CN112838134B - Copper indium gallium selenium thin film solar cell and preparation method thereof - Google Patents

Copper indium gallium selenium thin film solar cell and preparation method thereof Download PDF

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CN112838134B
CN112838134B CN202110098410.4A CN202110098410A CN112838134B CN 112838134 B CN112838134 B CN 112838134B CN 202110098410 A CN202110098410 A CN 202110098410A CN 112838134 B CN112838134 B CN 112838134B
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indium gallium
copper indium
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CN112838134A (en
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王正安
来华杭
郭峰
俞峰
周海龙
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Zhejiang Shangfang Electronic Equipment Co ltd
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/02Details
    • H01L31/0224Electrodes
    • H01L31/022408Electrodes for devices characterised by at least one potential jump barrier or surface barrier
    • H01L31/022425Electrodes for devices characterised by at least one potential jump barrier or surface barrier for solar cells
    • H01L31/022441Electrode arrangements specially adapted for back-contact solar cells
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/04Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
    • H01L31/042PV modules or arrays of single PV cells
    • H01L31/0445PV modules or arrays of single PV cells including thin film solar cells, e.g. single thin film a-Si, CIS or CdTe solar cells
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
    • H01L31/18Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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Abstract

The application discloses a copper indium gallium selenium thin film solar cell and a preparation method thereof, wherein the copper indium gallium selenium thin film solar cell comprises: the copper indium gallium selenide solar cell comprises a substrate, a molybdenum back electrode layer, a copper indium gallium selenide absorption layer, a buffer layer and a window layer which are sequentially arranged from bottom to top, wherein the molybdenum back electrode layer is positioned in the copper indium gallium selenide absorption layer, the thickness of the copper indium gallium selenide absorption layer is 2.3-3 mu m, the thickness of the molybdenum back electrode layer is 1.9-2.1 mu m, the molybdenum back electrode layer is provided with hollowed-out areas allowing light to pass through, the hollowed-out areas are regularly arranged, and the area of each hollowed-out area is 14-25 mu m 2 . The copper indium gallium selenide thin film solar cell provided by the application can absorb about 50% -70% of back light to generate electricity, and the photoelectric conversion efficiency is improved.

Description

Copper indium gallium selenium thin film solar cell and preparation method thereof
Technical Field
The application relates to the technical field of photovoltaics, in particular to a copper indium gallium diselenide thin film solar cell and a preparation method thereof.
Background
In the prior art, the structure of the copper indium gallium diselenide thin film solar cell is shown in fig. 1, and the main structure of the cell is as follows from bottom to top: a substrate 1, a silicon nitride barrier layer 2 (SiNx), a molybdenum back electrode layer 3 (Mo), a copper indium gallium selenium absorber layer 4 (CIGS), a cadmium sulfide buffer layer 5 (CdS), an intrinsic zinc oxide window layer 6 (i-ZnO) and an aluminum doped zinc oxide window layer 7 (AZO).
The functions of the layers are simply expressed as follows:
a) The substrate 1 mainly provides support for the battery device. Conventional substrates typically use float Glass, i.e., glass substrates (Glass) typically have a thickness of 2-5mm, corresponding devices typically are used in the building photovoltaic integration field, and specific flexible devices typically use stainless steel sheets as the substrate material, 0.1-0.5mm thick.
b) The silicon nitride barrier layer 2 is mainly used for blocking impurity ions (metal ions such as sodium, calcium, iron and the like) in the glass substrate from entering the battery device to influence the performance of the battery, and the stainless steel substrate uses chromium metal as the barrier layer, and the thickness of the silicon nitride barrier layer is 100-200nm.
c) The molybdenum back electrode layer 3 exists as a back electrode of the device and is positioned on one side of the P-type semiconductor material to provide a path for the directional movement of electrons, and the thickness of the molybdenum back electrode layer is about 300nm.
d) The copper indium gallium selenide absorption layer 4 is a light absorption material of the whole solar cell device, and after reaching the layer, light is absorbed by the layer and excited in the layer to generate photo-generated electron-hole pairs. The copper indium gallium selenide material is a P-type semiconductor material, and the thickness of the copper indium gallium selenide absorption layer is generally 1.5-2.5 mu m.
e) The cadmium sulfide buffer layer 5 is used as an N-type semiconductor material and forms a PN junction with a P-type copper indium gallium selenide material, photo-generated electron-hole pairs generated by light absorbed by the copper indium gallium selenide material are separated by a built-in electric field of PN in the PN junction region, a photo-generated potential difference is formed, and the thickness of the cadmium sulfide buffer layer is 30-70nm.
f) The intrinsic zinc oxide and the aluminum-doped zinc oxide together form a window layer. The window layer provides a path for light to enter the device on the one hand, and on the other hand, exists as a front electrode of the cell device, provides a path for electron flow of the solar cell, and has a thickness of typically 800-1200nm.
g) After a load is connected between the front electrode and the back electrode, under the action of the photo-generated potential difference, a current forms a passage between the two electrodes to generate photo-generated current for supplying power to an external load.
