WO2018159799A1 - 太陽電池及び太陽電池の製造方法 - Google Patents
太陽電池及び太陽電池の製造方法 Download PDFInfo
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- WO2018159799A1 WO2018159799A1 PCT/JP2018/007957 JP2018007957W WO2018159799A1 WO 2018159799 A1 WO2018159799 A1 WO 2018159799A1 JP 2018007957 W JP2018007957 W JP 2018007957W WO 2018159799 A1 WO2018159799 A1 WO 2018159799A1
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- Prior art keywords
- solar cell
- photoelectric conversion
- electrode
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- conversion layer
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- H10K77/10—Substrates, e.g. flexible substrates
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- H01L31/02—Details
- H01L31/0224—Electrodes
- H01L31/022408—Electrodes for devices characterised by at least one potential jump barrier or surface barrier
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- H01L31/036—Semiconductor 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 characterised by their semiconductor bodies characterised by their crystalline structure or particular orientation of the crystalline planes
- H01L31/0392—Semiconductor 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 characterised by their semiconductor bodies characterised by their crystalline structure or particular orientation of the crystalline planes including thin films deposited on metallic or insulating substrates ; characterised by specific substrate materials or substrate features or by the presence of intermediate layers, e.g. barrier layers, on the substrate
- H01L31/03926—Semiconductor 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 characterised by their semiconductor bodies characterised by their crystalline structure or particular orientation of the crystalline planes including thin films deposited on metallic or insulating substrates ; characterised by specific substrate materials or substrate features or by the presence of intermediate layers, e.g. barrier layers, on the substrate comprising a flexible substrate
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- H01L31/18—Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
- H01L31/1884—Manufacture of transparent electrodes, e.g. TCO, ITO
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- H10K71/20—Changing the shape of the active layer in the devices, e.g. patterning
- H10K71/211—Changing the shape of the active layer in the devices, e.g. patterning by selective transformation of an existing layer
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- H10K85/50—Organic perovskites; Hybrid organic-inorganic perovskites [HOIP], e.g. CH3NH3PbI3
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- H10K30/50—Photovoltaic [PV] devices
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/549—Organic PV cells
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Definitions
- the present invention relates to a solar cell excellent in photoelectric conversion efficiency in which cutting processing (for example, mechanical patterning) at the time of manufacture is favorably performed, and a method for manufacturing the solar cell.
- the present invention also relates to a solar cell with low series resistance and high photoelectric conversion efficiency.
- a solar cell As a solar cell, a laminate in which an N-type semiconductor layer and a P-type semiconductor layer are arranged between opposing electrodes has been actively developed, and inorganic semiconductors such as silicon are mainly used as the N-type and P-type semiconductors. It is used.
- inorganic solar cells are expensive to manufacture and difficult to increase in size, and have a problem in that the range of use is limited. Therefore, in recent years, a perovskite solar cell using an organic / inorganic perovskite compound having a perovskite structure using lead, tin or the like as a central metal for a photoelectric conversion layer has attracted attention (for example, Patent Document 1, Non-Patent Document 1). .
- Perovskite solar cells can be expected to have high photoelectric conversion efficiency and can be manufactured by a printing method, so that manufacturing costs can be greatly reduced.
- a photoelectric conversion layer having a function of generating current when irradiated with light on a flexible substrate It is manufactured by laminating a plurality of layers such as a thin film.
- a solar cell sealing sheet is laminated
- Patent Document 2 describes a semiconductor device substrate including a sheet-like aluminum base material, and an organic thin film solar cell including the semiconductor device substrate.
- a first object of the present invention is to provide a solar cell excellent in photoelectric conversion efficiency, in which cutting (for example, mechanical patterning) at the time of manufacture is performed, and a method for manufacturing the solar cell.
- a second object of the present invention is to provide a solar cell with low series resistance and high photoelectric conversion efficiency.
- the present invention is a solar cell having an electrode, a transparent electrode, and a photoelectric conversion layer disposed between the electrode and the transparent electrode on a flexible substrate, and further, the flexible substrate and the And a hard film disposed between the electrode and at least one element selected from the group consisting of titanium, zirconium, aluminum, silicon, magnesium, vanadium, chromium, molybdenum, tantalum, and tungsten.
- a solar cell containing a nitride, carbide or boride also referred to as the first invention of the present specification).
- the present invention also relates to a solar cell having a cathode, an electron transport layer, a photoelectric conversion layer, and an anode in this order, wherein the photoelectric conversion layer has a general formula RMX 3 (where R is an organic molecule, M Is a metal atom, X is a halogen atom or a chalcogen atom), and the cathode is a solar cell containing a metal having a smaller ionization tendency than titanium (in this specification, the second Also referred to as the present invention).
- R is an organic molecule
- X is a halogen atom or a chalcogen atom
- the cathode is a solar cell containing a metal having a smaller ionization tendency than titanium (in this specification, the second Also referred to as the present invention).
- the present invention is described in detail below.
- the electrode When manufacturing a solar cell having an electrode, a transparent electrode, and a photoelectric conversion layer disposed between the electrode and the transparent electrode on a flexible substrate, the electrode is generally formed on the flexible substrate.
- the formed electrode is partially cut by a physical method such as mechanical patterning using a cutting tool.
- the load applied to the cutting tool is applied to the cutting edge of the cutting tool, and the portion of the electrode hitting the edge is cut and peeled off.
- the present inventors hit the cutting edge of the cutting tool against the flexible base located under the electrode, and the cutting of the cutting edge into the flexible base and the dent of the flexible base occur. We found a new problem of product defects.
- the cutting depth can be controlled by changing the load applied to the cutting tool, the load may not be stable and vary in mass production. It was difficult to sufficiently suppress the occurrence.
- a photoelectric conversion layer is then formed on the cut electrode, the formed photoelectric conversion layer is further partially cut, and the transparent electrode is further formed on the cut photoelectric conversion layer. The transparent electrode thus formed is further partially cut.
- the inventors examined a solar cell having an electrode, a transparent electrode, and a photoelectric conversion layer disposed between the electrode and the transparent electrode on a flexible substrate.
- the present inventors further provide a specific hard film between the flexible base material and the electrode, so that the cutting edge bites into the flexible base material and the dent of the flexible base material is generated. It was found that cutting (for example, mechanical patterning) can be performed satisfactorily while suppressing, and a solar cell excellent in photoelectric conversion efficiency can be obtained. Thus, the first present invention has been completed.
- the solar cell of 1st this invention has an electrode, a transparent electrode, and the photoelectric converting layer arrange
- the “layer” means not only a layer having a clear boundary but also a layer having a concentration gradient in which contained elements gradually change.
- the elemental analysis of the layer can be performed, for example, by performing FE-TEM / EDS line analysis measurement of the cross section of the solar cell and confirming the element distribution of the specific element.
- a layer means not only a flat thin film-like layer but also a layer that can form a complicated and complicated structure together with other layers.
- the said flexible base material is not specifically limited, For example, what has a resin film, metal foil, thin plate glass, etc. which consist of a polyimide and a polyester-type heat resistant polymer is mentioned. Of these, metal foil is preferred. By using the metal foil, costs can be reduced as compared with the case of using a heat-resistant polymer, and high-temperature treatment can be performed. That is, even when thermal annealing (heat treatment) is performed at a temperature of 80 ° C. or higher for the purpose of imparting light resistance (resistance to photodegradation) when forming a photoelectric conversion layer containing an organic / inorganic perovskite compound, generation of distortion is minimized. And high photoelectric conversion efficiency can be obtained.
- thermal annealing heat treatment
- light resistance resistance to photodegradation
- the said metal foil is not specifically limited, For example, metal foil which consists of metals, such as aluminum, titanium, copper, gold
- metal foil which consists of metals, such as aluminum, titanium, copper, gold
- the flexible substrate may further have an insulating layer formed on the metal foil. That is, the flexible substrate may have a metal foil and an insulating layer formed on the metal foil.
- the insulating layer is not particularly limited, and examples thereof include an inorganic insulating layer made of aluminum oxide, silicon oxide, zinc oxide, etc., and an organic insulating layer made of epoxy resin, polyimide, or the like.
- the said metal foil is an aluminum foil, it is preferable that the said insulating layer is an aluminum oxide film.
- the aluminum oxide film as the insulating layer, it is possible to suppress the phenomenon that the photoelectric conversion layer containing the organic / inorganic perovskite compound is discolored and corroded over time due to contact with the aluminum foil. it can.
- the photoelectric conversion layer reacts with aluminum to cause discoloration, and the phenomenon that the above corrosion occurs is that the photoelectric conversion layer contains an organic-inorganic perovskite compound.
- the present inventors have found as a problem peculiar to perovskite solar cells.
- the thickness of the aluminum oxide film is not particularly limited, but a preferable lower limit is 0.1 ⁇ m, a preferable upper limit is 20 ⁇ m, a more preferable lower limit is 0.5 ⁇ m, and a more preferable upper limit is 10 ⁇ m.
- a preferable lower limit is 0.1 ⁇ m
- a preferable upper limit is 20 ⁇ m
- a more preferable lower limit is 0.5 ⁇ m
- a more preferable upper limit is 10 ⁇ m.
