact layer is a dense electron transport layer. Preferably TiO ₂ As a compact electron transport layer material. In other words, the first coherent contact layer is dense TiO ₂ And (3) a layer.

Specifically, the first mesoporous contact layer is a mesoporous electron transport layer. Preferably TiO ₂ As the mesoporous electron transport layer material. In other words, the first mesoporous contact layer is mesoporous TiO ₂ And (3) a layer.

Specifically, the inorganic ferroelectric includes PZT. PZT powder can be ground to obtain PZT nanocrystalline; adding PZT nanocrystalline into deionized water and stirring to obtain PZT hydrosol; coating the PZT hydrosol on the first mesoporous contact layer, and annealing the PZT hydrosol coated on the first mesoporous contact layer to prepare the first ferroelectric interval insulating layer.

Specifically, a carbon paste may be printed on the first ferroelectric spacer insulating layer by screen printing, dried, sintered, held at a temperature, and naturally cooled to room temperature, thereby forming the first carbon electrode.

Specifically, a positive ferroelectric polarization field perpendicular to the surface of the thin film battery, which is directed from the glass substrate 101 to the absorption layer 13, may be applied to the first ferroelectric spacer insulating layer using a constant current power supply, and the applied external electric field is larger than the ferroelectric coercive field of PZT. Therefore, the first ferroelectric interval insulating layer is polarized, the method is simple, the speed is high, and the equipment cost is low.

It is understood that in other embodiments, PFM application may also be employed.

In particular, MA + -free organic-inorganic hybrid perovskite material FA is preferred _0.91 Cs _0.09 PbI ₃ Absorption as perovskite solar cellsAnd (c) a layer 13.

Specifically, the compact electron transport layer is made of PCBM and TiO ₂ 、ZnO、SnO ₂ At least one of H-PDI and F-PDI.

Specifically, the mesoporous electron transport layer is made of PCBM and TiO ₂ 、ZnO、SnO ₂ At least one of H-PDI and F-PDI.

Specifically, the perovskite absorption layer 13 is made of an organic-inorganic hybrid perovskite having a general formula ABX ₃ Type A is Cs ⁺ 、CH(NH ₂ ) ₂ ⁺ 、CH ₃ NH ₃ ⁺ 、C(NH2) ₃ ⁺ B is Pb ²⁺ 、Sn ²⁺ At least one of (1), X is Br ^- 、I ^- 、Cl ^- One or more of (a). Thus, the perovskite light absorption layer 13 has a good light absorption effect, and is advantageous for improving the photoelectric conversion efficiency.

Optionally, the second contact layer 14 includes a second dense contact layer, a second mesoporous contact layer, a second ferroelectric spacer insulating layer, and a second carbon electrode sequentially disposed on the absorption layer 13.

In addition, a ferroelectric polarization field directed from the absorption layer 13 toward the second contact layer 14 may be applied to the second ferroelectric spacer insulating layer with a strength greater than the ferroelectric coercive field of the second ferroelectric spacer insulating layer.

Note that "directed from the absorption layer 13 to the second contact layer 14" means a polarization direction directed from the positive electrode to the negative electrode. In this embodiment, the second contact layer 14 is a hole transport layer.

For the explanation and explanation of this part, reference is made to the foregoing description, and redundant description is omitted here.

Specifically, the hole transport layer includes one or more of a NiOx film, a PEDOT PSS film, a Spiro-oMeTad film, a CuSCN film, and a PTAA film.

In addition, the second contact layer can be prepared by magnetron sputtering, spray coating, blade coating, spin coating, screen printing, and the like.

Referring to fig. 1, optionally, the thin film battery array 10 is provided with a first contact terminal 110 and a second contact terminal 120, the crystalline silicon battery array 30 is provided with a third contact terminal 310 and a fourth contact terminal 320, and the first contact terminal 110, the second contact terminal 120, the third contact terminal 310 and the fourth contact terminal 320 are respectively led out of the solar battery composite component 100.

