US20190148578A1 - Solar cell module - Google Patents
Solar cell module Download PDFInfo
- Publication number
- US20190148578A1 US20190148578A1 US16/249,000 US201916249000A US2019148578A1 US 20190148578 A1 US20190148578 A1 US 20190148578A1 US 201916249000 A US201916249000 A US 201916249000A US 2019148578 A1 US2019148578 A1 US 2019148578A1
- Authority
- US
- United States
- Prior art keywords
- solar cell
- layer
- encapsulant layer
- wavelength conversion
- cell module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/40—Properties of the layers or laminate having particular optical properties
- B32B2307/412—Transparent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/40—Properties of the layers or laminate having particular optical properties
- B32B2307/422—Luminescent, fluorescent, phosphorescent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/51—Elastic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/724—Permeability to gases, adsorption
- B32B2307/7242—Non-permeable
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/732—Dimensional properties
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2457/00—Electrical equipment
- B32B2457/12—Photovoltaic modules
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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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/10—Photovoltaic [PV]
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- Y02B10/12—
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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
- 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
-
- 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
- Y02E10/52—PV systems with concentrators
Definitions
- the present disclosure relates to a solar cell module.
- Patent Literature 1 discloses a solar cell module in which an encapsulant layer containing a wavelength conversion substance therein is disposed on the light receiving surface side of a solar cell.
- the wavelength conversion substance is preferably disposed on the light receiving surface side of the solar cell from a viewpoint of improvement of wavelength conversion efficiency.
- the wavelength conversion substance is diffused on the rear surface side of the solar cell by long term use of the solar cell module, and the concentration of the wavelength conversion substance on the light receiving surface side is reduced.
- An aspect of a solar cell module includes: a solar cell; a first protection member provided on a light receiving surface side of the solar cell; a second protection member provided on a rear surface side of the solar cell; an encapsulant layer that includes a first encapsulant layer disposed between the solar cell and the first protection member, and a second encapsulant layer disposed between the solar cell and the second protection member, and seals the solar cell; and a wavelength conversion substance that is contained in at least the first encapsulant layer, and that absorbs light having a specified wavelength, and converts the wavelength, wherein concentration of the wavelength conversion substance in the first encapsulant layer is higher than concentration of the wavelength conversion substance in the second encapsulant layer, and resin constituting the second encapsulant layer has a smaller diffusion coefficient of the wavelength conversion substance than the diffusion coefficient of resin constituting the first encapsulant layer.
- a diffusion inhibiting layer constituted from a material having a smaller diffusion coefficient of the wavelength conversion substance than the diffusion coefficient of resin constituting the first encapsulant layer is provided between the first encapsulant layer and the second encapsulant layer.
- a wavelength conversion substance disposed on the light receiving surface side of a solar cell can be inhibited from being diffused on the rear surface side of the solar cell.
- FIG. 1 is a sectional view of a solar cell module of a first embodiment.
- FIG. 2 is a sectional view of a solar cell panel constituting the solar cell module of the first embodiment (wiring materials are omitted).
- FIG. 3 is a sectional view of a solar cell panel constituting a solar cell module of a second embodiment (wiring materials are omitted).
- FIG. 4 is a plan view illustrating an extracted diffusion inhibiting layer of FIG. 3 .
- FIG. 5 is a sectional view of a solar cell panel constituting a solar cell module of a third embodiment (wiring materials are omitted).
- a “light receiving surface” of each of a solar cell module, a solar cell, and a photoelectric conversion section means a surface on which light is mainly incident (incident from a light receiving surface upon which 50% to 100% of light is incident), while a “rear surface” means a surface opposite to the light receiving surface.
- description that “a second member is provided on a first member” does not means only a case where the first and second members are provided so as to be in direct contact with each other, unless otherwise mentioned. That is, this description includes a case where another member exists between the first and second members.
- Description of “substantial . . . ” is intended to include not only “entirely identical” but also “substantially the same”, when “substantially the same” is taken as an example.
- FIG. 1 is a sectional view of the solar cell module 10 which is an example of the embodiment.