In the conventional copper indium gallium diselenide solar cell device shown in fig. 1, the molybdenum back electrode layer 3 is designed to be a complete molybdenum metal film layer, the device can only absorb the light entering the absorption layer from the front electrode (window layer) and generate a photovoltaic effect, and the light at the back of the device can be blocked by the molybdenum back electrode layer and cannot enter the absorption layer at all, so that the photoelectric conversion efficiency is affected.
Disclosure of Invention
Based on the structure, the copper indium gallium diselenide thin film solar cell structure provided by the application fully utilizes the front light and simultaneously utilizes most of the back light to perform photoelectric conversion, so that the photoelectric conversion efficiency of the solar cell is improved.
A copper indium gallium diselenide thin film solar cell comprising: the substrate, the molybdenum back electrode layer, the copper indium gallium selenide absorption layer, the buffer layer and the window layer are sequentially arranged from bottom to top;
the molybdenum back electrode layer is positioned in the copper indium gallium selenide absorption layer, the thickness of the copper indium gallium selenide absorption layer is 2.3-3 mu m, the thickness of the molybdenum back electrode layer is 1.9-2.1 mu m, the molybdenum back electrode layer is provided with hollowed-out areas allowing light to pass through, the hollowed-out areas are regularly arranged, and the area of each hollowed-out area is 14-25 mu m 2
The following provides several alternatives, but not as additional limitations to the above-described overall scheme, and only further additions or preferences, each of which may be individually combined for the above-described overall scheme, or may be combined among multiple alternatives, without technical or logical contradictions.
Optionally, the molybdenum back electrode layer includes a first surface and a second surface parallel to each other, the first surface is in contact with the substrate, and the second surface is in the copper indium gallium selenide absorption layer.
Optionally, the distance between the second surface and the buffer layer is 0.4-0.7 μm.
Optionally, each hollow area is rectangular, and each hollow area is arranged in a matrix.
Optionally, the distance between the nearest edges of two adjacent hollow areas is 0.3-0.5 μm.
Optionally, a barrier layer is further disposed between the substrate and the molybdenum back electrode layer, the first surface of the molybdenum back electrode layer is in contact with the barrier layer, and the second surface is in the copper indium gallium selenide absorption layer.
Optionally, the window layer includes: an intrinsic zinc oxide window layer in contact with the buffer layer, and an aluminum-doped zinc oxide window layer in contact with the intrinsic zinc oxide window layer.
Optionally, the thickness of the barrier layer is 100-200nm.
Optionally, the thickness of the intrinsic zinc oxide window layer is 20-50nm, and the thickness of the aluminum-doped zinc oxide window layer is 800-1000nm.
The application also provides a preparation method of the copper indium gallium selenide thin-film solar cell, the molybdenum back electrode layer, the copper indium gallium selenide absorption layer, the buffer layer and the window layer are sequentially prepared on a substrate, and the preparation process of the molybdenum back electrode layer comprises the following steps:
an initial film layer is obtained by magnetron sputtering;
and etching the initial film layer by using laser to obtain the molybdenum back electrode layer.
The copper indium gallium selenide thin film solar cell provided by the application can absorb about 50% -70% of back light to generate electricity, and the photoelectric conversion efficiency is improved.
Drawings
Fig. 1 is a block diagram of a copper indium gallium diselenide thin film solar cell in the prior art;
FIG. 2 is a block diagram of a CIGS thin film solar cell according to the present application;
fig. 3 is a schematic diagram of a molybdenum back electrode layer in a copper indium gallium diselenide thin film solar cell according to the present application.
In the figure: 1. a substrate; 2. a barrier layer; 3. a molybdenum back electrode layer; 4. a copper indium gallium selenium absorption layer; 5. a buffer layer; 6. an intrinsic zinc oxide window layer; 7. an aluminum-doped zinc oxide window layer; 8. and (5) a hollowed-out area.
Detailed Description
The following description of the embodiments of the present application will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present application, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the application without making any inventive effort, are intended to be within the scope of the application.