Therefore, the first contact end 110, the second contact end 120, the third contact end 310 and the fourth contact end 320 are led out independently to form the solar cell composite assembly 100 with four series-connected ends, voltage matching and current matching are not needed, the process is simple, and the efficiency is high.

Specifically, one of the first contact end 110 and the second contact end 120 is a positive contact end, and the other is a negative contact end. One of the third contact end 310 and the fourth contact end 320 is a positive contact end, and the other is a negative contact end.

In the example of fig. 1, the first contact end 110 and the third contact end 310 are negative contact ends, and the second contact end 120 and the fourth contact end 320 are positive contact ends. It is understood that in other examples, the first contact end 110 and the third contact end 310 may be positive contact ends, and the second contact end 120 and the fourth contact end 320 may be negative contact ends.

Referring to fig. 2, optionally, the thin film battery array 10 is provided with a first contact end 110 and a second contact end 120, the crystalline silicon battery array 30 is provided with a third contact end 310 and a fourth contact end 320, the polarities of the first contact end 110 and the third contact end 310 are the same, the polarities of the second contact end 120 and the fourth contact end 320 are the same, the first contact end 110 and the third contact end 310 are connected to form a first lead-out end, and the first lead-out end, the second contact end 120 and the fourth contact end 320 are led out from the solar battery assembly 100 respectively.

Therefore, the first leading-out end, the second contact end 120 and the fourth contact end 320 are independently led out to form the solar cell composite component 100 with three ends connected in series, voltage matching and current matching are not needed, the process is simple, and the efficiency is high.

Specifically, one of the first contact end 110 and the second contact end 120 is a positive contact end, and the other is a negative contact end. One of the third contact end 310 and the fourth contact end 320 is a positive contact end, and the other is a negative contact end.

In the example of fig. 2, the first contact end 110 and the third contact end 310 are negative contact ends, and the second contact end 120 and the fourth contact end 320 are positive contact ends. It is understood that in other examples, the first contact end 110 and the third contact end 310 may be positive contact ends, and the second contact end 120 and the fourth contact end 320 may be negative contact ends.

In the example of fig. 2, the negative first contact end 110 is connected to the negative third contact end 310, which forms a first terminal that is also the negative contact end.

Referring to fig. 3, optionally, the thin film battery array 10 is provided with a first contact terminal 110 and a second contact terminal 120, the crystalline silicon battery array 30 is provided with a third contact terminal 310 and a fourth contact terminal 320, the polarities of the first contact terminal 110 and the third contact terminal 310 are the same, the polarities of the second contact terminal 120 and the fourth contact terminal 320 are the same, the voltages of the thin film battery array 10 and the crystalline silicon battery array 30 are matched, the first contact terminal 110 and the third contact terminal 310 are connected to form a first lead-out terminal, the second contact terminal 120 and the fourth contact terminal 320 are connected to form a second lead-out terminal, and the first lead-out terminal and the second lead-out terminal are led out of the solar cell composite assembly 100 respectively.

In this way, the first terminal formed by connecting the first contact terminal 110 and the third contact terminal 310, the second terminal formed by connecting the second contact terminal 120 and the fourth contact terminal 320 are independently led out to form the solar cell composite assembly 100 with two parallel ends, and the electrical performance of the solar cell composite assembly 100 is better due to the voltage matching.

Specifically, one of the first contact end 110 and the second contact end 120 is a positive contact end, and the other is a negative contact end. One of the third contact end 310 and the fourth contact end 320 is a positive contact end, and the other is a negative contact end.

In the example of fig. 3, the first contact end 110 and the third contact end 310 are positive contact ends, and the second contact end 120 and the fourth contact end 320 are negative contact ends. It is understood that in other examples, the first contact end 110 and the third contact end 310 may be negative contact ends, and the second contact end 120 and the fourth contact end 320 may be positive contact ends.

