Electronic Devices

Abstract

An electronic device 100 of the present disclosure comprises a first electrode 2, a photoelectric conversion layer 4, a hole transport layer 5, and a second electrode 6 in this order. In the electronic device 100 of the present disclosure, the second electrode 6 includes a conductive material and a first p-type dopant. The electronic device 100 of the present disclosure may further include, for example, an electron transport layer 3. The electron transport layer 3 is arranged, for example, between the first electrode 2 and the photoelectric conversion layer 4.

Description

[Technical Field]

[0001] The present disclosure relates to electronic devices. [Background technology]

[0002] In many electronic devices, in order to exhibit functions such as light absorption, light emission, amplification, or rectification, a hole transport layer or an electron transport layer is placed in contact with a photoelectric conversion layer, thereby extracting or supplying only holes or electrons in one direction.

[0003] The hole transport layer is a layer that allows holes to enter and exit the valence band of the adjacent photoelectric conversion layer and has the function of insulating electrons from the conduction band of the photoelectric conversion layer. The electron transport layer is a layer that allows electrons to enter and exit the conduction band of the adjacent photoelectric conversion layer and has the function of insulating holes from the valence band of the photoelectric conversion layer.

[0004] Although various hole transport materials exist as the main material constituting a hole transport layer, few materials have a hole concentration sufficient to function alone as a hole transport layer of an electronic device. In many cases, the required hole concentration can be achieved by adding an additive to the hole transport material. That is, the additive is a material that has the function of removing electrons from the valence band from the hole transport material.

[0005] A perovskite solar cell has a structure in which, for example, a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode are formed in this order. An electron transport layer may also be located between the first electrode and the photoelectric conversion layer. In a perovskite solar cell, the photoelectric conversion layer is a layer that absorbs light and generates electrons and holes. The hole transport layer is a layer that conducts only the holes generated in the photoelectric conversion layer to the second electrode and insulates the electrons. The electron transport layer is a layer that conducts only the electrons generated in the photoelectric conversion layer to the first electrode and insulates the holes (Non-Patent Document 1).

[0006] For example, an organic thin-film solar cell has a structure in which a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode are formed in this order. Although the details of the operating principle differ in some respects from perovskite solar cells, they are the same as perovskite solar cells in that the hole transport layer is a layer that does not conduct electrons but conducts only holes to the second electrode (Patent Document 1).

[0007] An organic EL light-emitting device using an organic compound as the light-emitting layer has a structure in which, for example, a first electrode, a light-emitting layer, a hole-transport layer, and a second electrode are formed in this order. The hole-transport layer in an organic EL light-emitting device is a functional layer that does not conduct electrons to the light-emitting layer but conducts only holes, and therefore operates differently from the perovskite solar cell or organic thin-film solar cell described above. However, the hole-transport layer is the same as a perovskite solar cell or organic thin-film solar cell in that it is a layer that does not conduct electrons but conducts only holes (Patent Document 2).

[0008] Thus, the hole transport layer is a core component for the operation of electronic devices. However, when an electrode is fabricated on the hole transport layer by coating ink, the performance of the electronic device tends to be poor (Non-Patent Document 2).

[0009] Patent Document 3 discloses an electrode containing a dopant for an electron transport layer. [Prior art documents] [Non-patent literature]

[0010] [Non-Patent Document 1] Materials Chemistry and Physics 256,p.123594(2020) [Non-patent document 2] Journal of Materials chemistry A,3,p.15996(2015) [Patent documents]

[0011] [Patent Document 1] JP 2012-216673 A [Patent Document 2] Patent Publication No. 2019-77685 [Patent Document 3] International Publication No. 2011 / 052546 Summary of the Invention [Problem to be solved by the invention]

[0012] It is an object of the present disclosure to provide electronic devices with improved device performance. [Means for solving the problem]

[0013] The electronic device of the present disclosure comprises, in this order, a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode, the second electrode including a conductive material and a first p-type dopant. [Effects of the Invention]

[0014] The present disclosure provides electronic devices with improved device performance. [Brief explanation of the drawings]

[0015] [Figure 1] FIG. 1 shows a cross-sectional view of a schematic configuration of a solar cell 100 according to a first embodiment. [Figure 2] FIG. 2 shows a cross-sectional view of a schematic configuration of a solar cell 200 according to the first embodiment. [Figure 3] FIG. 3 shows a cross-sectional view of a schematic configuration of a solar cell 300 according to the second embodiment. [Figure 4] FIG. 4 shows a cross-sectional view of a schematic configuration of a solar cell 400 according to the second embodiment. DETAILED DESCRIPTION OF THE INVENTION

[0016] Hereinafter, embodiments of the present disclosure will be described with reference to the drawings.

[0017] (First embodiment) The electronic device according to the first embodiment comprises, in this order, a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode, the second electrode including a conductive material and a first p-type dopant.

[0018] In this specification, a p-type dopant refers to a material that functions as an acceptor when added to a hole transport material that constitutes a hole transport layer, i.e., a material that has the function of extracting electrons in the valence band from the hole transport material.

[0019] According to the above configuration, it is possible to prevent a decrease in the concentration of holes in the hole transport layer, thereby improving the performance of the electronic device according to the first embodiment.

[0020] As used herein, a hole transport material is a material that allows the injection and emission of holes and rejects the injection and emission of electrons.

[0021] The conductive material that constitutes the electrodes is a material that allows the injection and emission of holes and electrons.

[0022] The electronic device according to the first embodiment may further include a substrate.

[0023] The electronic device according to the first embodiment may further include an electron transport layer disposed between the first electrode and the photoelectric conversion layer.