- the solar cell module 10 includes solar cells 11 , a first protection member 12 provided on the light receiving surface side of the solar cells 11 , a second protection member 13 provided on the rear surface side of the solar cells 11 , and an encapsulant layer 14 that seals the solar cells 11 .
- the encapsulant layer 14 includes an encapsulant layer 14 a (first encapsulant layer) disposed between the solar cells 11 and the first protection member 12 , and an encapsulant layer 14 b (second encapsulant layer) disposed between the solar cells 11 and the second protection member 13 .
- the solar cell module 10 includes wavelength conversion substances 30 contained in at least the encapsulant layer 14 a (refer to FIG. 2 and the like described below).
- the wavelength conversion substances 30 are substances that absorb light having a specified wavelength to convert the wavelength, and play a role in converting light in a wavelength region hardly contributing to power generation into light in a wavelength region contributing greatly to power generation.
- a plurality of the solar cells 11 are disposed on substantially the same plane.
- the adjacent solar cells 11 are connected in series by wiring materials 15 , thereby forming a string of the solar cells 11 .
- each wiring material 15 bends in the module thickness direction between the adjacent solar cells 11 , and is mounted on an electrode on the light receiving surface side of one of the solar cells 11 and an electrode on the rear surface side of the other solar cell 11 by an adhesive or the like.
- the solar cells 11 , the first protection member 12 , the second protection member 13 , and the encapsulant layer 14 constitute a solar cell panel 16 .
- the solar cell panel 16 is a plate-like body in which a string of the solar cells 11 are disposed between the respective protection members, and has, for example, a substantially rectangular shape in plan view (when viewed from the direction perpendicular to the light receiving surface).
- a frame 17 is preferably mounted on an end edge of the solar cell panel 16 . The frame 17 protects the end edge of the solar cell panel 16 , and is utilized when the solar cell module 10 is installed on a roof or the like.
- the solar cells 11 each include a photoelectric conversion section that generates carriers by receiving light.
- Each solar cell 11 has a light receiving surface electrode formed on the light receiving surface of the photoelectric conversion section and a rear surface electrode formed on a rear surface, as electrodes for collecting the carriers generated in the photoelectric conversion section.
- the structure of each solar cell 11 is not limited to the above, and may be, for example, a structure in which an electrode is formed only on the rear surface of the photoelectric conversion section.
- the rear surface electrode is preferably formed to have a larger area than the light receiving surface electrode, and it can be said that the surface having a lager electrode area (or a surface with an electrode formed thereon) is the “rear surface” of the solar cell 11 .
- the photoelectric conversion section has, for example, a semiconductor substrate, an amorphous semiconductor layer formed on the substrate, and a transparent conductive layer formed on the amorphous semiconductor layer.
- a semiconductor constituting the semiconductor substrate can include crystalline silicon (c-Si), gallium arsenide (GaAs), indium phosphide (InP) and the like.
- Examples of an amorphous semiconductor constituting the amorphous semiconductor layer can include an i-type amorphous silicon, an n-type amorphous silicon, a p-type amorphous silicon, and the like.
- the transparent conductive layer is preferably formed of transparent conductive oxide in which tin (Sn), antimony (Sb) or the like is doped in metal oxide such as indium oxide (In 2 O 3 ) and zinc oxide (ZnO).
- an n-type single crystal silicon substrate is applied to the semiconductor substrate.
- the photoelectric conversion section has a structure in which an i-type amorphous silicon layer, a p-type amorphous silicon layer, and a transparent conductive layer are sequentially formed on the light receiving surface of the n-type single crystal silicon substrate, and an i-type amorphous silicon layer, an n-type amorphous silicon layer, and a transparent conductive layer are sequentially formed on the rear surface of the substrate.
- the p-type amorphous silicon layer may be formed on the rear surface side of the n-type single crystal silicon substrate, and the n-type amorphous silicon layer may be formed on the light receiving surface side of the substrate.
- the photoelectric conversion section has a junction of semiconductors having different optical gaps (heterojunction).