- the heat treatment when the heat treatment is performed during the formation of the photoelectric conversion layer containing the organic / inorganic perovskite compound, cracks are generated in the aluminum oxide film and / or the layer formed thereon due to a difference in thermal expansion coefficient from the aluminum foil. Can be suppressed.
- the thickness of the aluminum oxide film can be measured, for example, by observing a cross section of the flexible substrate with an electron microscope (for example, S-4800, manufactured by HITACHI, etc.) and analyzing the contrast of the obtained photograph. it can.
- the thickness ratio of the aluminum oxide film is not particularly limited, but a preferable lower limit with respect to 100% of the thickness of the flexible substrate is 0.1%, a preferable upper limit is 15%, and a more preferable lower limit is 0.5%, more preferable.
- the upper limit is 5%.
- Increasing the thickness of the aluminum oxide film may suppress the occurrence of cutting edge biting into the aluminum foil and the depression of the aluminum foil, thereby suppressing the occurrence of product defects. Is increased, it is difficult to suppress the occurrence of such product defects for the following reasons. That is, since the aluminum oxide film has a lower hardness than a hard film described later, it is necessary to increase the thickness greatly in order to suppress the biting of the blade edge into the aluminum foil and the generation of the dent in the aluminum foil. . On the other hand, when the thickness is greatly increased, a problem that cracks are likely to occur in the aluminum oxide film occurs.
- the aluminum oxide film generally has a Vickers hardness of about 300 HV.
- the method for forming the aluminum oxide film is not particularly limited.
- the method for anodizing the aluminum foil, the method for applying an aluminum alkoxide to the surface of the aluminum foil, and the surface of the aluminum foil by heat treatment examples thereof include a method of forming a natural oxide film.
- the method of anodizing to the said aluminum foil is preferable. That is, the aluminum oxide film is preferably an anodized film.
- the thickness of the aluminum oxide film can be adjusted by changing the treatment concentration, treatment temperature, current density, treatment time, etc. in the anodization.
- the said processing time is not specifically limited, From a viewpoint of the ease of preparation of the said flexible base material, a preferable minimum is 5 minutes, a preferable upper limit is 120 minutes, and a more preferable upper limit is 60 minutes.
- the thickness of the said flexible base material is not specifically limited, A preferable minimum is 5 micrometers and a preferable upper limit is 500 micrometers.
- a preferable minimum is 5 micrometers and a preferable upper limit is 500 micrometers.
- the thickness of the flexible substrate is 5 ⁇ m or more, a solar cell having sufficient mechanical strength and excellent handleability can be obtained.
- the thickness of the flexible substrate is 500 ⁇ m or less, a solar cell having excellent flexibility can be obtained.
- the minimum with more preferable thickness of the said flexible base material is 10 micrometers, and a more preferable upper limit is 100 micrometers.
- the thickness of the flexible substrate includes the thickness of the entire flexible substrate including the metal foil and the insulating layer. Means.
- the electrode is disposed on the insulating layer side of the flexible substrate.
- Either the electrode or the transparent electrode may be a cathode or an anode.
- the material of the electrode and the transparent electrode include FTO (fluorine-doped tin oxide), sodium, sodium-potassium alloy, lithium, magnesium, aluminum, magnesium-silver mixture, magnesium-indium mixture, aluminum-lithium alloy, Al / Examples thereof include an Al 2 O 3 mixture, an Al / LiF mixture, and a metal such as gold.
- conductive transparent materials such as CuI, ITO (indium tin oxide), SnO 2 , AZO (aluminum zinc oxide), IZO (indium zinc oxide), GZO (gallium zinc oxide), conductive transparent polymers, etc. Is mentioned. These materials may be used alone or in combination of two or more.
- the photoelectric conversion layer contains an organic / inorganic perovskite compound represented by the general formula R-MX 3 (where R is an organic molecule, M is a metal atom, and X is a halogen atom or a chalcogen atom). preferable.
- R-MX 3 organic / inorganic perovskite compound represented by the general formula R-MX 3 (where R is an organic molecule, M is a metal atom, and X is a halogen atom or a chalcogen atom.
- the R is an organic molecule, and is preferably represented by C 1 N m H n (l, m, and n are all positive integers). Specifically, R is, for example, methylamine, ethylamine, propylamine, butylamine, pentylamine, hexylamine, dimethylamine, diethylamine, dipropylamine, dibutylamine, dipentylamine, dihexylamine, trimethylamine, triethylamine, tripropyl.
- Examples of the ion for example, such as ammonium (CH 3 NH 3) is.
- ammonium CH 3 NH 3
- methylamine, ethylamine, propylamine, propylcarboxyamine, butylcarboxyamine, pentylcarboxyamine, formamidinium, guanidine and their ions are preferred, and methylamine, ethylamine, pentylcarboxyamine, formamidinium, guanidine and These ions are more preferred.
- methylamine, formamidinium, and these ions are more preferable because high photoelectric conversion efficiency can be obtained.
- M is a metal atom, for example, lead, tin, zinc, titanium, antimony, bismuth, nickel, iron, cobalt, silver, copper, gallium, germanium, magnesium, calcium, indium, aluminum, manganese, chromium, molybdenum, Europium etc. are mentioned.
- lead or tin is preferable from the viewpoint of overlapping of electron orbits.
- These metal atoms may be used independently and 2 or more types may be used together.
- X is a halogen atom or a chalcogen atom, and examples thereof include chlorine, bromine, iodine, sulfur, and selenium. These halogen atoms or chalcogen atoms may be used alone or in combination of two or more. Among these, the halogen atom is preferable because the organic / inorganic perovskite compound becomes soluble in an organic solvent and can be applied to an inexpensive printing method by containing halogen in the structure. Furthermore, iodine is more preferable because the energy band gap of the organic-inorganic perovskite compound becomes narrow.
- the organic / inorganic perovskite compound preferably has a cubic structure in which a metal atom M is disposed at the body center, an organic molecule R is disposed at each vertex, and a halogen atom or a chalcogen atom X is disposed at the face center.
- FIG. 2 shows an example of a crystal structure of an organic-inorganic perovskite compound having a cubic structure in which a metal atom M is disposed in the body center, an organic molecule R is disposed at each vertex, and a halogen atom or a chalcogen atom X is disposed in the face center. It is a schematic diagram.
- the organic / inorganic perovskite compound is preferably a crystalline semiconductor.
- the crystalline semiconductor means a semiconductor capable of measuring the X-ray scattering intensity distribution and detecting a scattering peak. If the organic / inorganic perovskite compound is a crystalline semiconductor, the mobility of electrons in the organic / inorganic perovskite compound is increased, and the photoelectric conversion efficiency of the solar cell is improved. If the organic / inorganic perovskite compound is a crystalline semiconductor, it is easy to suppress a decrease in photoelectric conversion efficiency (photodegradation) caused by continuing to irradiate the solar cell with light, particularly a photodegradation due to a decrease in short-circuit current.
- the degree of crystallinity can also be evaluated as an index of crystallization.
- the degree of crystallinity is determined by separating the crystalline-derived scattering peak detected by the X-ray scattering intensity distribution measurement and the halo derived from the amorphous part by fitting, obtaining the respective intensity integrals, Can be obtained by calculating the ratio.
- a preferable lower limit of the crystallinity of the organic-inorganic perovskite compound is 30%. If the crystallinity is 30% or more, the mobility of electrons in the organic / inorganic perovskite compound is increased, and the photoelectric conversion efficiency of the solar cell is improved.
- the crystallinity When the crystallinity is 30% or more, it is easy to suppress the deterioration of photoelectric conversion efficiency (photodegradation) caused by continuously irradiating the solar cell with light, particularly the photodegradation due to the decrease of short circuit current.
- a more preferred lower limit of the crystallinity is 50%, and a more preferred lower limit is 70%.
- Examples of the method for increasing the crystallinity of the organic / inorganic perovskite compound include thermal annealing (heat treatment), irradiation with intense light such as laser, and plasma irradiation.
- the crystallite diameter can also be evaluated as another crystallization index.
- the crystallite diameter can be calculated by the holder-Wagner method from the half width of the scattering peak derived from the crystal detected by the X-ray scattering intensity distribution measurement.
- the crystallite diameter of the organic / inorganic perovskite compound is 5 nm or more, a decrease in photoelectric conversion efficiency (photodegradation) caused by continuing to irradiate light to the solar cell, particularly a photodegradation due to a decrease in short-circuit current is suppressed. .
- the mobility of electrons in the organic / inorganic perovskite compound is increased, and the photoelectric conversion efficiency of the solar cell is improved.
- a more preferred lower limit of the crystallite diameter is 10 nm, and a more preferred lower limit is 20 nm.
- the photoelectric conversion layer may further contain an organic semiconductor or an inorganic semiconductor in addition to the organic / inorganic perovskite compound as long as the effects of the present invention are not impaired.
- the organic semiconductor or inorganic semiconductor here may serve as a hole transport layer or an electron transport layer.
- the organic semiconductor include compounds having a thiophene skeleton such as poly (3-alkylthiophene).