[0024] The electronic device according to the first embodiment is not particularly limited as long as it is an electronic device including a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode in this order. The electronic device according to the first embodiment is, for example, a solar cell, a light-emitting element, or a photosensor. The electronic device according to the first embodiment may be, for example, a solar cell.

[0025] An example of the configuration when the electronic device according to the first embodiment is a solar cell will be described with reference to FIGS.

[0026] FIG. 1 shows a cross-sectional view of a schematic configuration of a solar cell 100 according to a first embodiment.

[0027] The solar cell 100 comprises a substrate 1, a first electrode 2, an electron transport layer 3, a photoelectric conversion layer 4, a hole transport layer 5, and a second electrode 6 in this order.

[0028] The electronic device of the present disclosure may further include an auxiliary electrode electrically connected to the second electrode.

[0029] FIG. 2 shows a cross-sectional view of a schematic configuration of a solar cell 200 according to the first embodiment.

[0030] Solar cell 200 has a configuration in which an auxiliary electrode 7 is added to solar cell 100. Specifically, solar cell 200 includes a substrate 1, a first electrode 2, an electron transport layer 3, a photoelectric conversion layer 4, a hole transport layer 5, a second electrode 6, and an auxiliary electrode 7, in this order.

[0031] (Substrate 1) The substrate 1 serves to support each layer of the solar cell and is made of a stable material that will not corrode or disappear during the process of forming the first electrode 2, the photoelectric conversion layer 4, the hole transport layer 5, and the second electrode 6 on the substrate 1.

[0032] When the solar cell generates power using light incident from the substrate side, the substrate 1 is made of a light-transmitting material.

[0033] The substrate 1 may be a ceramic substrate such as glass or a plastic substrate. The plastic substrate may be a plastic film.

[0034] If the first electrode 2 has sufficient strength, the layers of the solar cell can be held by the first electrode 2, and therefore the substrate 1 does not need to be provided.

[0035] (first electrode 2) The function of the first electrode 2 is to accept electrons generated in the photoelectric conversion layer 4 and extract them to the outside. The first electrode 2 has electrical conductivity. It is desirable that the first electrode 2 has low electrical resistance.

[0036] Examples of materials that form the first electrode 2 include metals, conductive compounds that exhibit electronic conductivity, and conductive carbon.

[0037] There are no restrictions on the metal, and almost all metals can be used.

[0038] If light transmission is required for the first electrode 2, a conductive compound with light transmission properties is desirable. Examples of conductive compounds include indium, zinc, or tin oxide, titanium oxide and nitride, or organic conductors. Fluorine-doped tin oxide (SnO2:F), indium tin oxide (ITO), aluminum-doped zinc oxide (ZnO:Al), gallium-doped zinc oxide (ZnO:Ga), niobium-doped titanium oxide (TiO2:Nb), or barium tin oxide (BTO) have low volume resistivity and can therefore be used in outdoor solar cells that carry large currents. SnO2:F, ITO, ZnO:Al, ZnO:Ga, TiO2:Nb, and BTO are particularly useful for solar cells because they are also light-transmitting.

[0039] Examples of conductive carbon are carbon black, carbon nanotubes (CNT), graphene, or graphite. Ketjen black and acetylene black are materials classified as carbon black.

[0040] Examples of methods for manufacturing the first electrode 2 include vacuum film formation methods such as sputtering, vapor deposition, or ion plating, screen printing, spraying, or CVD (Chemical Vapor Deposition). CVD is a method for forming a film on the surface of the heated substrate 1 by spraying fine droplets of a special material liquid or gas onto the substrate 1. For example, the first electrode 2 may be formed on the substrate 1 by sputtering ITO so that the sheet resistance is approximately 10 Ω / □ or more and 40 Ω / □ or less.

[0041] (electron transport layer 3) The function of the electron transport layer 3 is to accept electrons in the conduction band of the photoelectric conversion layer 4 and conduct the electrons to the first electrode 2 while insulating holes in the valence band of the photoelectric conversion layer 4 .

[0042] Examples of materials that form the electron transport layer 3 include titanium oxide and tin oxide.

[0043] The electron transport layer 3 can be produced, for example, by spin-coating or spray-coating an alcohol dispersion (concentration: 1% by mass) containing TiO2 nanoparticles, and then heating to 100°C or higher to remove the alcohol. For example, the electron transport layer 3 may be produced by sputtering TiO2 onto the first electrode 2 to a thickness of 10 nm or more and 100 nm or less. Alternatively, the electron transport layer 3 may be produced by forming an aggregate of TiO2 nanoparticles to a thickness of approximately 100 nm or more and 500 nm or less.

[0044] (Photoelectric conversion layer 4) The function of the photoelectric conversion layer 4 is to receive light incident from the substrate side or the opposite side, generate electrons and holes, and diffuse the electrons and holes without recombining.

[0045] The photoelectric conversion layer 4 may contain a perovskite compound. The perovskite compound refers to a compound having a perovskite-type crystal structure represented by the composition formula ABX3 or a structure similar thereto. Here, A is a monovalent cation. Examples of the cation A are monovalent cations such as alkali metal cations or organic cations. Examples of the alkali metal cations include sodium cations (Na + ), potassium cation (K + ), cesium cation (Cs + ), or rubidium cation (Rb + ) An example of an organic cation is the methylammonium cation (CH3NH3 + ) or formamidinium cation (NH2CHNH2 +) B is a divalent metal cation. Examples of cation B are Pb cation, Sn cation, or Ge cation. X is a monovalent anion. Examples of anion X are halogen anions. Examples of halogen anions are iodine anions or bromine anions. Each site of cation A, cation B, and anion X may be occupied by multiple types of ions.