- An amorphous silicon layer (thickness: several nm to several tens of nm) forming a heterojunction generally absorbs light having a wavelength of 600 nm or less.
- the first protection member 12 a member having transparency such as a glass substrate, a resin substrate and a resin film can be used.
- the glass substrate is preferably used.
- the thickness of the glass substrate is not particularly limited, but is preferably about 2 mm to 6 mm.
- a transparent member which is the same as the first protection member 12 may be used, or an opaque member may be used.
- a resin film is used as the second protection member 13 .
- the resin film is not particularly limited, but is preferably a polyethylene terephthalate (PET) film. From a viewpoint of lowering moisture permeability and the like, in the resin film, an inorganic compound layer of silica or the like, or a metal layer of aluminum or the like may be formed in a case where it is not assumed that light is incident from the rear surface side.
- the thickness of the resin film is not particularly limited, but is preferably about 50 ⁇ m to 300 ⁇ m.
- the encapsulant layer 14 plays a role in preventing moisture and the like from coming into contact with the solar cells 11 .
- the encapsulant layer 14 is also called a sealing layer (sealant).
- the encapsulant layer 14 is formed, for example, by a lamination step described below, by use of two respective resin sheets constituting the encapsulant layers 14 a, 14 b. In this embodiment, the encapsulant layers 14 a, 14 b are closely adhered to each other between the solar cells 11 , and between ends of the solar cell panel 16 and the solar cells 11 near the ends.
- the thickness of the encapsulant layer 14 is not particularly limited, and the thickness of each of the encapsulant layers 14 a, 14 b is preferably about 100 ⁇ m to 600 ⁇ m.
- FIG. 2 is a sectional view of the solar cell panel 16 .
- the wavelength conversion substances 30 are illustrated by white circles.
- the wavelength conversion substances 30 are contained in the encapsulant layer 14 a provided on at least the light receiving surface side of the solar cells 11 . That is, the wavelength conversion substances 30 may be contained only in the encapsulant layer 14 a (in this case, the concentration of the wavelength conversion substances 30 satisfies, of course, concentration in encapsulant layer 14 a >concentration in encapsulant layer 14 b ). The wavelength conversion substances 30 may be contained in the encapsulant layer 14 b provided on the rear surface side of the solar cells 11 , but the concentration of the wavelength conversion substances 30 in the encapsulant layer 14 a is higher than the concentration of the wavelength conversion substances 30 in the encapsulant layer 14 b.
- the concentration of the wavelength conversion substances 30 in the encapsulant layer 14 a is, for example, 0.1 weight percent to 15 weight percent, and more preferably 1.5 weight percent to 10 weight percent.
- the concentration of the wavelength conversion substances 30 is, for example, 0.02 weight percent to 2.0 weight percent, and more preferably 0.05 weight percent to 0.8 weight percent.
- Resin constituting the encapsulant layer 14 is preferably excellent in adhesion to the respective protection members and the solar cells 11 , and highly impermeable to moisture. More specifically, examples of the resin constituting the encapsulant layer include olefin based resin obtained by polymerizing at least one selected from ⁇ -olefin of 2-20C (for example, a random or block copolymer of polyethylene, polypropylene, ethylene, and other ⁇ -olefin), ester-based resin (for example, polycondensate of polyol and polycarboxylic acid or acid anhydride/acid lower alkyl ester thereof), urethane-based resin (for example, a polyaddition product with polyisocyanate and active hydrogen-containing compounds (such as diol, polyol, dicarboxylic acid, polycarboxylic acid, polyamine, polythiol)), epoxy-based resin (for example, opening polymer of polyepoxid
- the resin constituting the encapsulant layer is particularly preferably olefin based resin (particularly, a polymer containing ethylene), and a copolymer of ⁇ -olefin and vinyl carboxylate.
- olefin based resin particularly, a polymer containing ethylene
- a copolymer of ⁇ -olefin and vinyl carboxylate As the copolymer of ⁇ -olefin and vinyl carboxylate, ethylene-vinyl acetate copolymer (EVA) is particularly preferable.