- a conductive polymer having a polyparaphenylene vinylene skeleton, a polyvinyl carbazole skeleton, a polyaniline skeleton, a polyacetylene skeleton, or the like can be given.
- compounds having a porphyrin skeleton such as a phthalocyanine skeleton, a naphthalocyanine skeleton, a pentacene skeleton, or a benzoporphyrin skeleton, a spirobifluorene skeleton, etc.
- carbon-containing materials such as carbon nanotubes, graphene, and fullerene that may be surface-modified Also mentioned.
- the inorganic semiconductor examples include titanium oxide, zinc oxide, indium oxide, tin oxide, gallium oxide, tin sulfide, indium sulfide, zinc sulfide, CuSCN, Cu 2 O, CuI, MoO 3 , V 2 O 5 , WO 3 , MoS 2, MoSe 2, Cu 2 S , and the like.
- the photoelectric conversion layer includes the organic-inorganic perovskite compound and the organic semiconductor or the inorganic semiconductor
- the photoelectric conversion layer is a laminated body in which a thin-film organic semiconductor or an inorganic semiconductor portion and a thin-film organic-inorganic perovskite compound portion are stacked.
- a composite film in which an organic semiconductor or inorganic semiconductor part and an organic / inorganic perovskite compound part are combined may be used.
- a laminated body is preferable in that the production method is simple, and a composite film is preferable in that the charge separation efficiency in the organic semiconductor or the inorganic semiconductor can be improved.
- the preferable lower limit of the thickness of the thin-film organic / inorganic perovskite compound site is 5 nm, and the preferable upper limit is 5000 nm. If the thickness is 5 nm or more, light can be sufficiently absorbed, and the photoelectric conversion efficiency is increased. If the said thickness is 5000 nm or less, since it can suppress that the area
- the more preferable lower limit of the thickness is 10 nm, the more preferable upper limit is 1000 nm, the still more preferable lower limit is 20 nm, and the still more preferable upper limit is 500 nm.
- a preferable lower limit of the thickness of the composite film is 30 nm, and a preferable upper limit is 3000 nm. If the thickness is 30 nm or more, light can be sufficiently absorbed, and the photoelectric conversion efficiency is increased. If the said thickness is 3000 nm or less, since it becomes easy to reach
- the more preferable lower limit of the thickness is 40 nm, the more preferable upper limit is 2000 nm, the still more preferable lower limit is 50 nm, and the still more preferable upper limit is 1000 nm.
- the photoelectric conversion layer is preferably subjected to thermal annealing (heat treatment) after the photoelectric conversion layer is formed.
- thermal annealing heat treatment
- the degree of crystallinity of the organic-inorganic perovskite compound in the photoelectric conversion layer can be sufficiently increased, and the decrease in photoelectric conversion efficiency (photodegradation) due to continued irradiation with light is further increased. Can be suppressed.
- thermal annealing heat treatment
- distortion occurs during annealing due to the difference in thermal expansion coefficient between the resin film and the photoelectric conversion layer, etc. As a result, it may be difficult to achieve high photoelectric conversion efficiency.
- the metal foil even if thermal annealing (heat treatment) is performed, generation of distortion can be minimized and high photoelectric conversion efficiency can be obtained.
- the temperature for heating the photoelectric conversion layer is not particularly limited, but is preferably 100 ° C. or higher and lower than 250 ° C.
- the heating temperature is 100 ° C. or higher, the crystallinity of the organic / inorganic perovskite compound can be sufficiently increased. If the said heating temperature is less than 250 degreeC, it can heat-process, without thermally degrading the said organic-inorganic perovskite compound.
- a more preferable heating temperature is 120 ° C. or higher and 200 ° C. or lower.
- the heating time is not particularly limited, but is preferably 3 minutes or longer and 2 hours or shorter.
- the heating time is 3 minutes or longer, the crystallinity of the organic-inorganic perovskite compound can be sufficiently increased. If the heating time is within 2 hours, the organic inorganic perovskite compound can be heat-treated without causing thermal degradation.
- These heating operations are preferably performed in a vacuum or under an inert gas, and the dew point temperature is preferably 10 ° C or lower, more preferably 7.5 ° C or lower, and further preferably 5 ° C or lower.
- the method for forming the photoelectric conversion layer is not particularly limited, and examples thereof include a vacuum deposition method, a sputtering method, a gas phase reaction method (CVD), an electrochemical deposition method, and a printing method.
- the solar cell which can exhibit high photoelectric conversion efficiency can be simply formed in a large area by employ
- the printing method include a spin coating method and a casting method, and examples of a method using the printing method include a roll-to-roll method.
- the solar cell of the first aspect of the present invention further has a hard film disposed between the flexible base material and the electrode.
- the hard film includes a nitride, carbide, or boride containing at least one element selected from the group consisting of titanium, zirconium, aluminum, silicon, magnesium, vanadium, chromium, molybdenum, tantalum, and tungsten.
- FIG. 1 is a cross-sectional view schematically showing an example of the manufacturing process of the solar cell of the first invention.
- the hard film 3 is formed on the flexible base material having the metal foil 1 and the insulating layer 2 formed on the metal foil 1.
- An electrode 4 is formed on the hard film 3 (FIG. 1A). Then, the formed electrode 4 is partly cut by mechanical patterning using the cutting tool 5, whereby the portion of the electrode 4 that is in contact with the cutting edge is cut, peeled off, and the groove 41 is formed. (FIG. 1B).
- cutting is performed while suppressing the biting of the cutting edge into the flexible base material having the metal foil 1 and the insulating layer 2 formed on the metal foil 1 and the occurrence of the dent of the flexible base material.
- Processing for example, mechanical patterning
- a solar cell excellent in photoelectric conversion efficiency can be obtained.
- the hard film includes a nitride, carbide, or boride containing at least one element selected from the group consisting of titanium, zirconium, aluminum, silicon, magnesium, vanadium, chromium, molybdenum, tantalum, and tungsten. These may be used independently and 2 or more types may be used together. Of these, titanium nitride, titanium carbide, titanium boride, and molybdenum boride are preferred because the hardness is high and a hard film can be easily produced by a film forming apparatus used in the process of manufacturing a solar cell. Titanium nitride, titanium carbide, Titanium boride is more preferable, and titanium nitride is particularly preferable.
- the above-mentioned hard film has a preferred lower limit of Vickers hardness (HV) of 500 HV, and a preferred upper limit of 3500 HV.
- HV Vickers hardness
- the hard film can sufficiently suppress the cutting edge from being bitten into the flexible base material and the dent of the flexible base material. If the Vickers hardness is 3500 HV or less, the occurrence of cracks in the hard film can be suppressed.
- the more preferable lower limit of the Vickers hardness is 700 HV, and the more preferable upper limit is 2500 HV.
- the Vickers hardness (HV) of the hard film is determined, for example, from the obtained load-mutation curve by using a nanoindenter G200 (manufactured by Keysight Technologies) and pressing an indenter against the hard film formed on the glass substrate. It can be obtained by calculating.
- the thickness of the said hard film is not specifically limited, A preferable minimum is 30 nm and a preferable upper limit is 5000 nm. If the thickness of the hard film is 30 nm or more, the hard film can sufficiently suppress the cutting edge from being bitten into the flexible base material and the dent of the flexible base material. When the thickness of the hard film is 5000 nm or less, it takes no time to form the hard film, and the productivity of the solar cell is improved. A more preferable lower limit of the thickness of the hard film is 50 nm, and a more preferable upper limit is 1000 nm.
- the thickness of the hard film can be measured, for example, by a step shape measuring device P-16 + (manufactured by KLA Tencor).
- the method for forming the hard film is not particularly limited, and vacuum dry film forming methods such as sputtering, ion plating, vapor deposition, and CVD are preferable. Of these, sputtering is preferable.
- a TiN thin film can be formed by using Ti as a magnetron sputtering target and using Ar and N 2 as process gases.
- the solar cell of 1st this invention may have an electron carrying layer between the side used as the cathode of the said electrode and the said transparent electrode, and the said photoelectric converting layer.
- the material of the electron transport layer is not particularly limited.
- N-type conductive polymer N-type low molecular organic semiconductor, N-type metal oxide, N-type metal sulfide, alkali metal halide, alkali metal, surface activity Agents and the like.
- examples thereof include compounds and fluoro group-containing phthalocyanines. Examples thereof include titanium oxide, zinc oxide, indium oxide, tin oxide, gallium oxide, tin sulfide, indium sulfide, and zinc sulfide.
- the electron transport layer may consist of only a thin film electron transport layer (buffer layer), but preferably includes a porous electron transport layer.
- a thin film electron transport layer buffer layer
- the photoelectric conversion layer is a composite film in which an organic semiconductor or an inorganic semiconductor part and an organic / inorganic perovskite compound part are combined, a more complex composite film (a more complicated and complicated structure) is obtained.
- the composite film is formed on the porous electron transport layer.
- the preferable lower limit of the thickness of the electron transport layer is 1 nm, and the preferable upper limit is 2000 nm. If the thickness is 1 nm or more, holes can be sufficiently blocked. If the said thickness is 2000 nm or less, it will become difficult to become resistance at the time of electron transport, and photoelectric conversion efficiency will become high.