[0046] An example of a method for producing the photoelectric conversion layer 4 is to apply a solution in which a predetermined material is dissolved in an organic solvent, remove the organic solvent from the coating film, and then perform a heat treatment. The organic solvent can be removed from the coating film, for example, by evaporating the organic solvent by reducing the pressure, or by adding a solvent that is a poor solvent for the predetermined material dissolved in the organic solvent but is compatible with the organic solvent, thereby removing only the organic solvent from the coating film. This method is common. This method is simple and can produce a photoelectric conversion layer 4 with high performance. The photoelectric conversion layer 4 can also be produced by vacuum deposition.

[0047] (Hole transport layer 5) The function of the hole transport layer 5 is to accept only holes from the photoelectric conversion layer 4 and block electrons. The hole transport layer 5 contains a hole transport material. The hole transport material desirably has a HOMO (Highest Occupied Molecular Orbital) level close to the HOMO level of the photoelectric conversion layer 4 and a LUMO (Lowest Unoccupied Molecular Orbital) level higher than the LUMO level of the photoelectric conversion layer 4.

[0048] For example, in the case of a perovskite solar cell, the LUMO level of the photoelectric conversion layer 4 is around -4 eV, and the HOMO level is around -5 eV. Therefore, examples of hole transport materials include poly(bis(4-phenyl)(2,4,6-trimethylphenyl))amine (PTAA), N 2 ,N 2 ,N 2’ ,N 2’ ,N 7 ,N7 ,N 7’ ,N 7’ -octakis(4-methoxyphenyl)-9,9'-spirobi[9H-fluorene]-2,2',7,7'-tetramine (Spiro-OMeTAD), dithiophenebenzene copolymer (DTB), poly-3-hexylthiophene (P3HT), or poly-3-hexylthiophene-polystyrene block polymer (P3HT-b-PSt).

[0049] The hole transport layer 5 may contain at least one selected from the group consisting of PTAA, Spiro-OMeTAD, DTB, P3HT, and P3HT-b-PSt. Note that these materials alone may not provide sufficient hole density in the hole transport layer. Therefore, the hole transport layer 5 may contain not only a hole transport material but also an additive. The additive has the function of removing electrons from the valence band from the hole transport material. In other words, the hole transport layer 5 may contain a p-type dopant. The p-type dopant contained in the hole transport layer 5 is referred to as a second p-type dopant.

[0050] The second p-type dopant may be a material exemplified as the first p-type dopant contained in the second electrode 6, as described below. The hole transport layer 5 may contain, as the second p-type dopant, the same substance as the first p-type dopant contained in the second electrode 6, or a different substance. When the hole transport layer 5 and the second electrode 6 contain the same substance as the p-type dopant, the manufacturing process of the electronic device is not complicated. When the hole transport layer 5 and the second electrode 6 contain different substances as the p-type dopant, p-type dopants with different properties can be used in the electronic device, and the properties of each can be complemented. For example, when the hole transport layer 5 and the second electrode 6 contain a p-type dopant that is durable against light and a p-type dopant that is durable against heat, the light and heat durability of the electronic device can be improved.

[0051] The hole transport layer 5 may be formed by applying a solution of a hole transport material and a second p-type dopant in an organic solvent onto an underlying layer (e.g., onto the photoelectric conversion layer 4) and drying the solution. The organic solvent used for this is selected to be one that does not dissolve the first electrode 2, the electron transport layer 3, and the photoelectric conversion layer 4. Examples of such organic solvents include benzene, chlorobenzene, toluene, xylene, anisole, and mesitylene.

[0052] (Second electrode 6) The function of the second electrode 6 is to receive holes generated in the photoelectric conversion layer 4 and extract them to the outside.

[0053] The second electrode 6 includes a conductive material and a first p-type dopant.

[0054] The conductive material may be any of the materials exemplified for forming the first electrode 2. That is, examples of the conductive material include metals, conductive compounds exhibiting electronic conductivity, and conductive carbon. The conductive material may be carbon black or acetylene black.

[0055] The first p-type dopant may include at least one selected from the group consisting of a metal salt including a bis(trifluoromethanesulfonyl)imide group, a metal salt including a bis(fluorosulfonyl)imide group, a metal salt including a bis(pentafluoroethylsulfonyl)imide group, a metal salt including a 4,4,5,5-tetrafluoro-1,3,2-dithiazolidine-1,1,3,3-tetraoxide group, tris(pentafluorophenyl)borane (TPFPB), 2,3,5,6-tetrafluoro-7,7,8,8-tetracyanoquinodimethane (F4-TCNQ), SnCl4, SbCl5, FeCl3, and WO3.

[0056] The first p-type dopant may be at least one selected from the group consisting of a metal salt containing a bis(trifluoromethanesulfonyl)imide group, a metal salt containing a bis(fluorosulfonyl)imide group, a metal salt containing a bis(pentafluoroethylsulfonyl)imide group, a metal salt containing a 4,4,5,5-tetrafluoro-1,3,2-dithiazolidine-1,1,3,3-tetraoxide group, TPFPB, F4-TCNQ, SnCl4, SbCl5, FeCl3, and WO3.

[0057] The first p-type dopant may include at least one selected from the group consisting of lithium bis(trifluoromethanesulfonyl)imide (LiTFSI) and TFPPB. The first p-type dopant may be at least one selected from the group consisting of LiTFSI and TFPPB.

[0058] According to the above configuration, it is possible to suppress a decrease in the dopant concentration in the hole transport layer 5 due to elution of the p-type dopant contained in the hole transport layer 5 into the second electrode 6. This makes it possible to suppress a decrease in the concentration of holes in the hole transport layer 5. As a result, the performance of the solar cell 100 or the solar cell 200 is improved.