- EVA ethylene-vinyl acetate copolymer
- a combination of resin constituting the encapsulant layer 14 a hereinafter, sometimes referred to as “resin 14 a ”
- resin constituting the encapsulant layer 14 b herein 14 b
- the diffusion coefficient is a factor of proportionality which regulates the speed of diffusion appearing in Fick's laws of diffusion.
- the diffusion coefficient of the wavelength conversion substances 30 can be calculated by overlapping of a layer constituted from resin which contains the wavelength conversion substances 30 and which is to be measured, and an olefin based resin layer which does not contain the wavelength conversion substances 30 , and obtaining the outflow speed of the wavelength conversion substances 30 from the resin layer to be measured.
- the outflow speed can be obtained by quantity by Gas Chromatography, or transmission spectrum measurement.
- the diffusion coefficient of the wavelength conversion substances 30 is made to satisfy diffusion coefficient of resin 14 b ⁇ diffusion coefficient of resin 14 a, so that the wavelength conversion substances 30 contained in the encapsulant layer 14 a can be inhibited from being diffused into the encapsulant layer 14 b.
- the diffusion coefficient of the wavelength conversion substances 30 in the resin 14 a is, for example, 1 ⁇ 10 ⁇ 12 to 1 ⁇ 10 ⁇ 10 (m 2 /s) at 120° C.
- the diffusion coefficient of the wavelength conversion substances 30 in the resin 14 b is, for example, 1 ⁇ 10 ⁇ 13 to 1 ⁇ 10 ⁇ 11 (m 2 /s) at 120° C.
- the resin 14 b preferably has a higher storage elastic modulus at 25° C. to 90° C. (hereinafter, simply referred to as a “storage elastic modulus”) than that of the resin 14 a .
- the storage elastic modulus is a ratio of elastic stress of the same phase as strain, and is represented by a real part of a complex modulus of elasticity. The larger a numeral value of the storage elastic modulus, the higher the elasticity of resin.
- the storage elastic modulus of each resin 14 a, 14 b can be measured by use of a dynamic viscoelasticity measuring device.
- the storage elastic modulus satisfies the relation storage elastic modulus of resin 14 b >storage elastic modulus of resin 14 a, so that the diffusion coefficient of the wavelength conversion substances 30 easily satisfies diffusion coefficient of resin 14 b ⁇ diffusion coefficient of resin 14 a.
- the storage elastic modulus (value at a frequency of 10 Hz in a tension mode at 25° C.) of the resin 14 a is preferably 1 ⁇ 10 7 to 1 ⁇ 10 8 (Pa), and the storage elastic modulus of the resin 14 b in the same condition is 1 ⁇ 10 8 to 1 ⁇ 10 9 (Pa).
- the resin 14 b preferably has a smaller intermolecular void size at 25° C. to 90° C. than that of the resin 14 a. In other words, the resin 14 b preferably has a smaller free volume at 25° C. to 90° C. than that of the resin 14 a.
- the intermolecular void size means size of a void part which is not occupied by molecules (atoms).
- the intermolecular void size of each resin 14 a, 14 b can be measured by use of a positron annihilation method.
- the intermolecular void size satisfies void size of resin 14 b ⁇ void size of resin 14 a, so that the diffusion coefficient of the wavelength conversion substances 30 easily satisfies void size of resin 14 b ⁇ void size of resin 14 a.
- the intermolecular void size of the resin 14 a is preferably 0.08 nm 3 to 0.12 nm 3
- the intermolecular void size of the resin 14 b is preferably 0.05 nm 3 to 0.09 nm 3 .
- the combination is not particularly limited.
- the following is an example of the combination.
- Example 1 resin 14 a; low-density polyolefin, resin 14 b : high-density polyolefin
- Example 2 resin 14 a; low molecular weight polyolefin, resin 14 b : high molecular weight polyolefin
- the wavelength conversion substances 30 absorb, for example, ultraviolet light which is light having a wavelength shorter than 380 nm, and convert the ultraviolet light into light having a longer wavelength (e.g., 400 nm to 800 nm). In this case, the wavelength conversion substances 30 contribute to inhibition of deterioration of component materials due to the ultraviolet light.