- the more preferable lower limit of the thickness of the electron transport layer is 3 nm, the more preferable upper limit is 1000 nm, the still more preferable lower limit is 5 nm, and the still more preferable upper limit is 500 nm.
- the solar cell of 1st this invention may have a hole transport layer between the said photoelectric converting layer and the side used as the anode among the said electrodes and the said transparent electrodes.
- the material for the hole transport layer is not particularly limited, and examples thereof include a P-type conductive polymer, a P-type low molecular organic semiconductor, a P-type metal oxide, a P-type metal sulfide, and a surfactant. Specific examples include compounds having a thiophene skeleton such as poly (3-alkylthiophene).
- conductive polymers having a triphenylamine skeleton, a polyparaphenylene vinylene skeleton, a polyvinyl carbazole skeleton, a polyaniline skeleton, a polyacetylene skeleton, and the like can be given.
- compounds having a porphyrin skeleton such as a phthalocyanine skeleton, a naphthalocyanine skeleton, a pentacene skeleton, and a benzoporphyrin skeleton, a spirobifluorene skeleton, and the like can be given.
- molybdenum oxide, vanadium oxide, tungsten oxide, nickel oxide, copper oxide, tin oxide, molybdenum sulfide, tungsten sulfide, copper sulfide, tin sulfide, etc. fluoro group-containing phosphonic acid, carbonyl group-containing phosphonic acid, CuSCN, CuI And carbon-containing materials such as carbon nanotubes, graphene and the like.
- a part of the hole transport layer may be immersed in the photoelectric conversion layer, or may be disposed in a thin film shape on the photoelectric conversion layer.
- the thickness when the hole transport layer is in the form of a thin film has a preferred lower limit of 1 nm and a preferred upper limit of 2000 nm. If the thickness is 1 nm or more, electrons can be sufficiently blocked. If the said thickness is 2000 nm or less, it will become difficult to become resistance at the time of hole transport, and a photoelectric conversion efficiency will become high.
- the more preferable lower limit of the thickness is 3 nm, the more preferable upper limit is 1000 nm, the still more preferable lower limit is 5 nm, and the still more preferable upper limit is 500 nm.
- the solar cell of the first aspect of the present invention may be configured as described above, but a plurality of grooves are formed by patterning the electrode, the photoelectric conversion layer, and the transparent electrode, respectively. It is preferable to be divided into solar cells. It is preferable that adjacent solar cells are electrically connected to the plurality of solar cells.
- the solar cell according to the first aspect of the present invention includes the electrode, the transparent electrode, and the photoelectric conversion layer disposed between the electrode and the transparent electrode on the flexible substrate as described above. Furthermore, the laminated body which has the said hard film arrange
- the material of the barrier layer is not particularly limited as long as it has a barrier property, and examples thereof include a thermosetting resin, a thermoplastic resin, and an inorganic material.
- thermosetting resin or thermoplastic resin examples include epoxy resin, acrylic resin, silicone resin, phenol resin, melamine resin, urea resin, and the like.
- thermosetting resin or thermoplastic resin examples include epoxy resin, acrylic resin, silicone resin, phenol resin, melamine resin, urea resin, and the like.
- butyl rubber, polyester, polyurethane, polyethylene, polypropylene, polyvinyl chloride, polystyrene, polyvinyl alcohol, polyvinyl acetate, ABS resin, polybutadiene, polyamide, polycarbonate, polyimide, polyisobutylene, and the like can be given.
- the barrier layer (resin layer) has a preferable lower limit of 100 nm and a preferable upper limit of 100,000 nm.
- a more preferable lower limit of the thickness is 500 nm, a more preferable upper limit is 50000 nm, a still more preferable lower limit is 1000 nm, and a still more preferable upper limit is 20000 nm.
- the inorganic material examples include Si, Al, Zn, Sn, In, Ti, Mg, Zr, Ni, Ta, W, Cu, or an oxide, nitride, or oxynitride of an alloy containing two or more of these. .
- oxides, nitrides, or oxynitrides of metal elements including both metal elements of Zn and Sn are preferable.
- the barrier layer (inorganic layer) has a preferable lower limit of 30 nm and a preferable upper limit of 3000 nm.
- the inorganic layer can have a sufficient water vapor barrier property, and the durability of the solar cell is improved. If the thickness is 3000 nm or less, even if the thickness of the inorganic layer is increased, the generated stress is small, and therefore, the peeling between the inorganic layer and the laminate can be suppressed.
- the more preferable lower limit of the thickness is 50 nm, the more preferable upper limit is 1000 nm, the still more preferable lower limit is 100 nm, and the still more preferable upper limit is 500 nm.
- the thickness of the inorganic layer can be measured using an optical interference type film thickness measuring device (for example, FE-3000 manufactured by Otsuka Electronics Co., Ltd.).
- the method for sealing the laminate with the thermosetting resin or thermoplastic resin is not particularly limited.
- the laminate is sealed using a sheet-like barrier layer material. Methods and the like.
- the materials for the barrier layer vacuum deposition, sputtering, gas phase reaction (CVD), and ion plating are preferred as methods for sealing the laminate with the inorganic material.
- the sputtering method is preferable for forming a dense layer, and the DC magnetron sputtering method is more preferable among the sputtering methods.
- an inorganic layer made of an inorganic material can be formed by using a metal target and oxygen gas or nitrogen gas as raw materials and depositing the raw material on the laminate to form a film.
- the barrier layer material may be a combination of the thermosetting resin or thermoplastic resin and the inorganic material.
- the barrier layer may be covered with another material such as a resin film or a resin film coated with an inorganic material. That is, the solar cell of the first aspect of the present invention may have a configuration in which the layered body and the other materials are sealed, filled, or bonded with the barrier layer. Thereby, even if there is a pinhole in the barrier layer, water vapor can be sufficiently blocked, and the durability of the solar cell can be further improved.
- a method of manufacturing a solar cell containing nitride, carbide or boride containing at least one element selected from the group consisting of silicon, magnesium, vanadium, chromium, molybdenum, tantalum and tungsten is also one aspect of the present invention. It is.
- the solar cell production method of the present invention is preferably a roll-to-roll method from the viewpoint of productivity.
- the roll-to-roll system may be a system that transports samples continuously or a step feed system that transports samples intermittently.
- a single wafer system can be used.
- an electron transport layer is provided between the cathode and the photoelectric conversion layer.
- the electron transport layer plays a role of improving the photoelectric conversion efficiency of the solar cell by efficiently moving electrons and holes generated by photoexcitation without re-joining.
- materials such as aluminum are often used as electrodes because of low material costs and low resistivity.
- the present inventors have used a metal having a relatively low ionization tendency as a cathode, in particular, a metal having a lower ionization tendency than titanium, so that a halogen atom or a chalcogen atom is formed on the cathode from the organic / inorganic perovskite compound contained in the photoelectric conversion layer. It was found that the series resistance of the solar cell can be kept low by suppressing diffusion and the photoelectric conversion efficiency can be improved. As a result, the second present invention was completed.
- the solar cell of 2nd this invention has a cathode, an electron carrying layer, a photoelectric converting layer, and an anode in this order.
- the cathode includes a metal having a smaller ionization tendency than titanium. Suppresses diffusion of halogen atoms or chalcogen atoms from the organic / inorganic perovskite compound contained in the photoelectric conversion layer to the cathode by using a metal with a relatively low ionization tendency as the cathode, especially a metal with a lower ionization tendency than titanium.
- the series resistance of the solar cell can be kept low, and the photoelectric conversion efficiency can be improved.
- the metal having a lower ionization tendency than titanium is not particularly limited. Specifically, for example, molybdenum, zirconium, manganese, tantalum, zinc, chromium, iron, cadmium, cobalt, nickel, tin, lead, antimony, bismuth, copper , Mercury, silver, palladium, iridium, platinum, gold and the like. These metals may be used independently and 2 or more types may be used together. Among these, one or more metals selected from the group consisting of molybdenum, cobalt, and nickel are preferable from the viewpoint of workability, and molybdenum is more preferable because there is less fear of diffusing into the photoelectric conversion layer and corroding the photoelectric conversion layer. .
- a preferable minimum is 10 nm and a preferable upper limit is 1000 nm.
- the cathode can sufficiently receive electrons. If the said thickness is 1000 nm or less, the thermal damage to the board
- the more preferable lower limit of the thickness of the cathode is 30 nm, the more preferable upper limit is 500 nm, the still more preferable lower limit is 50 nm, and the still more preferable upper limit is 200 nm.
- the solar cell of the second aspect of the present invention preferably further has a conductive layer under the cathode.
- the cathode means a conductive layer in direct contact with the electron transport layer
- the conductive layer means a layer that does not directly touch the electron transport layer.
- the material for the conductive layer is not particularly limited, but aluminum, gold, silver, and copper are preferable because of low resistivity. Among these, aluminum is more preferable because the material cost is low. These materials may be used alone or in combination of two or more.