[0059] The second electrode 6 may contain, as the first p-type dopant, the same substance as the second p-type dopant contained in the hole transport layer 5, or may contain a different substance.

[0060] The second electrode 6 may contain two or more kinds of the first p-type dopant.

[0061] The second electrode 6 does not need to contain the first p-type dopant uniformly. The second electrode 6 may include a dopant layer and a conductive layer. The dopant layer includes the first p-type dopant. The dopant layer may include a conductive material. The conductive layer includes a conductive material and is substantially free of the first p-type dopant. Here, the dopant layer may be disposed between the hole transport layer 5 and the conductive layer, or the positions of the dopant layer and the conductive layer may be reversed. That is, the conductive layer may be disposed between the hole transport layer 5 and the dopant layer. The concentration of the first dopant in the dopant layer does not need to be uniform throughout the layer.

[0062] "The conductive layer is substantially free of the first p-type dopant" means that the conductive layer does not contain the first p-type dopant as a constituent component, except for the first p-type dopant inevitably mixed in as an impurity. The first p-type dopant inevitably mixed in as an impurity refers to the first p-type dopant that has migrated from the hole transport layer 5 to the conductive layer during manufacturing or due to repeated use of the solar cell, for example. The amount of the first p-type dopant mixed in as an impurity in the conductive layer is, for example, 0.1 mass % or less.

[0063] The second electrode 6 may consist of a dopant layer and a conductive layer.

[0064] The dopant layer may be in contact with the hole transport layer 5. This can further prevent a decrease in the dopant concentration in the hole transport layer 5 due to elution of the p-type dopant contained in the hole transport layer 5 into the second electrode 6, and as a result, can prevent a decrease in the hole concentration.

[0065] In the second electrode 6, the concentration of the first p-type dopant may be 0.4 mass% or more and less than 100 mass%, 0.4 mass% or more and 80 mass% or less, 0.4 mass% or more and less than 78 mass%, or 0.4 mass% or more and 77.7 mass% or less. This configuration can further suppress a decrease in the dopant concentration in the hole transport layer 5 and a decrease in the hole concentration in the hole transport layer 15. As a result, the performance of the electronic device can be improved.

[0066] When the first p-type dopant in the second electrode 6 is LiTFSI, the concentration of the dopant may be 0.8% by mass or more and less than 100% by mass, 0.8% by mass or more and less than 78% by mass, 1.7% by mass or more and less than 100% by mass, or 1.7% by mass or more and less than 78% by mass. This configuration can suppress a decrease in the dopant concentration in the hole transport layer 5 and a decrease in the hole concentration in the hole transport layer 15. As a result, the performance of the electronic device can be improved.

[0067] When the first p-type dopant in the second electrode 6 is TPFPB, the concentration of the dopant may be 0.4% by mass or more and less than 100% by mass, or 0.4% by mass or more and less than 78% by mass. This configuration can suppress a decrease in the dopant concentration in the hole transport layer 5 and a decrease in the hole concentration in the hole transport layer 15. As a result, the performance of the electronic device can be improved.

[0068] The second electrode 6 is substantially free of a hole transport material. Here, "the second electrode 6 is substantially free of a hole transport material" means that the second electrode 6 does not contain a hole transport material as a constituent component, except for a hole transport material inevitably mixed in as an impurity. The hole transport material inevitably mixed in as an impurity is, for example, a hole transport material that has migrated from the hole transport layer 5 to the second electrode 6 during production or due to repeated use of the solar cell. The amount of the hole transport material mixed in as an impurity in the second electrode 6 is, for example, 0.1 mass % or less.

[0069] The second electrode 6 may contain a binder. When the second electrode 6 is manufactured by applying an ink-like material, the second electrode 6 contains a binder, which can reduce the resistance and increase the durability of the second electrode.

[0070] Examples of binders include polyvinylidene fluoride, polytetrafluoroethylene, polyhexafluoropropylene, polyethylene, polypropylene, polymethyl methacrylate, polyvinyl chloride, polyvinylidene chloride, polyvinyl acetate, polyacrylic acid, polyvinyl butyral, polyacrylamide, polyurethane, polydimethylsiloxane, epoxy resin, acrylic resin, polyester resin, melamine resin, phenolic resin, various rubbers, lignin, pectin, gelatin, xanthan gum, welan gum, succinoglycan, polyvinyl alcohol, polyvinyl acetal, cellulose-based resin, polyalkylene oxide, polyvinyl ether, polyvinylpyrrolidone, chitins, chitosans, and starch.

[0071] When the second electrode 6 is formed by coating an ink-like material, a solvent that does not dissolve the material to be coated is selected for the ink-like material. That is, a solvent that does not corrode the hole transport layer 5, the photoelectric conversion layer 4, the first electrode 2, and the substrate 1 is selected.