- the wavelength conversion substances 30 are preferably substances that absorb ultraviolet light to emit visible light, but may be substances that absorb visible light or infrared light. Generally, the wavelength conversion substances 30 convert light having a shorter wavelength into light having a longer wavelength, but may convert light having a longer wavelength into light having a shorter wavelength, namely, cause so-called up-conversion light emission.
- the preferable conversion wavelength varies depending on the type of the solar cells 11 .
- the solar cells 11 each have a heterojunction layer (amorphous semiconductor layer), and therefore the wavelength conversion substances 30 preferably absorb light having energy larger than a band gap of the heterojunction layer to convert the wavelength. That is, the wavelength conversion substances 30 preferably convert the light having the wavelength absorbed in the heterojunction layer.
- the wavelength conversion substances 30 are used to absorb light having a wavelength ⁇ ⁇ absorbed by an amorphous semiconductor layer and to convert the light having a wavelength ⁇ ⁇ into light having a wavelength ⁇ ⁇ which is not absorbed in the semiconductor layer.
- the wavelength ⁇ ⁇ is 600 nm or less.
- the wavelength conversion substances 30 include semiconductor nanoparticles (quantum dots), inorganic compounds such as a luminescent metal complex, and organic compounds such as an organic fluorescence dye.
- semiconductor nanoparticles can include zinc oxide (ZnO) nanoparticles, cadmium selenide (CdSe) nanoparticles, cadmium telluride (CdTe) nanoparticles, gallium nitride (GaN) nanoparticles, yttrium oxide (Y 2 O 3 ) nanoparticles, and indium phosphide (InP) nanoparticles.
- Examples of the luminescent metal complex can include Ir complexes such as [Ir(bqn) 3 ](PF 6 ) 3 , [Ir(dpbpy) 3 ](PF 6 ) 3 , Ru complexes such as [Ru(bqn) 3 ](PF 6 ) 3 , [Ru(bpy) 3 ](ClO 4 ) 2 , Eu complexes such as [Eu(FOD) 3 ]phen, [Eu(TFA) 3 ]phen, and Tb complexes such as [Tb(FOD) 3 ]phen, [Tb(HFA) 3 ]phen.
- Examples of the organic fluorescence dye can include a rhodamine dye, a coumarin dye, a fluorescein dye, and a perylene dye.
- the wavelength conversion substances 30 substantially uniformly disperse into, for example, the encapsulant layer 14 a.
- the encapsulant layer 14 a may contain ultraviolet light absorbing substances that absorb ultraviolet light and do not emit light. In this case, there may be an uneven concentration distribution of the wavelength conversion substances 30 in the encapsulant layer 14 a.
- the concentration of the wavelength conversion substances 30 near the first protection member 12 may be made higher than the concentration of the wavelength conversion substances 30 near the solar cells 11 .
- two or more kinds of the wavelength conversion substances 30 may be added to the encapsulant layer 14 a, or there may be an uneven concentration distribution of each wavelength conversion substance 30 in the encapsulant layer 14 a.
- the solar cell module 10 having the above configuration can be manufactured by laminating the string of the solar cells 11 connected by the wiring materials 15 by use of resin sheets constituting the first protection member 12 , the second protection member 13 , and the encapsulant layer 14 .
- a laminating device for example, the first protection member 12 , the resin sheet constituting the encapsulant layer 14 a, the string of the solar cells 11 , the resin sheet constituting the encapsulant layer 14 b, and the second protection member 13 are sequentially laminated on a heater.
- the resin sheet constituting the encapsulant layer 14 a contains the wavelength conversion substances 30 therein. This laminated body is heated to about 150° C., for example, in a vacuum state.
- the laminated body continues to be heated under atmospheric pressure while respective components are pressed onto the heater side, and the resin composition of the resin sheet is crosslinked, so that the solar cell panel 16 is obtained.