- the thickness of the said conductive layer is not specifically limited, A preferable minimum is 10 nm and a preferable upper limit is 5 mm. If the said thickness is 10 nm or more, the series resistance of a solar cell can be reduced more and photoelectric conversion efficiency can be improved. If the said thickness is 5 mm or less, material cost can be suppressed and a solar cell can be manufactured cheaply. A more preferable lower limit of the thickness of the conductive layer is 50 nm, and a more preferable upper limit is 1 mm.
- the material for the electron transport layer is not particularly limited, and examples thereof include an n-type metal oxide, an N-type conductive polymer, an N-type low molecular organic semiconductor, an alkali metal halide, an alkali metal, and a surfactant. Specific examples include titanium oxide and tin oxide. Cyano group-containing polyphenylene vinylene, boron-containing polymer, bathocuproine, bathophenanthrene, hydroxyquinolinato aluminum, oxadiazole compound, benzimidazole compound, naphthalene tetracarboxylic acid compound, perylene derivative, phosphine oxide compound, phosphine sulfide compound, fluoro group-containing phthalocyanine And so on.
- n-type metal oxides, alkali metal halides, and alkali metals are preferable from the viewpoint of suppressing diffusion of halogen atoms or chalcogen atoms from the organic / inorganic perovskite compound contained in the photoelectric conversion layer to the cathode.
- the density of the electron transport layer can be increased, and the diffusion of halogen atoms or chalcogen atoms from the organic-inorganic perovskite compound contained in the photoelectric conversion layer can be further reduced.
- an oxide for example, titanium oxide or tin oxide
- a metal having a relatively low ionization tendency is more preferable.
- the electron transport layer may consist of only a thin film electron transport layer (buffer layer), but preferably includes a porous electron transport layer.
- the photoelectric conversion layer is a composite film in which an organic semiconductor or an inorganic semiconductor part and an organic / inorganic perovskite compound part are combined, a more complex composite film (a more complicated structure) is obtained, and the photoelectric conversion efficiency Therefore, the composite film is preferably formed on the porous electron transport layer.
- the preferable lower limit of the thickness of the electron transport layer is 1 nm, and the preferable upper limit is 2000 nm. If the thickness is 1 nm or more, holes can be sufficiently blocked. If the said thickness is 2000 nm or less, it will become difficult to become resistance at the time of electron transport, and photoelectric conversion efficiency will become high.
- the more preferable lower limit of the thickness of the electron transport layer is 3 nm, the more preferable upper limit is 1000 nm, the still more preferable lower limit is 5 nm, and the still more preferable upper limit is 500 nm.
- the photoelectric conversion layer includes an organic / inorganic perovskite compound represented by the general formula R-MX 3 (where R is an organic molecule, M is a metal atom, and X is a halogen atom or a chalcogen atom).
- the solar cell in which the photoelectric conversion layer includes the organic / inorganic perovskite compound is also referred to as an organic / inorganic hybrid solar cell.
- the material of the said anode is not specifically limited, A conventionally well-known material can be used.
- the anode is preferably a patterned electrode.
- the anode material include ITO (indium tin oxide), SnO 2 , AZO (aluminum zinc oxide), IZO (indium zinc oxide), GZO (gallium zinc oxide), and BZO (boron zinc oxide).
- ITO indium tin oxide
- SnO 2 aluminum zinc oxide
- IZO indium zinc oxide
- GZO gallium zinc oxide
- BZO boron zinc oxide
- Examples thereof include a conductive transparent material and a conductive transparent polymer. These materials may be used alone or in combination of two or more.
- the solar cell of the second aspect of the present invention may have a hole transport layer between the photoelectric conversion layer and the anode.
- a hole transport layer between the photoelectric conversion layer and the anode.
- the solar cell of the second aspect of the present invention may further have a substrate or the like.
- substrate is not specifically limited, For example, transparent glass substrates, such as soda-lime glass and an alkali free glass, a ceramic substrate, a plastic substrate, a metal substrate, etc. are mentioned.
- the laminate having the cathode, the electron transport layer, the photoelectric conversion layer, and the anode in this order may be sealed with a barrier layer.
- a barrier layer is the same as that of the barrier layer in the solar cell of the 1st this invention mentioned above.
- the solar cell of the second aspect of the present invention in the same manner as the solar cell of the first aspect of the present invention described above, other materials such as a resin film and a resin film coated with an inorganic material are further formed on the barrier layer. It may be covered.
- FIG. 3 is a cross-sectional view schematically showing an example of the solar cell of the second invention.
- 3 includes an electron transport layer 8 (a thin film electron transport layer 81 and a porous electron transport layer 82), a photoelectric conversion layer 9 containing an organic / inorganic perovskite compound, a hole transport layer on a cathode 7. 10 and the anode 11 are laminated in this order.
- a conductive layer may be disposed under the cathode 7.
- the anode 11 is a patterned electrode.
- the method for producing the solar cell of the second invention is not particularly limited.
- the conductive layer, the cathode, the electron transport layer, the photoelectric conversion layer, the hole transport layer, and the anode are formed on the substrate.
- the method of forming in order is mentioned.
- the cutting process for example, mechanical patterning
- the solar cell excellent in the photoelectric conversion efficiency and the manufacturing method of this solar cell can be provided.
- a solar cell with low series resistance and high photoelectric conversion efficiency can be provided.
- Example 1 An aluminum oxide film (thickness 5 ⁇ m, thickness ratio 5%) is formed on the surface of the aluminum foil by anodizing aluminum foil (manufactured by UACJ, general-purpose aluminum material A1N30 grade, thickness 100 ⁇ m) by alumite sulfate treatment for 30 minutes. ) To obtain a flexible substrate.
- a hard film (thickness: 100 nm, Vickers hardness: 2100 HV) made of titanium nitride (TiN) is produced with a RF output of 300 W against a 6-inch Ti target using a batch type sputtering apparatus (manufactured by ULVAC). Filmed. At this time, 20 sccm of Ar and 5 sccm of N 2 were introduced as process gases, and the pressure during film formation was adjusted to 0.1 Pa.
- Ti / Al film An Al film having a thickness of 100 nm was formed on the hard film by a vapor deposition machine, and a Ti film having a thickness of 100 nm was further formed on the Al film by a sputtering method to form a cathode (Ti / Al film).
- the Ti / Al film was patterned (cutting width: 40 ⁇ m) by mechanical patterning using a mechanical scribing machine (manufactured by Samsung Diamond Industrial Co., Ltd., KMPD100).
- a titanium oxide paste containing polyisobutyl methacrylate as an organic binder and titanium oxide (a mixture of an average particle diameter of 10 nm and 30 nm) is applied onto the Ti / Al film by spin coating, and then at 200 ° C. for 30 minutes. Firing was performed to form a porous electron transport layer having a thickness of 500 nm.
- lead iodide as a metal halide compound was dissolved in N, N-dimethylformamide (DMF) to prepare a 1M solution, and a film was formed on the porous electron transport layer by a spin coating method. Further, methylammonium iodide as an amine compound was dissolved in 2-propanol to prepare a 1M solution. A layer containing CH 3 NH 3 PbI 3 , which is an organic / inorganic perovskite compound, was formed by immersing the sample formed of lead iodide in the solution. Thereafter, the obtained sample was annealed at 120 ° C. for 30 minutes.
- a solution was prepared by dissolving 68 mM Spiro-OMeTAD (having a spirobifluorene skeleton), 55 mM t-butylpyridine, and 9 mM bis (trifluoromethylsulfonyl) imide / silver salt in 25 ⁇ L of chlorobenzene.
- This solution was applied onto the photoelectric conversion layer by a spin coating method to form a hole transport layer having a thickness of 150 nm.
- an ITO film having a thickness of 100 nm was formed as a positive electrode (transparent electrode) by sputtering.
- the ITO film was patterned by mechanical patterning.
- a barrier layer made of ZnSnO with a thickness of 100 nm was formed on the obtained anode by a sputtering method to obtain a solar cell.
- Example 2 to 12 A solar cell was obtained in the same manner as in Example 1 except that the hard film was changed as shown in Table 1.
- Example 2 A solar cell was obtained in the same manner as in Example 1 except that the hard film was not formed and the thickness of the aluminum oxide film was changed to 10 ⁇ m.
- a power source (manufactured by KEITHLEY, model 236) is connected between the electrodes of the solar cell, and a photoelectric simulation is performed with an exposure area of 1 cm 2 using a solar simulation (manufactured by Yamashita Denso Co., Ltd.) with an intensity of 100 mW / cm 2. Conversion efficiency was measured.
- the photoelectric conversion efficiency of the solar cells obtained in Example 1 was normalized to 1.0, and the photoelectric conversion efficiency of the solar cells obtained in Examples 2 to 12 and Comparative Examples 1 to 3 was normalized.
- Example 13 An aluminum film having a thickness of 200 nm as a conductive layer and a molybdenum film having a thickness of 50 nm as a cathode were successively formed on a glass substrate by an electron beam evaporation method.
- titanium oxide was sputtered on the surface of the cathode using a sputtering apparatus (manufactured by ULVAC) to form a thin-film electron transport layer having a thickness of 30 nm.