[0072] Examples of solvents that are effective in perovskite solar cells and organic thin film solar cells include 1-propanol, 2-propanol, 1-butanol, 2-butanol, 1-pentanol, 2-pentanol, 3-pentanol, hexanol, heptanol, octanol, nonanol, decanol, undecanol, dodecanol, 1,2-propanediol, 1,3-propanediol, 1,2-pentanediol, 1,3-pentanediol, hexane, heptane, hexane ... Cetane, nonane, decane, undecane, dodecane, hexamethyldisiloxane, hexamethoxydisiloxane, 1,1,3,3-tetramethyldisiloxane, 1,1,3,3,5,5,7,7,9,9,11,11-dodecamethylhexasiloxane, 1,1,5,5-tetramethyl-3,3-diphenyltrisiloxane, 1,1,1,3,3-pentamethyldisiloxane, methyl acetate, ethyl acetate, propyl acetate, butyl acetate, methyl cellosolve, ethyl cellosolve , propyl cellosolve, butyl cellosolve, dimethyl cellosolve, phenyl cellosolve, diisopropyl ether, ethylene glycol monoethyl ether acetate, propylene glycol monomethyl ether acetate, diethylene glycol monobutyl ether acetate, diethylene glycol monoethyl ether acetate, diethylene glycol monomethyl ether, diethylene glycol monoethyl ether, diethylene glycol monobutyl ether, propylene glycol monomethyl ether, propylene glycol monomethyl ether propionate, ethylene glycol dimethyl ether, diethylene glycol dimethyl ether, ethylene glycol diethyl ether, diethylene glycol diethyl ether, triethylene glycol dimethyl ether, diethylene glycol dibutyl ether, tetraethylene glycol dimethyl ether, or dipropylene glycol dimethyl ether.

[0073] The second electrode 6 does not need to be formed simultaneously with the conductive material and the first p-type dopant. For example, the second electrode 6 may be formed by first forming a layer containing the conductive material and then subsequently incorporating the first p-type dopant. In this case, the layer containing the conductive material may have a porous structure. This structure has the advantage of making it easier to incorporate the dopant later. That is, the second electrode 6 may be formed by forming a layer containing the conductive material, followed by immersion in a solution containing the first p-type dopant and drying, or by vapor deposition of the dopant.

[0074] 1 has an exposed first electrode 2 as a negative electrode. To expose the first electrode 2 in this manner, the electron transport layer 3, photoelectric conversion layer 4, hole transport layer 5, and second electrode 6 are removed from the portions where the first electrode 2 is to be exposed, for example, by laser scribing using laser irradiation or mechanical scribing using a metal blade. This completes the solar cell as a device.

[0075] If the resistance of the second electrode 6 is high, an auxiliary electrode 7 may be formed on the second electrode 6, as in the solar cell 200 shown in Fig. 2. The function of the auxiliary electrode 7 is to extract the current from the second electrode 6 to the outside with minimal loss. The auxiliary electrode 7 may be made of a low-resistance material.

[0076] (Second embodiment) An electronic device according to the second embodiment will be described below. The matters described in the first embodiment may be omitted as appropriate.

[0077] The electronic device according to the second embodiment includes a substrate, a second electrode, a hole transport layer, a photoelectric conversion layer, and a first electrode, in this order. The second electrode contains a first p-type dopant.

[0078] According to the above configuration, it is possible to prevent the concentration of holes in the hole transport layer from decreasing, thereby improving the performance of the electronic device according to the second embodiment.

[0079] The electronic device according to the second embodiment may be, for example, a solar cell.

[0080] An example of the configuration when the electronic device according to the second embodiment is a solar cell will be described with reference to FIGS.

[0081] FIG. 3 shows a cross-sectional view of a schematic configuration of a solar cell 300 according to the second embodiment.

[0082] The solar cell 300 includes a substrate 11, a second electrode 16, a hole transport layer 15, a photoelectric conversion layer 14, an electron transport layer 13, and a first electrode 12 in this order.

[0083] FIG. 4 shows a cross-sectional view of a schematic configuration of a solar cell 400 according to the second embodiment.

[0084] Solar cell 400 has a configuration in which an auxiliary electrode 17 is added to solar cell 300. Specifically, solar cell 400 includes a substrate 11, an auxiliary electrode 17, a second electrode 16, a hole transport layer 15, a photoelectric conversion layer 14, an electron transport layer 13, and a first electrode 12, in this order.

[0085] Since the solar cell 400 includes the auxiliary electrode 17, the current from the second electrode 16 can be extracted to the outside with little loss.

[0086] The substrate 11 has the same configuration as the substrate 1 described in the first embodiment. The auxiliary electrode 17 has the same configuration as the auxiliary electrode 7 described in the first embodiment. The hole transport layer 15 has the same configuration as the hole transport layer 5 described in the first embodiment. The photoelectric conversion layer 14 has the same configuration as the photoelectric conversion layer 4 described in the first embodiment. The electron transport layer 13 has the same configuration as the electron transport layer 3 described in the first embodiment. The first electrode 12 has the same configuration as the first electrode 2 described in the first embodiment.

[0087] The function of the second electrode 16 is to accept holes from the hole transport layer 15 and extract them to the outside. The second electrode 16 includes a conductive material and a first p-type dopant. The conductive material applicable to the second electrode 16 is the same as the material exemplified for the first electrode 2 described in the first embodiment. That is, examples of the conductive material are metals, conductive compounds exhibiting electronic conductivity, or conductive carbon. The conductive material may be carbon black or acetylene black.

[0088] The above configuration can prevent a decrease in the concentration of holes in the hole transport layer 15. As a result, the performance of the solar cell 300 or the solar cell 400 is improved.

[0089] The second electrode 16 may contain, as a first p-type dopant, the same material as a second p-type dopant that may be contained in the hole transport layer 15 formed on the second electrode 16, or may contain a different material.

[0090] The second electrode 16 may include two or more first p-type dopants.

[0091] The second electrode 16 does not need to uniformly contain the first p-type dopant. The second electrode 16 may include a dopant layer and a conductive layer. The dopant layer includes the first p-type dopant. The dopant layer may include a conductive material. The conductive layer includes a conductive material and is substantially free of the first p-type dopant. Here, the dopant layer may be disposed between the hole transport layer 15 and the conductive layer, or the positions of the dopant layer and the conductive layer may be reversed. That is, the conductive layer may be disposed between the hole transport layer 15 and the dopant layer. The dopant concentration in the dopant layer does not need to be uniform throughout the layer.