- the frame 17 and the like are mounted on the solar cell panel 16 , so that the solar cell module 10 is obtained.
- the wavelength conversion substances 30 in the encapsulant layer 14 a disposed on the light receiving surface side of the solar cells 11 can be inhibited from being diffused into the encapsulant layer 14 b disposed on the rear surface side of the solar cells 11 . That is, in the solar cell module 10 , the high concentration of the wavelength conversion substances 30 is maintained in the encapsulant layer 14 a upon which a large quantity of light is incident, for a long period. Consequently, it is possible to improve efficiency of utilization of incident light, and improve photoelectric conversion efficiency.
- FIG. 3 is a sectional view of a solar cell panel 51 constituting the solar cell module 50 .
- FIG. 4 is a plan view illustrating an extracted diffusion inhibiting layer 52 constituting the solar cell module 50 .
- differences from the first embodiment will be mainly described, with components similar to the components of the first embodiment being denoted by the same reference numerals, and repeated description omitted (the same applies to a third embodiment).
- the solar cell module 50 is different from the solar cell module 10 in that the diffusion inhibiting layer 52 which inhibits diffusion of wavelength conversion substances 30 is provided between an encapsulant layer 14 a and an encapsulant layer 14 b.
- the diffusion inhibiting layer 52 is preferably interposed between both layers over substantially the whole area such that the encapsulant layer 14 a is not in contact with the encapsulant layer 14 b.
- the diffusion inhibiting layer 52 is provided, for example, between voids of adjacent solar cells 11 , between ends of the solar cell panel 51 and the solar cells 11 near the ends.
- the diffusion inhibiting layer 52 is formed of a material having a smaller diffusion coefficient of the wavelength conversion substances 30 than that of the resin 14 a.
- the diffusion inhibiting layer 52 is formed by use of a resin sheet which does not have a metal layer and an inorganic compound layer, and a resin constituting the diffusion inhibiting layer 52 (hereinafter, sometimes referred to as “resin 52 ”) has wavelength conversion substances 30 of smaller diffusion coefficient than in the resin 14 a .
- the resin 52 preferably has a higher storage elastic modulus than that of the resin 14 a, and preferably a smaller intermolecular void size than that of the resin 14 a.
- the relation of the resin 14 a and the resin 52 is the same as the relation of the resin 14 a and the resin 14 b in the first embodiment, for example.
- the resin 52 preferably has wavelength conversion substances 30 of smaller diffusion coefficient than in the resin 14 b.
- the diffusion inhibiting layer 52 is formed of a resin sheet formed with through holes 53 at portions where the solar cells 11 are disposed, and the resin sheet is preferably provided to be interposed between a resin sheet constituting the encapsulant layer 14 a and a resin sheet constituting the encapsulant layer 14 b.
- the solar cells 11 each have a shape formed by obliquely cutting four corners of a substantial square in plan view, and the through holes 53 each have a shape which is substantially the same as the solar cell 11 .
- the through holes 53 are formed to correspond to the number of the solar cells 11 (eight in the example illustrated in FIG. 4 ).
- the through holes 53 may be formed so as to be larger than the solar cells 11 and may be provided so as not to overlap with the solar cells 11 .
- the through holes 53 are preferably formed so as to be slightly smaller than the solar cells 11 and so as not to overlap with the end edges of the solar cells 11 .
- the wavelength conversion substances 30 in the encapsulant layer 14 a can be inhibited from being diffused on the rear surface side of the solar cells 11 . Furthermore, in a case of the solar cell module 50 , the diffusion inhibiting layer 52 inhibits diffusion of the wavelength conversion substances 30 , and therefore design freedom of the encapsulant layer 14 b is improved compared to the case of the solar cell module 10 .
- FIG. 5 is a sectional view of a solar cell panel 61 constituting the solar cell module 60 , and illustrates a void portion between adjacent solar cells 11 .