- an ethanol dispersion of titanium oxide (a mixture of an average particle size of 10 nm and 30 nm) was applied on the thin film electron transport layer by a spin coating method, then baked at 200 ° C. for 10 minutes, and a porous material having a thickness of 150 nm.
- a shaped electron transport layer was formed.
- CH 3 NH 3 I and PbI 2 were dissolved at a molar ratio of 1: 1 using N, N-dimethylformamide (DMF) as a solvent as a solution for forming an organic inorganic perovskite compound, and the total of CH 3 NH 3 I and PbI 2 The weight concentration was adjusted to 20%. After laminating this solution on the electron transport layer by spin coating, it was baked at 100 ° C. for 10 minutes to form a photoelectric conversion layer.
- DMF N, N-dimethylformamide
- an ITO film having a thickness of 200 nm is formed as an anode by sputtering using a sputtering apparatus (manufactured by ULVAC), and a conductive layer / cathode / electron transport layer / photoelectric conversion layer / hole transport layer. / A solar cell with an anode laminated was obtained.
- Example 14 to 22 Conductive layer / cathode / electron transport layer / photoelectric conversion layer in the same manner as in Example 13 except that the type of conductive layer, the type of cathode, the thickness of the cathode, and the type of electron transport layer were changed as shown in Table 2. A solar cell in which / hole transport layer / anode was laminated was obtained.
- Example 4 The cathode / electron transport layer / photoelectric conversion layer / hole transport layer / non-conductive film was formed in the same manner as in Example 13 except that an aluminum film (which has a higher ionization tendency than titanium) was formed as the cathode. A solar cell in which the anode was laminated was obtained.
- a power source (KEITHLEY, 236 model) is connected between the electrodes of the solar cell, and a current-voltage curve is drawn using a solar simulation (manufactured by Yamashita Denso) with an intensity of 100 mW / cm 2.
- the photoelectric conversion efficiency was calculated. When the photoelectric conversion efficiency was 10% or more, ⁇ , when it was 8% or more and less than 10%, ⁇ , and when it was less than 8%, it was marked as x.
- the cutting process for example, mechanical patterning
- the solar cell excellent in the photoelectric conversion efficiency and the manufacturing method of this solar cell can be provided.
- a solar cell with low series resistance and high photoelectric conversion efficiency can be provided.
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Abstract
Description
そこで、近年、中心金属に鉛、スズ等を用いたペロブスカイト構造を有する有機無機ペロブスカイト化合物を光電変換層に用いた、ペロブスカイト太陽電池が注目されている(例えば、特許文献1、非特許文献1)。ペロブスカイト太陽電池は、高い光電変換効率が期待できるうえに、印刷法によって製造できることから製造コストを大幅に削減することができる。
例えば、特許文献2には、シート状のアルミニウム基材を含む半導体装置用基板、及び、この半導体装置用基板を含む有機薄膜太陽電池が記載されている。
また、本発明は、陰極、電子輸送層、光電変換層及び陽極をこの順に有する太陽電池であって、前記光電変換層は、一般式R-M-X3(但し、Rは有機分子、Mは金属原子、Xはハロゲン原子又はカルコゲン原子である。)で表される有機無機ペロブスカイト化合物を含み、前記陰極は、チタンよりもイオン化傾向の小さい金属を含む太陽電池(本明細書中、第2の本発明ともいう)である。
以下、本発明を詳述する。
このような切削加工において、本発明者らは、電極の下に位置するフレキシブル基材に切削ツールの刃先が当たり、フレキシブル基材への刃先のくい込みやフレキシブル基材の凹みが発生することにより、製品不良が発生するという問題を新たに見出した。切削ツールにかける荷重を変えることにより切削深さを制御することはできるものの、大量生産においては荷重が安定せずばらつくことがあるため、フレキシブル基材への刃先のくい込みやフレキシブル基材の凹みの発生を充分に抑制することは難しかった。
太陽電池の製造時には、次いで、切削加工された電極上に光電変換層の形成を行い、その形成した光電変換層を更に一部切削加工し、更に、切削加工された光電変換層上に透明電極の形成を行い、その形成した透明電極を更に一部切削加工する。このようにして、フレキシブル基材上にパターニングされた複数の層を積層していくことが一般的である。
本発明者らは、フレキシブル基材上に、電極と、透明電極と、上記電極と上記透明電極との間に配置された光電変換層とを有する太陽電池を検討した。本発明者らは、このような太陽電池において、更に、フレキシブル基材と電極との間に特定の硬質膜を設けることにより、フレキシブル基材への刃先のくい込みやフレキシブル基材の凹みの発生を抑制しつつ切削加工(例えば、メカニカルパターニング)を良好に行うことができ、光電変換効率に優れた太陽電池を得ることができることを見出した。これにより、第1の本発明を完成させるに至った。
本明細書中、「層」とは、明確な境界を有する層だけではなく、含有元素が徐々に変化する濃度勾配のある層をも意味する。層の元素分析は、例えば、太陽電池の断面のFE-TEM/EDS線分析測定を行い、特定元素の元素分布を確認する等によって行うことができる。また、本明細書中、層とは、平坦な薄膜状の層だけではなく、他の層と一緒になって複雑に入り組んだ構造を形成しうる層をも意味する。
上記金属箔を用いることにより、耐熱性高分子を用いる場合と比べてコストを抑えられるとともに、高温処理を行うことができる。即ち、有機無機ペロブスカイト化合物を含む光電変換層形成時において耐光性(光劣化に対する耐性)を付与する目的で80℃以上の温度で熱アニール(加熱処理)を行っても、歪みの発生を最小限に抑えて、高い光電変換効率を得ることができる。
上記絶縁層として上記酸化アルミニウム被膜を用いることにより、有機絶縁層の場合と比べて、大気中の水分が絶縁層を透過して光電変換層(特に、有機無機ペロブスカイト化合物を含む光電変換層)を劣化させることを抑制することができる。また、上記絶縁層として上記酸化アルミニウム被膜を用いることにより、上記アルミニウム箔と接することで時間の経過とともに有機無機ペロブスカイト化合物を含む光電変換層に変色が生じ、腐食が起きるという現象を抑制することができる。