[0092] The second electrode 6 may consist of a dopant layer and a conductive layer.

[0093] In the second electrode 16, the concentration of the first p-type dopant may be 0.4 mass% or more and less than 100 mass%, 0.4 mass% or more and 80 mass% or less, 0.4 mass% or more and less than 78 mass%, or 0.4 mass% or more and 77.7 mass% or less. With the above configuration, a decrease in the second dopant concentration in the hole transport layer 15 can be further suppressed, and a decrease in the hole concentration in the hole transport layer 15 can be further suppressed. As a result, the performance of the electronic device can be improved.

[0094] In the second electrode 16, the first p-type dopant is LiTFSI, and the concentration of the dopant may be 0.8 mass % or more and less than 100 mass %, 0.8 mass % or more and less than 78 mass %, 1.7 mass % or more and less than 100 mass %, or 1.7 mass % or more and less than 78 mass %. This configuration can suppress a decrease in the dopant concentration in the hole transport layer 15, and a decrease in the hole concentration in the hole transport layer 15. As a result, the performance of the electronic device can be improved.

[0095] In the second electrode 16, the first p-type dopant is TPFPB, and the concentration of the dopant may be 0.4 mass % or more and less than 100 mass %, or 0.4 mass % or more and less than 78 mass %. This configuration can suppress a decrease in the dopant concentration in the hole transport layer 15, and can suppress a decrease in the hole concentration in the hole transport layer 15. As a result, the performance of the electronic device can be improved.

[0096] The second electrode 16 may contain a binder, similar to the second electrode 6. When the second electrode 16 is produced by applying an ink-like material, a solvent for the ink-like material is selected that does not corrode the substrate 11, for example.

[0097] The method for manufacturing the hole transport layer 15 is the same as that described in the first embodiment.

[0098] An example of a method for manufacturing the photoelectric conversion layer 14 is to apply a solution in which a predetermined material is dissolved in an organic solvent, evaporate and remove the organic solvent by reducing the pressure, and then perform a heat treatment.

[0099] The electron transport layer 13 may be formed, for example, by sputtering TiO2 or SnO2. Alternatively, the electron transport layer 13 may be formed by spin-coating or spray-coating an alcohol dispersion (concentration: 1% by mass) containing TiO2 nanoparticles, heating to 100°C or higher to remove the alcohol, and then sputtering TiO2 or SnO2.

[0100] The first electrode 12 can be formed by vacuum deposition such as sputtering or evaporation of indium tin oxide (ITO), Al-doped zinc oxide (ZnO:Al), Ga-doped zinc oxide (ZnO:Ga), Nb-doped titanium oxide (TiO:Nb), or barium tin oxide (BTO). [Example]

[0101] The present disclosure will now be described in more detail with reference to examples. In the examples, perovskite solar cells were fabricated and their device performance was evaluated.

[0102] (Examples 1 to 9) The methods for producing the solar cells according to Examples 1 to 9 will be described below.

[0103] A 25 mm square, 0.7 mm thick glass substrate was prepared. Indium tin oxide (ITO) was sputtered onto one side of the glass to give a sheet resistance of 10 Ω / □. In this way, a first electrode was formed on the substrate.

[0104] Titanium oxide (TiO2) was formed on the first electrode by sputtering to a thickness of 30 nm.

[0105] Furthermore, an aggregate of TiO2 nanoparticles was formed to a thickness of 250 nm, thus forming an electron transport layer on the first electrode.

[0106] Next, a raw material solution for the photoelectric conversion layer was prepared. The raw material solution was prepared by dissolving 2.91 g of formamidinium hydroiodide ((NH2)2CH2I), 0.57 g of methylammonium hydroiodide (CH3NH3I), and 10 g of lead iodide (PbI2) in a mixed solvent of 23.3 mL of N,N-dimethylformamide (DMF) and 5.8 mL of dimethyl sulfoxide (DMSO). The raw material solution (80 μL) was dropped onto the electron transport layer, and the substrate containing the electron transport layer was spun at 4000 rpm for 70 seconds using a spin coater. Thirty to 60 seconds after the start of rotation, 1 mL of toluene was dropped onto the rotating electron transport layer onto which the raw material solution had been dropped using a pipette. The substrate was then heated on a hot plate at 115°C for 30 minutes. In this way, a photoelectric conversion layer was formed on the electron transport layer.

[0107] Next, a hole transport material solution was prepared by adding 4.8 μL of a solution of 500 mg of LiTFSI in 1 mL of acetonitrile to a solution of 10 mg of PTAA and 6 μL of tert-butylpyridine in 1 mL of toluene. The hole transport layer was formed by dropping 60 μL of the hole transport material solution onto the photoelectric conversion layer and spinning it at 4000 rpm for 30 seconds using a spin coater.

[0108] 500 μL of carbon ink was dropped onto the hole transport layer, spun at 1000 rpm for 30 seconds using a spin coater, and then heated on a hot plate at 100°C for 2 hours. The carbon ink was prepared by placing 9 parts by weight of acetylene black and 1 part by weight of cellulose in a bead mill, adding the amount of 2-propanol listed in Table 1, and stirring. The amount of LiTFSI or TFPPB listed in Table 1 was then added as a p-type dopant. In this way, a second electrode was formed on the hole transport layer. A 200 nm thick layer of Au was then formed on the second electrode by vapor deposition. In this way, an auxiliary electrode was formed.

[0109] In this manner, the solar cells according to Examples 1 to 9 were fabricated.