For a better description and illustration of embodiments of the application, reference should be made to one or more of the accompanying drawings, but the additional details or examples used to describe the drawings should not be construed as limiting the scope of any of the inventive, presently described embodiments or preferred modes of carrying out the application.
It will be understood that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. When an element is referred to as being "disposed on" another element, it can be directly on the other element or intervening elements may also be present.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein in the description of the application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application.
Referring to fig. 2 and 3, a copper indium gallium diselenide thin film solar cell includes: the substrate 1, the molybdenum back electrode layer 3, the copper indium gallium selenide absorption layer 4, the buffer layer 5 and the window layer which are sequentially arranged from bottom to top, wherein the molybdenum back electrode layer 3 is positioned in the copper indium gallium selenide absorption layer 4, the thickness d5 of the copper indium gallium selenide absorption layer 4 is 2.3-3 mu m, the thickness d3 of the molybdenum back electrode layer 3 is 1.9-2.1 mu m, the molybdenum back electrode layer 3 is provided with hollowed-out areas 8 allowing light to pass through, the hollowed-out areas 8 are a plurality of regularly arranged, and the area of each hollowed-out area 8 is 14-25 mu m 2
The thickness of the molybdenum back electrode layer 3 is increased more than that of a molybdenum back electrode of a conventional copper indium gallium selenide absorption layer 4, and the molybdenum back electrode layer 3 is completely embedded into the copper indium gallium selenide absorption layer 4, so that the contact area between the molybdenum back electrode layer 3 and the copper indium gallium selenide absorption layer 4 is increased on one hand, and the transmission performance of carriers is ensured; on the other hand, the migration length of the photo-generated carriers in the absorption layer is shortened, and the recombination probability of the photo-generated carriers in the absorption layer is reduced.
In the traditional copper indium gallium selenide thin film solar cell, the carrier collecting length of the molybdenum back electrode layer 3 is about 2-2.5 mu m, and in the application, the carrier collecting length of the molybdenum back electrode layer 3 is 0.5-2.1 mu m, which is more beneficial to the carrier collecting, reduces the carrier recombination possibility, improves the filling factor of the copper indium gallium selenide thin film solar cell, and further increases the photoelectric conversion efficiency of the cell.
The thicker molybdenum back electrode layer 3 is completely buried in the copper indium gallium selenide absorption layer 4, so that the path of diffuse reflection light entering the absorption layer is increased, the contact area with the copper indium gallium selenide absorption layer 4 material is ensured, and the collection performance of carriers and the conductivity of the material are ensured.
Referring to fig. 2, the hollowed-out area 8 of the molybdenum back electrode layer 3 with the hollowed-out area 8 provides a channel for diffuse reflection light on the back surface to enter the absorption layer, the area of the hollowed-out area 8 determines that the diffuse reflection light enters the absorption layer in a diffraction light mode, and the light entering the back surface is absorbed by the absorption layer and excites the photo-generated carrier pair as the light entering the front surface after entering the absorption layer, so that the overall light absorption capacity of the battery is finally improved, the short-circuit current of the battery is improved, and the final photoelectric conversion efficiency of the battery is increased.
As shown in fig. 2, the hollowed-out area 8 of the molybdenum back electrode layer 3 allows light to pass through from the back surface, and on the other hand, light loss from the front surface is caused, so that the shape, arrangement and area of the hollowed-out area 8 need to be reasonably optimized to balance advantages and disadvantages.
The molybdenum back electrode layer 3 comprises a first surface and a second surface parallel to each other, the first surface being in contact with the substrate 1, the second surface being in the copper indium gallium selenide absorbing layer 4. In one embodiment, as shown in fig. 2, a barrier layer 2 is further disposed between the substrate 1 and the molybdenum back electrode layer 3, and a first surface of the molybdenum back electrode layer 3 contacts the barrier layer 2, and a second surface is located in the copper indium gallium selenide absorption layer 4.
The distance between the second surface and the buffer layer 5 is 0.4-0.7 μm. In one embodiment, as shown in fig. 2, the distance d1 between the second surface and the buffer layer 5 is 0.5 μm.
Referring to fig. 2 and 3, each hollow area 8 is rectangular, and each hollow area 8 is arranged in a matrix.
In one embodiment, the hollow area 8 is square, and the side length d2 of the square is 0.4 μm.
The distance between the nearest edges of two adjacent hollow areas 8 is 0.3-0.5 mu m.