In the example of fig. 3, the first contact end 110 of the positive electrode is connected to the third contact end 310 of the positive electrode, and the first lead-out terminal is also formed as the positive contact end. The second contact end 120 of the negative electrode is connected to the fourth contact end 320 of the negative electrode, and the formed second lead-out end is also the negative contact end.

Specifically, the voltage matching may be performed by controlling the number of thin film cells in the thin film cell array 10 and the number of crystalline silicon cells in the crystalline silicon cell array 30. Further, the number of thin film batteries in the thin film battery array 10 can be controlled by controlling the number of scribe lines of the thin film battery array 10.

Referring to fig. 4, alternatively, the thin film battery array 10 is provided with a first contact terminal 110 and a second contact terminal 120, the crystalline silicon battery array 30 is provided with a third contact terminal 310 and a fourth contact terminal 320, the polarities of the first contact terminal 110 and the third contact terminal 310 are the same, the polarities of the second contact terminal 120 and the fourth contact terminal 320 are the same, the currents of the thin film battery array 10 and the crystalline silicon battery array 30 are matched, the second contact terminal 120 and the third contact terminal 310 are connected, and the first contact terminal 110 and the fourth contact terminal 320 are led out of the solar cell composite assembly 100 respectively.

In this way, the second contact end 120 is connected to the third contact end 310, and the first contact end 110 and the fourth contact end 320 are led out independently, so as to form the solar cell composite assembly 100 with two ends connected in series, which makes the electrical performance of the solar cell composite assembly 100 better due to the current matching.

Specifically, one of the first contact end 110 and the second contact end 120 is a positive contact end, and the other is a negative contact end. One of the third contact end 310 and the fourth contact end 320 is a positive contact end, and the other is a negative contact end.

In the example of fig. 4, the first contact end 110 and the third contact end 310 are negative contact ends, and the second contact end 120 and the fourth contact end 320 are positive contact ends. It is understood that in other examples, the first contact end 110 and the third contact end 310 may be positive contact ends, and the second contact end 120 and the fourth contact end 320 may be negative contact ends.

Specifically, the current matching may be performed by controlling the size of the thin film cell in the thin film cell array 10 and the size of the crystalline silicon cell in the crystalline silicon cell array 30.

Further, the area of the thin film battery in the thin film battery array 10 can be controlled by controlling the number of scribe lines of the thin film battery array 10; the area of the thin-film cells in the thin-film cell array 10 can be controlled by controlling the total area of the thin-film cell array 10.

Further, the current of the crystalline silicon battery can be controlled by controlling the area of the crystalline silicon battery; the current of the crystalline silicon cell can be controlled by controlling the thickness of the crystalline silicon cell.

For further explanation and explanation of this embodiment, reference may be made to other parts of the present document, and further explanation is omitted here to avoid redundancy.

Example two

The photovoltaic system of the embodiment of the present application includes the solar cell composite assembly 100 of any one of the embodiments.

According to the photovoltaic system provided by the embodiment of the application, the crystalline silicon battery array 30 is arranged on the thin film battery array 10 to form the solar battery composite assembly 100, and only two layers of packaging glass and a packaging adhesive film 103 are needed. When two layers of glass are adopted for packaging, one piece of glass is used as a substrate to prepare the thin film battery array 10, so that the process difficulty and the material cost can be effectively reduced. Meanwhile, the insulating layer 20 is used for isolating the thin film battery array 10 and the crystalline silicon battery array 30, so that tunneling junctions can be avoided, the short-circuit current of the crystalline silicon battery array 30 can be effectively increased, and the photoelectric conversion efficiency of the solar battery composite assembly 100 can be further improved.