一般的な他の太陽電池では光電変換層がアルミニウムと反応して変色が生じること等は報告されておらず、上記のような腐食が起きるという現象は、光電変換層が有機無機ペロブスカイト化合物を含むペロブスカイト太陽電池に特有の問題として本発明者らが見出したものである。
上記酸化アルミニウム被膜の厚みは、例えば、上記フレキシブル基材の断面を電子顕微鏡(例えば、S-4800、HITACHI社製等)で観察し、得られた写真のコントラストを解析することにより測定することができる。
即ち、上記酸化アルミニウム被膜は後述する硬質膜に比べて硬度が低いため、上記アルミニウム箔への刃先のくい込みや上記アルミニウム箔の凹みの発生を抑制するためには、厚みを大きく増加させる必要がある。一方で、厚みを大きく増加させると、上記酸化アルミニウム被膜にクラックが生じやすくなる弊害が発生する。
上記酸化アルミニウム被膜は、一般的にビッカース硬さが300HV程度である。
上記アルミニウム箔に陽極酸化を施す場合には、陽極酸化における処理濃度、処理温度、電流密度、処理時間等を変更することにより、上記酸化アルミニウム被膜の厚みを調整することができる。上記処理時間は特に限定されないが、上記フレキシブル基材の作製の容易さの観点から、好ましい下限は5分、好ましい上限は120分であり、より好ましい上限は60分である。
上記フレキシブル基材の厚みとは、上記フレキシブル基材が上記金属箔と上記金属箔上に形成された絶縁層とを有する場合、上記金属箔と上記絶縁層とを含む上記フレキシブル基材全体の厚みを意味する。
上記電極及び上記透明電極は、どちらが陰極になってもよく、陽極になってもよい。上記電極及び上記透明電極の材料として、例えば、FTO(フッ素ドープ酸化スズ)、ナトリウム、ナトリウム-カリウム合金、リチウム、マグネシウム、アルミニウム、マグネシウム-銀混合物、マグネシウム-インジウム混合物、アルミニウム-リチウム合金、Al/Al2O3混合物、Al/LiF混合物、金等の金属等が挙げられる。また、CuI、ITO(インジウムスズ酸化物)、SnO2、AZO(アルミニウム亜鉛酸化物)、IZO(インジウム亜鉛酸化物)、GZO(ガリウム亜鉛酸化物)等の導電性透明材料、導電性透明ポリマー等が挙げられる。これらの材料は単独で用いられてもよく、2種以上が併用されてもよい。
上記光電変換層に上記有機無機ペロブスカイト化合物を用いることにより、太陽電池の光電変換効率を向上させることができる。
上記Rは、具体的には例えば、メチルアミン、エチルアミン、プロピルアミン、ブチルアミン、ペンチルアミン、ヘキシルアミン、ジメチルアミン、ジエチルアミン、ジプロピルアミン、ジブチルアミン、ジペンチルアミン、ジヘキシルアミン、トリメチルアミン、トリエチルアミン、トリプロピルアミン、トリブチルアミン、トリペンチルアミン、トリヘキシルアミン、エチルメチルアミン、メチルプロピルアミン、ブチルメチルアミン、メチルペンチルアミン、ヘキシルメチルアミン、エチルプロピルアミン、エチルブチルアミン、イミダゾール、アゾール、ピロール、アジリジン、アジリン、アゼチジン、アゼト、イミダゾリン、カルバゾール、メチルカルボキシアミン、エチルカルボキシアミン、プロピルカルボキシアミン、ブチルカルボキシアミン、ペンチルカルボキシアミン、ヘキシルカルボキシアミン、ホルムアミジニウム、グアニジン、アニリン、ピリジン及びこれらのイオンやフェネチルアンモニウム等が挙げられる。上記イオンとしては、例えば、メチルアンモニウム(CH3NH3)等が挙げられる。なかでも、メチルアミン、エチルアミン、プロピルアミン、プロピルカルボキシアミン、ブチルカルボキシアミン、ペンチルカルボキシアミン、ホルムアミジニウム、グアニジン及びこれらのイオンが好ましく、メチルアミン、エチルアミン、ペンチルカルボキシアミン、ホルムアミジニウム、グアニジン及びこれらのイオンがより好ましい。なかでも、高い光電変換効率が得られることから、メチルアミン、ホルムアミジニウム及びこれらのイオンが更に好ましい。
図2は、体心に金属原子M、各頂点に有機分子R、面心にハロゲン原子又はカルコゲン原子Xが配置された立方晶系の構造である、有機無機ペロブスカイト化合物の結晶構造の一例を示す模式図である。詳細は明らかではないが、上記構造を有することにより、結晶格子内の八面体の向きが容易に変わることができるため、上記有機無機ペロブスカイト化合物中の電子の移動度が高くなり太陽電池の光電変換効率が向上すると推定される。
上記有機無機ペロブスカイト化合物が結晶性半導体であれば、上記有機無機ペロブスカイト化合物中の電子の移動度が高くなり、太陽電池の光電変換効率が向上する。上記有機無機ペロブスカイト化合物が結晶性半導体であれば、太陽電池に光を照射し続けることによる光電変換効率の低下(光劣化)、特に短絡電流の低下に起因する光劣化が抑制されやすくなる。
上記有機無機ペロブスカイト化合物の結晶化度の好ましい下限は30%である。上記結晶化度が30%以上であれば、上記有機無機ペロブスカイト化合物中の電子の移動度が高くなり、太陽電池の光電変換効率が向上する。上記結晶化度が30%以上であれば、太陽電池に光を照射し続けることによる光電変換効率の低下(光劣化)、特に短絡電流の低下に起因する光劣化が抑制されやすくなる。上記結晶化度のより好ましい下限は50%、更に好ましい下限は70%である。
上記有機無機ペロブスカイト化合物の結晶化度を上げる方法として、例えば、熱アニール(加熱処理)、レーザー等の強度の強い光の照射、プラズマ照射等が挙げられる。
上記有機無機ペロブスカイト化合物の結晶子径が5nm以上であれば、太陽電池に光を照射し続けることによる光電変換効率の低下(光劣化)、特に短絡電流の低下に起因する光劣化が抑制される。上記有機無機ペロブスカイト化合物中の電子の移動度が高くなり、太陽電池の光電変換効率が向上する。上記結晶子径のより好ましい下限は10nm、更に好ましい下限は20nmである。
上記有機半導体として、例えば、ポリ(3-アルキルチオフェン)等のチオフェン骨格を有する化合物等が挙げられる。例えば、ポリパラフェニレンビニレン骨格、ポリビニルカルバゾール骨格、ポリアニリン骨格、ポリアセチレン骨格等を有する導電性高分子等も挙げられる。更に、例えば、フタロシアニン骨格、ナフタロシアニン骨格、ペンタセン骨格、ベンゾポルフィリン骨格等のポルフィリン骨格、スピロビフルオレン骨格等を有する化合物や、表面修飾されていてもよいカーボンナノチューブ、グラフェン、フラーレン等のカーボン含有材料も挙げられる。
耐熱性高分子からなる樹脂フィルムを用いた太陽電池にこのような熱アニール(加熱処理)を行うと、樹脂フィルムと光電変換層等との熱膨張係数の差により、アニール時に歪みが生じ、その結果、高い光電変換効率を達成することが難しくなることがある。上記金属箔を用いた場合には、熱アニール(加熱処理)を行っても、歪みの発生を最小限に抑えて、高い光電変換効率を得ることができる。
これらの加熱操作は真空又は不活性ガス下で行われることが好ましく、露点温度は10℃以下が好ましく、7.5℃以下がより好ましく、5℃以下が更に好ましい。
上記フレキシブル基材と上記電極との間に上記硬質膜を設けることにより、フレキシブル基材への刃先のくい込みやフレキシブル基材の凹みの発生を抑制しつつ切削加工(例えば、メカニカルパターニング)を良好に行うことができ、光電変換効率に優れた太陽電池を得ることができる。
上記硬質膜のビッカース硬さ(HV)は、例えば、ナノインデンターG200(Keysight Technologies社製)を用い、ガラス基板上に形成した硬質膜に対して圧子を押し込み、得られた荷重-変異曲線から算出することで求めることができる。
上記硬質膜の厚みは、例えば、段差形状測定装置P-16+(KLA Tencor社製)により測定することができる。
上記電子輸送層の材料は特に限定されず、例えば、N型導電性高分子、N型低分子有機半導体、N型金属酸化物、N型金属硫化物、ハロゲン化アルカリ金属、アルカリ金属、界面活性剤等が挙げられる。具体的には例えば、シアノ基含有ポリフェニレンビニレン、ホウ素含有ポリマー、バソキュプロイン、バソフェナントレン、ヒドロキシキノリナトアルミニウム、オキサジアゾール化合物、ベンゾイミダゾール化合物、ナフタレンテトラカルボン酸化合物、ペリレン誘導体、ホスフィンオキサイド化合物、ホスフィンスルフィド化合物、フルオロ基含有フタロシアニン等が挙げられる。酸化チタン、酸化亜鉛、酸化インジウム、酸化スズ、酸化ガリウム、硫化スズ、硫化インジウム、硫化亜鉛等も挙げられる。
上記ホール輸送層の材料は特に限定されず、例えば、P型導電性高分子、P型低分子有機半導体、P型金属酸化物、P型金属硫化物、界面活性剤等が挙げられる。具体的には例えば、ポリ(3-アルキルチオフェン)等のチオフェン骨格を有する化合物等が挙げられる。また、例えば、トリフェニルアミン骨格、ポリパラフェニレンビニレン骨格、ポリビニルカルバゾール骨格、ポリアニリン骨格、ポリアセチレン骨格等を有する導電性高分子等も挙げられる。更に、例えば、フタロシアニン骨格、ナフタロシアニン骨格、ペンタセン骨格、ベンゾポルフィリン骨格等のポルフィリン骨格、スピロビフルオレン骨格等を有する化合物等も挙げられる。更に、例えば、酸化モリブデン、酸化バナジウム、酸化タングステン、酸化ニッケル、酸化銅、酸化スズ、硫化モリブデン、硫化タングステン、硫化銅、硫化スズ等、フルオロ基含有ホスホン酸、カルボニル基含有ホスホン酸、CuSCN、CuI等の銅化合物、カーボンナノチューブ、グラフェン等のカーボン含有材料等が挙げられる。
上記バリア層の材料としてはバリア性を有していれば特に限定されないが、熱硬化性樹脂、熱可塑性樹脂又は無機材料等が挙げられる。
上記無機層の厚みは、光学干渉式膜厚測定装置(例えば、大塚電子社製のFE-3000等)を用いて測定することができる。