[0110] (Comparative Example 1) A solar cell of Comparative Example 1 was fabricated in the same manner as in Examples 1 to 9, except that no p-type dopant was added to the carbon ink dropped onto the hole transport layer.

[0111] (Measurement of the mass of the second electrode) The second electrode was peeled off with a metal blade, and its mass was measured with an electronic balance.

[0112] (Measurement of the mass of LiTFSI contained in the second electrode) The peeled off second electrode fragment was placed in a platinum crucible and heated to 800°C in an electric furnace for 1 hour to incinerate it. A small amount of nitric acid was added to the residue and dissolved by heating. After diluting it with pure water, the amount of Li was determined by inductively coupled plasma atomic emission spectroscopy (ICP-AES) using an inductively coupled plasma atomic emission spectrometer (Thermo Fisher Scientific, iCAP7400Duo), and the estimated mass of LiTFSI was calculated.

[0113] (Measurement of the mass of TPFPB contained in the second electrode) In the same manner as above, the amount of B was determined by inductively coupled plasma atomic emission spectroscopy (ICP-AES), and the estimated mass of TPFPB was calculated.

[0114] The concentration of the p-type dopant in the second electrode of the solar cell was calculated from the measured mass. Here, the concentration of the p-type dopant in the second electrode is the mass fraction of the first p-type dopant in the second electrode. Table 1 shows the concentrations of the p-type dopant in the second electrode of the solar cells of Examples 1 to 9.

[0115] (Rating 1) The characteristics of the fabricated solar cells of Examples 1 to 9 and Comparative Example 1 were evaluated under fluorescent light. The solar cells were irradiated with fluorescent light (illuminance 200 lx) so that light was incident on the glass substrate side, and a light-shielding mask with an aperture of 0.4 cm × 0.25 cm was attached to the glass surface to define the light-receiving area. A source meter (6246, manufactured by ADC Corporation) was used to measure the current at an operating voltage of 0.6 V. Hereinafter, the operating voltage will also be referred to as "Vop." Table 1 shows the current values ​​at Vop = 0.6 V and an illuminance of 200 lx for the solar cells of Examples 1 to 9 and Comparative Example 1.

[0116] (Rating 2) The characteristics of the solar cells fabricated in Examples 1 to 9 and Comparative Example 1 were evaluated under simulated sunlight. The solar cells were irradiated with 1 sun's light from a solar simulator through a light-shielding mask with an aperture of 0.4 cm x 0.25 cm, with light incident from the glass substrate side. A source meter (6246, manufactured by ADC Corporation) was used to measure the voltage-current characteristics in the voltage range of -0.2 V to +1.2 V, and the output at the maximum output point was determined. The maximum output of the solar cells in Examples 1 to 9 and Comparative Example 1 is shown in Table 1.

[0117] [Table 1]

[0118] (Consideration 1) As shown in Table 1, the current values ​​in Evaluation 1 and the maximum output values ​​in Evaluation 2 of Examples 1 to 7 are greater than those of Comparative Example 1. The inclusion of LiTFSI, a p-type dopant, in the second electrode improves the characteristics of the solar cell. Furthermore, the characteristics of the solar cell are improved when the LiTFSI concentration in the second electrode is in the range of 0.4 mass % to 77.7 mass %.

[0119] The current values ​​in Evaluation 1 and the maximum output values ​​in Evaluation 2 of Examples 8 and 9 were greater than those of Comparative Example 1. This shows that the solar cell characteristics are improved even when the p-type dopant contained in the hole transport layer is LiTFSI and the p-type dopant contained in the second electrode is TPFPB. In other words, it was shown that the p-type dopant contained in the second electrode is not limited to the dopant contained in the hole transport layer and may be a different material.

[0120] Examples 10 to 18 The following describes the method for producing the solar cells of Examples 10 to 18. Except for the hole transport layer and the second electrode, the solar cells were produced in the same manner as in Examples 1 to 9, and therefore, the description will be omitted.

[0121] The hole transport layer was formed by dropping 60 μL of hole transport material solution onto the photoelectric conversion layer and spinning it at 4000 rpm for 30 seconds using a spin coater. The hole transport material solution was obtained by placing 0.1 g of PTAA in a glass container, adding 10 mL of TFPPB solution obtained by dissolving 1 g of TFPPB powder in 10 mL of toluene, and shaking for 2 hours. That is, the hole transport layers in Examples 10 to 18 differ from Examples 1 to 9 in that the p-type dopant contained therein was TFPPB.

[0122] 500 μL of carbon ink was dropped onto the hole transport layer, spun at 1000 rpm for 30 seconds using a spin coater, and then heated on a hot plate at 100°C for 2 hours. The carbon ink was prepared by placing 9 parts by weight of acetylene black and 1 part by weight of cellulose in a bead mill, adding the amount of 2-propanol listed in Table 2, and stirring. The amount of LiTFSI or TFPPB listed in Table 1 was then added as a p-type dopant. In this way, a second electrode was formed on the hole transport layer. A 200 nm thick layer of Au was then formed on the second electrode by vapor deposition. In this way, an auxiliary electrode was formed.

[0123] (Comparative Example 2) The solar cell of Comparative Example 2 was fabricated in the same manner as in Examples 10 to 18, except that no p-type dopant was added to the carbon ink dropped onto the hole transport layer.

[0124] (Measurement of the mass of the p-type dopant contained in the second electrode) The masses of LiTFSI and TPFPB contained in the second electrodes of the solar cells of Examples 10 to 18 were measured, and the concentrations of the p-type dopants in the second electrodes were calculated in the same manner as in Examples 1 to 9. Table 2 shows the concentrations of the p-type dopants in the second electrodes of the solar cells of Examples 10 to 18.