In this embodiment, the photovoltaic system can be applied to photovoltaic power stations, such as ground power stations, roof power stations, water surface power stations, etc., and can also be applied to devices or apparatuses that generate electricity by using solar energy, such as user solar power sources, solar street lamps, solar cars, solar buildings, etc. Of course, it is understood that the application scenario of the photovoltaic system is not limited thereto, that is, the photovoltaic system can be applied in all fields requiring solar energy for power generation. Taking a photovoltaic power generation system network as an example, a photovoltaic system may include a photovoltaic array, a combiner box and an inverter, the photovoltaic array may be an array combination of a plurality of battery modules, for example, the plurality of battery modules may constitute a plurality of photovoltaic arrays, the photovoltaic array is connected to the combiner box, the combiner box may combine currents generated by the photovoltaic array, and the combined currents are converted into alternating currents required by a utility grid through the inverter and then are connected to the utility grid to realize solar power supply.

For further explanation and description of this embodiment, reference may be made to other parts herein, especially to the first embodiment and the second embodiment, and further description is omitted here for the sake of avoiding redundancy.

The present invention is not intended to be limited to the particular embodiments shown and described, but is to be accorded the widest scope consistent with the principles and novel features herein disclosed.

Claims (9)

1. A solar cell composite assembly, comprising, stacked in sequence: the solar cell comprises a glass substrate, a thin film battery array, an insulating layer, a crystalline silicon battery array, a packaging adhesive film and packaging glass; the glass substrate is made of conductive glass, and the thin film battery array comprises a first contact layer, an absorption layer, a second contact layer and a conductive layer which are sequentially arranged on the conductive glass; the thin film battery array is provided with a first groove, a second groove and a third groove, the first groove is formed in the conductive glass and contains the first contact layer, the second groove penetrates through the second contact layer, the absorption layer and the first contact layer, the second groove contains the conductive layer, and the third groove penetrates through the conductive layer, the second contact layer, the absorption layer and the first contact layer.

2. The solar cell composite assembly according to claim 1, wherein the conductive glass comprises an insulating glass and a conductive film, the conductive film is disposed between the insulating glass and the first contact layer, and the first groove penetrates through the conductive film.

3. The solar cell composite assembly according to claim 1, wherein the first contact layer comprises a first dense contact layer, a first mesoporous contact layer, a first ferroelectric spacer insulating layer, and a first carbon electrode sequentially disposed on the conductive glass.

4. The solar cell composite assembly according to claim 1, wherein the thin film cell array is provided with a first contact end and a second contact end, the crystalline silicon cell array is provided with a third contact end and a fourth contact end, and the first contact end, the second contact end, the third contact end and the fourth contact end are respectively led out of the solar cell composite assembly.

5. The solar cell composite assembly according to claim 1, wherein the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the polarities of the first contact end and the third contact end are the same, the polarities of the second contact end and the fourth contact end are the same, the first contact end and the third contact end are connected to form a first leading-out end, and the first leading-out end, the second contact end and the fourth contact end are respectively led out of the solar cell composite assembly.

6. The solar cell composite assembly according to claim 1, wherein the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the polarities of the first contact end and the third contact end are the same, the polarities of the second contact end and the fourth contact end are the same, the voltages of the thin film battery array and the crystalline silicon battery array are matched, the first contact end and the third contact end are connected to form a first leading-out end, the second contact end and the fourth contact end are connected to form a second leading-out end, and the first leading-out end and the second leading-out end are respectively led out from the solar cell composite assembly.

7. The solar cell composite assembly according to claim 1, wherein the thin film battery array is provided with a first contact end and a second contact end, the crystalline silicon battery array is provided with a third contact end and a fourth contact end, the first contact end and the third contact end have the same polarity, the second contact end and the fourth contact end have the same polarity, the thin film battery array and the crystalline silicon battery array are current matched, the second contact end and the third contact end are connected, and the first contact end and the fourth contact end are respectively led out of the solar cell composite assembly.

8. The solar cell composite assembly of claim 1, wherein the thin film cell array comprises at least one of a ferrous-based silicon cell, a copper indium gallium selenide cell, a microcrystalline silicon cell, a nanocrystalline silicon cell, an indium phosphide cell, an amorphous silicon cell, a perovskite cell, a gallium arsenide cell, and a cadmium telluride cell.

9. A photovoltaic system comprising a solar cell composite assembly according to any one of claims 1 to 8.

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