上記スパッタリング法においては、金属ターゲット、及び、酸素ガス又は窒素ガスを原料とし、上記積層体上に原料を堆積して製膜することにより、無機材料からなる無機層を形成することができる。
上記バリア層の材料は、上記熱硬化性樹脂又は熱可塑性樹脂と、上記無機材料との組み合わせでもよい。
本発明者らは、太陽電池の光電変換効率を向上させることを目的として検討を行った結果、光電変換層に含まれる有機無機ペロブスカイト化合物から陰極にハロゲン原子又はカルコゲン原子が拡散し、陰極を変質させてしまうことで直列抵抗が上昇し、太陽電池の光電変換効率が低下することを見出した。
本発明者らは、陰極としてイオン化傾向の比較的小さい金属、なかでもチタンよりもイオン化傾向の小さい金属を用いることにより、光電変換層に含まれる有機無機ペロブスカイト化合物から陰極にハロゲン原子又はカルコゲン原子が拡散することを抑制して、太陽電池の直列抵抗を低く維持することができ、光電変換効率を向上できることを見出した。これにより、第2の本発明を完成させるに至った。
上記陰極は、チタンよりもイオン化傾向の小さい金属を含む。
上記陰極としてイオン化傾向の比較的小さい金属、なかでもチタンよりもイオン化傾向の小さい金属を用いることにより、光電変換層に含まれる有機無機ペロブスカイト化合物から陰極にハロゲン原子又はカルコゲン原子が拡散することを抑制して、太陽電池の直列抵抗を低く維持することができ、光電変換効率を向上することができる。
本発明中、陰極とは、電子輸送層と直接接している導電性の層を意味し、導電層とは、電子輸送層には直接触れない層を意味する。
上記陰極の下に上記導電層を設けることにより、太陽電池の直列抵抗をより低減し、光電変換効率を向上することができる。
なかでも、光電変換層に含まれる有機無機ペロブスカイト化合物から陰極にハロゲン原子又はカルコゲン原子が拡散することを抑制する観点から、n型金属酸化物、ハロゲン化アルカリ金属、アルカリ金属が好ましい。これらの材料を用いることにより、電子輸送層の密度を大きくし、光電変換層に含まれる有機無機ペロブスカイト化合物からのハロゲン原子又はカルコゲン原子の拡散をより低減できる。更には、ハロゲン原子又はカルコゲン原子による電子輸送層の腐食を防ぐ観点から、イオン化傾向の比較的低い金属を含む酸化物(例えば、酸化チタン、酸化スズ)がより好ましい。これらの材料を用いることにより、電子輸送層の安定性を増し、太陽電池の耐久性を向上することができる。
上記光電変換層に上記有機無機ペロブスカイト化合物を用いることにより、太陽電池の光電変換効率を向上させることができる。
上記光電変換層の詳細については、上述した第1の本発明の太陽電池における光電変換層と同様である。
陽極材料として、例えば、ITO(インジウムスズ酸化物)、SnO2、AZO(アルミニウム亜鉛酸化物)、IZO(インジウム亜鉛酸化物)、GZO(ガリウム亜鉛酸化物)、BZO(ホウ素亜鉛酸化物)等の導電性透明材料、導電性透明ポリマー等が挙げられる。これらの材料は単独で用いられてもよく、2種以上が併用されてもよい。
上記ホール輸送層の詳細については、上述した第1の本発明の太陽電池におけるホール輸送層と同様である。
上記バリア層の詳細については、上述した第1の本発明の太陽電池におけるバリア層と同様である。
図3に示す太陽電池6は、陰極7上に電子輸送層8(薄膜状の電子輸送層81と多孔質状の電子輸送層82)、有機無機ペロブスカイト化合物を含む光電変換層9、ホール輸送層10及び陽極11がこの順に積層されたものである。図示しないが、陰極7の下に導電層が配置されていてもよい。図3に示す太陽電池6において、陽極11はパターニングされた電極である。
アルミニウム箔(UACJ社製、汎用アルミ材A1N30グレード、厚み100μm)に硫酸アルマイト処理により処理時間30分で陽極酸化を施すことにより、アルミニウム箔の表面に酸化アルミニウム被膜(厚み5μm、厚みの比率5%)を形成し、フレキシブル基材を得た。
硬質膜を表1に示すように変更したこと以外は実施例1と同様にして、太陽電池を得た。
硬質膜を形成しなかったこと以外は実施例1と同様にして、太陽電池を得た。
硬質膜を形成せず、酸化アルミニウム被膜の厚みを10μmに変更したこと以外は実施例1と同様にして、太陽電池を得た。
硬質膜を表1に示すように変更したこと以外は実施例1と同様にして、太陽電池を得た。
実施例1~12及び比較例1~3で得られた太陽電池について、下記の評価を行った。
太陽電池の電極間に電源(KEITHLEY社製、236モデル)を接続し、強度100mW/cm2のソーラーシミュレーション(山下電装社製)を用い、露光面積1cm2で光電変換効率を測定した。
実施例1で得られた太陽電池の光電変換効率を1.0として、実施例2~12及び比較例1~3で得られた太陽電池の光電変換効率を規格化した。規格化した値が0.9以上であった場合を「◎」、0.9未満0.7以上であった場合を「○」、0.7未満0.6以上であった場合を「△」、0.6未満であった場合を「×」とした。
ガラス基板上に、導電層として厚み200nmのアルミニウム膜、陰極として厚み50nmのモリブデン膜を電子ビーム蒸着法により立て続けに製膜した。
次に、陰極の表面上に酸化チタンをスパッタリング装置(アルバック社製)を用いてスパッタすることで厚み30nmの薄膜状の電子輸送層を形成した。更に、薄膜状の電子輸送層上に、酸化チタン(平均粒子径10nmと30nmとの混合物)のエタノール分散液をスピンコート法により塗布した後、200℃で10分間焼成し、厚み150nmの多孔質状の電子輸送層を形成した。
導電層の種類、陰極の種類、陰極の厚み及び電子輸送層の種類を表2に示すように変更したこと以外は実施例13と同様にして、導電層/陰極/電子輸送層/光電変換層/ホール輸送層/陽極が積層された太陽電池を得た。
導電層を製膜せず、陰極としてアルミニウム膜(チタンよりもイオン化傾向が大きい)を製膜したこと以外は実施例13と同様にして、陰極/電子輸送層/光電変換層/ホール輸送層/陽極が積層された太陽電池を得た。
陰極の種類を表2に示すように変更したこと以外は実施例13と同様にして、導電層/陰極/電子輸送層/光電変換層/ホール輸送層/陽極が積層された太陽電池を得た。
実施例13~22及び比較例4~6で得られた太陽電池について、以下の評価を行った。結果を表1に示した。
太陽電池の電極間に電源(KEITHLEY社製、236モデル)を接続し、強度100mW/cm2のソーラーシミュレーション(山下電装社製)を用いて電流-電圧曲線を描画し、光電変換効率を算出した。光電変換効率が10%以上の場合◎、8%以上10%未満の場合○、8%未満の場合×とした。
(1)で描画した電流-電圧曲線において、曲線のX軸との交点における傾きの逆数を直列抵抗として算出した。直列抵抗が5Ω未満の場合◎、5Ω以上10Ω未満の場合○、10Ω以上の場合×とした。
2 絶縁層
3 硬質膜
4 電極
41 溝
5 切削ツール
6 太陽電池
7 陰極
8 電子輸送層
81 薄膜状の電子輸送層
82 多孔質状の電子輸送層
9 有機無機ペロブスカイト化合物を含む光電変換層
10 ホール輸送層
11 陽極(パターニングされた電極)
Claims (11)
- フレキシブル基材上に、電極と、透明電極と、前記電極と前記透明電極との間に配置された光電変換層とを有する太陽電池であって、
更に、前記フレキシブル基材と前記電極との間に配置された硬質膜を有し、
前記硬質膜は、チタン、ジルコニウム、アルミニウム、ケイ素、マグネシウム、バナジウム、クロム、モリブデン、タンタル及びタングステンからなる群より選択される少なくとも1種の元素を含む窒化物、炭化物又はホウ化物を含む
ことを特徴とする太陽電池。 - 硬質膜は、ビッカース硬さが500~3500HVであることを特徴とする請求項1記載の太陽電池。
- フレキシブル基材は、金属箔と前記金属箔上に形成された絶縁層とを有することを特徴とする請求項1又は2記載の太陽電池。
- 金属箔は、アルミニウム箔であり、絶縁層は、酸化アルミニウム被膜であることを特徴とする請求項3記載の太陽電池。
- 酸化アルミニウム被膜は、陽極酸化被膜であることを特徴とする請求項4記載の太陽電池。
- 光電変換層は、一般式R-M-X3(但し、Rは有機分子、Mは金属原子、Xはハロゲン原子又はカルコゲン原子である。)で表される有機無機ペロブスカイト化合物を含むことを特徴とする請求項1、2、3、4又は5記載の太陽電池。
- フレキシブル基材上に硬質膜を形成する工程と、
前記硬質膜上に電極を形成し、前記電極の切削加工を行う工程と、
前記切削加工された電極上に光電変換層を形成し、前記光電変換層の切削加工を行う工程と、
前記切削加工された光電変換層上に透明電極を形成し、前記透明電極の切削加工を行う工程とを有し、
前記硬質膜は、チタン、ジルコニウム、アルミニウム、ケイ素、マグネシウム、バナジウム、クロム、モリブデン、タンタル及びタングステンからなる群より選択される少なくとも1種の元素を含む窒化物、炭化物又はホウ化物を含む
ことを特徴とする太陽電池の製造方法。 - 陰極、電子輸送層、光電変換層及び陽極をこの順に有する太陽電池であって、
前記光電変換層は、一般式R-M-X3(但し、Rは有機分子、Mは金属原子、Xはハロゲン原子又はカルコゲン原子である。)で表される有機無機ペロブスカイト化合物を含み、
前記陰極は、チタンよりもイオン化傾向の小さい金属を含む
ことを特徴とする太陽電池。 - チタンよりもイオン化傾向の小さい金属は、モリブデン、コバルト及びニッケルからなる群より選択される1種以上の金属であることを特徴とする請求項8記載の太陽電池。
- チタンよりもイオン化傾向の小さい金属は、モリブデンであることを特徴とする請求項9記載の太陽電池。
- 更に、陰極の下に導電層を有することを特徴とする請求項8、9又は10記載の太陽電池。
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