- the solar cell module 60 is similar to the solar cell module 50 in that a diffusion inhibiting layer 62 which inhibits diffusion of wavelength conversion substances 30 is provided between an encapsulant layer 14 a and an encapsulant layer 14 b .
- the solar cell module 60 is different from the solar cell module 50 in that the diffusion inhibiting layer 62 is constituted by a resin layer 63 and a metal layer 64 .
- Resin constituting the resin layer 63 is not particularly limited, and may be, for example, resin similar to the resin 14 a, 14 b.
- Metal constituting the metal layer 64 of the diffusion inhibiting layer 62 has a diffusion coefficient of the wavelength conversion substances 30 which is substantially zero (smaller diffusion coefficient of the wavelength conversion substances 30 than in the resin 14 a ). Therefore, the diffusion inhibiting layer 62 is interposed between the encapsulant layer 14 a and the encapsulant layer 14 b over substantially the whole area, so that it is possible to significantly inhibit diffusion of the wavelength conversion substances 30 to the encapsulant layer 14 b.
- the metal constituting the metal layer 64 has a higher storage elastic modulus than that of the resin 14 a.
- the diffusion inhibiting layer 62 is disposed so as to overlap with end edges of the solar cells 11 .
- the diffusion inhibiting layer 62 may be disposed on the rear surface side of the solar cells 11 . In either case, from a viewpoint of insulation securement, the diffusion inhibiting layer 62 is disposed such that the resin layer 63 is on the solar cell 11 side.
- the metal layer 64 functions as, for example, a reflection layer which diffuses and reflects incident light passing from voids between the solar cells 11 to the rear surface side, and allows the light to be incident upon the solar cells 11 again. In order to facilitate diffusion and reflection of light, irregularities may be formed on a surface of the metal layer 64 .
- the diffusion inhibiting layer 52 is provided by use of the resin sheet having the through holes 53 in the above embodiment, but may be a diffusion inhibiting layer by use of a resin sheet having no through hole, or by disposing a plurality of strip-shaped sheets in the voids between the solar cells 11 .
- the diffusion inhibiting layer may have an inorganic compound layer of silica or the like, in place of the metal layer 64 .
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- Engineering & Computer Science (AREA)
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- Photovoltaic Devices (AREA)
- Laminated Bodies (AREA)
Abstract
A solar cell module including: a solar cell; a first protection member provided on the light receiving surface side of the solar cell; a second protection member provided on the rear surface side of the solar cell; an encapsulant layer, including a first encapsulant layer disposed between the solar cell and the first protection member, and a second encapsulant layer disposed between the solar cell and the second protection member, which seals the solar cell; and a wavelength conversion substance, contained in at least the first encapsulant layer, which absorbs light having a specified wavelength, and converts the wavelength. The concentration of the wavelength conversion substance is higher in the first encapsulant layer than in the second encapsulant layer, and a resin constituting the second encapsulant layer has a smaller diffusion coefficient of the wavelength conversion substance than the diffusion coefficient of a resin constituting the first encapsulant layer.
Description
- The present application is a divisional of U.S. application Ser. No. 15/374,291 filed Dec. 9, 2016, which is a continuation under 35 U.S.C. § 120 of PCT/JP2015/002621, filed May 25, 2015, which is incorporated herein by reference and which claimed priority to Japanese Patent Application No. 2014-122136 filed on Jun. 13, 2014. The present application likewise claims priority under 35 U.S.C. § 119 to Japanese Patent Application No. 2014-122136 filed on Jun. 13, 2014, the entire content of which is also incorporated herein by reference.
- The present disclosure relates to a solar cell module.
- There is known a solar cell module including a wavelength conversion substance that absorbs light having a specified wavelength, and converts the wavelength. According to this solar cell module, light having a wavelength region that makes little contribution to power generation among incident light can be converted into light having a wavelength contributing greatly to power generation. For example, Patent Literature 1 discloses a solar cell module in which an encapsulant layer containing a wavelength conversion substance therein is disposed on the light receiving surface side of a solar cell.