In one embodiment, the distance d4 between the nearest edges of two adjacent hollow areas 8 is 0.5 μm.
Referring to fig. 2, the window layer includes: an intrinsic zinc oxide window layer 6 in contact with the buffer layer 5, and an aluminum-doped zinc oxide window layer 7 in contact with the intrinsic zinc oxide window layer 6.
The thickness of the barrier layer 2 is 100-200nm. The thickness of the intrinsic zinc oxide window layer 6 is 20-50nm, and the thickness of the aluminum-doped zinc oxide window layer 7 is 800-1000nm.
The application provides a preparation method of a copper indium gallium selenide thin-film solar cell, which sequentially prepares a molybdenum back electrode layer 3, a copper indium gallium selenide absorption layer 4, a buffer layer 5 and a window layer on a substrate 1, wherein the preparation process of the molybdenum back electrode layer 3 comprises the following steps:
an initial film layer is obtained by magnetron sputtering;
and etching the initial film layer by utilizing laser to obtain the molybdenum back electrode layer 3.
The preparation method of the copper indium gallium diselenide thin film solar cell provided by the application specifically comprises the following steps:
(1) Substrate 1 cleaning (one-time cleaning): taking a glass substrate as an example, sequentially performing cleaning processes such as dust removal by a hairbrush, primary washing by deionized water, ultrasonic cleaning, secondary cleaning by deionized water, air knife drying, static electricity removal and the like on the glass substrate to obtain the glass substrate;
(2) Preparation of a barrier layer: the clean glass substrate enters a magnetron sputtering device to prepare the barrier layer 2 silicon nitride. The barrier layer 2 silicon nitride is prepared by using a high-purity silicon target reaction magnetron sputtering mode. The sputtering atmosphere is the mixed atmosphere of argon and nitrogen, the ratio of the nitrogen to the argon is about 0.8-1.0, the sputtering pressure is kept between 0.3 Pa and 0.8Pa, and the thickness of the silicon nitride film is 100-200nm.
(3) Molybdenum back electrode layer 3 preparation: the molybdenum electrode layer is prepared by adopting a magnetron sputtering mode, and the thickness of the film layer is about 1900-2100nm and is about 4-5 times of the thickness of the traditional molybdenum back electrode layer 3 during sputtering.
The molybdenum back electrode layer 3 was processed in accordance with the structure shown in fig. 3 using a laser apparatus to prepare a mesh structure shown in fig. 3. The width of the grid structure of the molybdenum electrode is about 300-500nm, the mesh size is about 4 mu m multiplied by 4 mu m, and P1 scribing is carried out while preparing the grid structure.
(4) And (3) secondary cleaning: and cleaning the substrate after laser scribing by using a cleaning machine, wherein the cleaning machine is mainly used for cleaning metal dust residues generated in the laser process.
(5) Sputtering a preformed layer of an absorber layer: and respectively sputtering a sodium-doped copper gallium layer (CuGa: na), a CuGa layer and an In metal layer on the substrate by using magnetron sputtering, wherein Cu/(in+Ga) of the film layer is approximately equal to 0.89-0.91, ga/(in+Ga) is approximately equal to 0.3, and the thickness of the whole film layer is approximately 800-1000nm.
(6) Selenizing and vulcanizing the prefabricated layer: and (3) carrying out selenizing treatment on the prefabricated layer in Se atmosphere, wherein the temperature is kept at 250-300 ℃ in the first stage, and annealing is carried out for 20-40 minutes. And in the second stage, se atmosphere in the furnace chamber is maintained, the temperature is quickly raised to 550-600 ℃, and annealing is performed for 20-40 minutes. Finally let in H 2 S gas, carrying out vulcanization treatment on the surface of the film layer at 550-600 ℃ for about 6-10 minutes, introducing argon gas to protect the film layer, and cooling. The thickness of the copper indium gallium diselenide absorbing layer 4 after the selenization and sulfidation processes is about 2.5 μm.
(7) And (3) rapidly (less than 30 minutes) carrying out chemical water area method deposition of the cadmium sulfide film on the substrate after cooling. Cadmium acetate, ammonium humate, thiourea and ammonia water with certain concentration are used to prepare a reaction solution, the cooled substrate is placed in the reaction solution, the temperature of the solution is kept at about 45-70 ℃, and the reaction time is about 7-15 minutes (different temperatures correspond to different reaction times). The thickness of the cadmium sulfide buffer layer 5 is about 30-60 nm. After the chemical reaction is finished, cleaning the surface of the film layer by using a cleaning machine, removing deposited large particles and residual chemical components, and finally drying and removing static electricity by using an air knife.