[0125] (Rating 3) The characteristics of the solar cells fabricated in Examples 10 to 18 and Comparative Example 2 were evaluated under fluorescent light. The solar cells were irradiated with fluorescent light (illuminance 200 lx) so that light was incident on the glass substrate side, and a light-shielding mask with an aperture of 0.4 cm × 0.25 cm was attached to the glass surface to define the light-receiving area. A source meter (6246, manufactured by ADC Corporation) was used to measure the current at an operating voltage of 0.6 V. Table 2 shows the current values ​​at an illuminance of 200 lx and Vop = 0.6 V for the solar cells of Examples 10 to 18 and Comparative Example 2.

[0126] (Rating 4) The characteristics of the fabricated solar cell devices of Examples 10 to 18 and Comparative Example 2 were evaluated under simulated sunlight. The solar cells were irradiated with 1 sun's light from a solar simulator through a 0.4 cm x 0.25 cm light-shielding mask so that light was incident on the glass substrate side. A source meter (6246, manufactured by ADC Corporation) was used to measure the voltage-current characteristics over a voltage range of -0.2 V to +1.2 V, and the output at the maximum output point was determined. The maximum output of the solar cells of Examples 10 to 18 and Comparative Example 2 is shown in Table 2.

[0127] [Table 2]

[0128] (Consideration 2) As shown in Table 2, the values ​​of ratings 3 and 4 for Examples 10 to 16 are greater than the values ​​of ratings 1 and 2 for Comparative Example 2. The inclusion of TPFPB as a p-type dopant in the second electrode improves the solar cell characteristics. Furthermore, the solar cell characteristics are improved when the TPFPB concentration in the second electrode is in the range of 0.4 mass % to 77.7 mass %.

[0129] The current values ​​in Evaluation 3 and the maximum output values ​​in Evaluation 4 of Examples 17 and 18 are greater than those of Comparative Example 2. This indicates that the solar cell characteristics are improved even when the p-type dopant contained in the hole transport layer is TPFPB and the p-type dopant contained in the second electrode is LiTFSI. In other words, the p-type dopant contained in the second electrode is not limited to the p-type dopant contained in the hole transport layer, and may be a different material. Furthermore, Tables 1 and 2 indicate that the characteristics of the electronic device are improved when the second electrode contains a p-type dopant, regardless of the p-type dopant contained in the hole transport layer. [Industrial Applicability]

[0130] The electronic device of the present disclosure is useful because it exhibits improved performance in terms of initial and long-term reliability compared to conventional devices. [Explanation of symbols]

[0131] 1, 11 board 2, 12 First electrode 3, 13 Electron transport layer 4, 14 Photoelectric conversion layer 5, 15 Hole transport layer 6, 16 Second electrode 7, 17 Auxiliary electrode 100, 200, 300, 400 solar cells

Claims

1. a first electrode, a photoelectric conversion layer, a hole transport layer, and a second electrode in this order; the second electrode comprises a conductive material and a first p-type dopant; the conductive material is a metal, a conductive compound exhibiting electronic conductivity, or conductive carbon; the first p-type dopant is a material that functions as an acceptor for the hole transport material when added to the hole transport material constituting the hole transport layer, the second electrode comprises a dopant layer and a conductive layer and is substantially free of the hole transport material; the dopant layer includes the first p-type dopant and the conductive material; the conductive layer includes the conductive material and is substantially free of the first p-type dopant; the dopant layer is in contact with the hole transport layer; Solar cell.

2. The second electrode further comprises a binder. The solar cell according to claim 1 .

3. The hole transport layer is made of poly(bis(4-phenyl)(2,4,6-trimethylphenyl))amine, N 2 , N 2 , N 2’ , N 2’ , N 7 , N 7 , N 7’ , N 7’ -octakis(4-methoxyphenyl)-9,9'-spirobi[9H-fluorene]-2,2',7,7'-tetramine, dithiophenebenzene copolymer, poly-3-hexylthiophene, and poly-3-hexylthiophene-polystyrene block polymer, The solar cell according to claim 1 or 2.

4. The first p-type dopant may be a metal salt containing a bis(trifluoromethanesulfonyl)imide group, a metal salt containing a bis(fluorosulfonyl)imide group, a metal salt containing a bis(pentafluoroethylsulfonyl)imide group, a metal salt containing a 4,4,5,5-tetrafluoro-1,3,2-dithiazolidine-1,1,3,3-tetraoxide group, tris(pentafluorophenyl)borane, 2,3,5,6-tetrafluoro-7,7,8,8-tetracyanoquinodimethane, or SnCl 4 , SbCl 5 , FeCl 3 , and W.O. 3 At least one selected from the group consisting of: The solar cell according to claim 1 .

5. the first p-type dopant includes at least one selected from the group consisting of lithium bis(trifluoromethanesulfonyl)imide and tris(pentafluorophenyl)borane; The solar cell according to claim 4 .

6. In the second electrode, the concentration of the first p-type dopant is 0.4 mass% or more and less than 100 mass%. The solar cell according to claim 1 .

7. the concentration of the first p-type dopant is 0.4 mass% or more and 77.7 mass% or less; The solar cell according to claim 6 .

8. further comprising an electron transport layer; the electron transport layer is disposed between the first electrode and the photoelectric conversion layer; The solar cell according to any one of claims 1 to 7.

9. the hole transport layer comprises a second p-type dopant; The solar cell according to any one of claims 1 to 8.

10. further comprising an auxiliary electrode electrically connected to the second electrode; The solar cell according to any one of claims 1 to 9.

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