(8) Preparing an intrinsic zinc oxide layer by magnetron sputtering: the magnetron sputtering method is used for preparing the target material, the target material is undoped high-purity zinc oxide target material, the sputtering is carried out under the mixed atmosphere of argon and oxygen, the oxygen content is kept between 5 and 10 percent, and the sputtering air pressure is 0.8 to 1.5Pa. The thickness of the intrinsic zinc oxide film layer is about 20-50 nm.
(9) A mechanical needle was used for the P2 scribe process.
(10) Preparing an aluminum-doped zinc oxide layer by magnetron sputtering: the preparation method adopts a magnetron sputtering mode, and the target material is an aluminum-doped high-purity zinc oxide target material (98:2=ZnO: al 2 O 3 The sputtering is carried out under the mixed atmosphere of argon and oxygen, the oxygen content is kept between 0.2 and 0.5 percent, and the sputtering pressure is between 0.2 and 0.5Pa. The thickness of the aluminum-doped zinc oxide film layer is about 800-1000nm, the square resistance of the film layer is less than 10ohm/≡, and the average transmittance of visible light (380-780 nm) is more than 80%.
(11) A mechanical needle was used for the P3 scribe process.
(12) Testing and packaging the solar cell device.
The technical features of the above-described embodiments may be arbitrarily combined, and all possible combinations of the technical features in the above-described embodiments are not described for brevity of description, however, as long as there is no contradiction between the combinations of the technical features, they should be considered as the scope of the description.
The above examples illustrate only a few embodiments of the application, which are described in detail and are not to be construed as limiting the scope of the application. It should be noted that it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the spirit of the application, which are all within the scope of the application. Accordingly, the scope of protection of the present application is to be determined by the appended claims.

Claims (6)

1. A copper indium gallium diselenide thin film solar cell comprising: the substrate, the molybdenum back electrode layer, the copper indium gallium selenide absorption layer, the buffer layer and the window layer are sequentially arranged from bottom to top and are characterized in that,
the thickness of the copper indium gallium selenide absorbing layer and the molybdenum back electrode layer is uniform and continuously distributed;
the copper indium gallium selenide absorbing layers are continuously distributed, the molybdenum back electrode layer is located in the copper indium gallium selenide absorbing layers, the molybdenum back electrode layer and the copper indium gallium selenide absorbing layers form a layer with uniform thickness, the thickness of the copper indium gallium selenide absorbing layer is 2.3-3 mu m, the thickness of the molybdenum back electrode layer is 1.9-2.1 mu m, the molybdenum back electrode layer is provided with hollowed-out areas allowing light to pass through, the hollowed-out areas are regularly distributed, and the area of each hollowed-out area is 14-25 mu m 2 The method comprises the steps of carrying out a first treatment on the surface of the The distance between the nearest edges of two adjacent hollow areas is 0.3-0.5 mu m;
the molybdenum back electrode layer comprises a first surface and a second surface which are parallel to each other, a blocking layer is further arranged between the substrate and the molybdenum back electrode layer, the first surface of the molybdenum back electrode layer is in contact with the blocking layer, the second surface is positioned in the copper indium gallium selenide absorption layer, and the distance between the second surface and the buffer layer is 0.4-0.7 mu m.
2. The copper indium gallium diselenide thin film solar cell according to claim 1, wherein each hollowed-out area is rectangular, and each hollowed-out area is arranged in a matrix.
3. The copper indium gallium diselenide thin film solar cell of claim 1, wherein the window layer comprises: an intrinsic zinc oxide window layer in contact with the buffer layer, and an aluminum-doped zinc oxide window layer in contact with the intrinsic zinc oxide window layer.
4. The copper indium gallium diselenide thin film solar cell of claim 1, wherein the thickness of the barrier layer is 100-200nm.
5. A copper indium gallium diselenide thin film solar cell according to claim 3, wherein the intrinsic zinc oxide window layer has a thickness of 20-50nm and the aluminum doped zinc oxide window layer has a thickness of 800-1000nm.
6. A method for preparing the copper indium gallium selenide thin-film solar cell according to any one of claims 1 to 5, wherein the molybdenum back electrode layer, the copper indium gallium selenide absorption layer, the buffer layer and the window layer are sequentially prepared on a substrate, and the preparation process of the molybdenum back electrode layer comprises the following steps:
an initial film layer is obtained by magnetron sputtering;
and etching the initial film layer by using laser to obtain the molybdenum back electrode layer.
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