- Patent Literature 1
- WO 2011/148951 A
- In the solar cell module, light is mostly incident from the light receiving surface side, and therefore the wavelength conversion substance is preferably disposed on the light receiving surface side of the solar cell from a viewpoint of improvement of wavelength conversion efficiency. However, there is a case where the wavelength conversion substance is diffused on the rear surface side of the solar cell by long term use of the solar cell module, and the concentration of the wavelength conversion substance on the light receiving surface side is reduced.
- An aspect of a solar cell module according to the present disclosure includes: a solar cell; a first protection member provided on a light receiving surface side of the solar cell; a second protection member provided on a rear surface side of the solar cell; an encapsulant layer that includes a first encapsulant layer disposed between the solar cell and the first protection member, and a second encapsulant layer disposed between the solar cell and the second protection member, and seals the solar cell; and a wavelength conversion substance that is contained in at least the first encapsulant layer, and that absorbs light having a specified wavelength, and converts the wavelength, wherein concentration of the wavelength conversion substance in the first encapsulant layer is higher than concentration of the wavelength conversion substance in the second encapsulant layer, and resin constituting the second encapsulant layer has a smaller diffusion coefficient of the wavelength conversion substance than the diffusion coefficient of resin constituting the first encapsulant layer.
- In an aspect of the solar cell module according to the present disclosure, a diffusion inhibiting layer constituted from a material having a smaller diffusion coefficient of the wavelength conversion substance than the diffusion coefficient of resin constituting the first encapsulant layer is provided between the first encapsulant layer and the second encapsulant layer.
- According to a solar cell module of the present disclosure, a wavelength conversion substance disposed on the light receiving surface side of a solar cell can be inhibited from being diffused on the rear surface side of the solar cell.
-
FIG. 1 is a sectional view of a solar cell module of a first embodiment. -
FIG. 2 is a sectional view of a solar cell panel constituting the solar cell module of the first embodiment (wiring materials are omitted). -
FIG. 3 is a sectional view of a solar cell panel constituting a solar cell module of a second embodiment (wiring materials are omitted). -
FIG. 4 is a plan view illustrating an extracted diffusion inhibiting layer ofFIG. 3 . -
FIG. 5 is a sectional view of a solar cell panel constituting a solar cell module of a third embodiment (wiring materials are omitted). - Hereinafter, an example of embodiments will be described in detail with reference to the drawings.
- The drawings referred to in the embodiments are schematically illustrated, and the dimension ratios of components illustrated in the drawing are sometimes different from the dimension ratios of real components. Specific dimension ratios and the like should be determined in consideration of the following description.
- In this specification, a “light receiving surface” of each of a solar cell module, a solar cell, and a photoelectric conversion section means a surface on which light is mainly incident (incident from a light receiving surface upon which 50% to 100% of light is incident), while a “rear surface” means a surface opposite to the light receiving surface. Additionally, description that “a second member is provided on a first member” does not means only a case where the first and second members are provided so as to be in direct contact with each other, unless otherwise mentioned. That is, this description includes a case where another member exists between the first and second members. Description of “substantial . . . ” is intended to include not only “entirely identical” but also “substantially the same”, when “substantially the same” is taken as an example.
- Hereinafter, a
solar cell module 10 of a first embodiment will be described in detail with reference toFIG. 1 andFIG. 2 . -
FIG. 1 is a sectional view of thesolar cell module 10 which is an example of the embodiment. - As illustrated in
FIG. 1 , thesolar cell module 10 includessolar cells 11, afirst protection member 12 provided on the light receiving surface side of thesolar cells 11, asecond protection member 13 provided on the rear surface side of thesolar cells 11, and anencapsulant layer 14 that seals thesolar cells 11. Theencapsulant layer 14 includes anencapsulant layer 14 a (first encapsulant layer) disposed between thesolar cells 11 and thefirst protection member 12, and anencapsulant layer 14 b (second encapsulant layer) disposed between thesolar cells 11 and thesecond protection member 13. - The
solar cell module 10 includeswavelength conversion substances 30 contained in at least theencapsulant layer 14 a (refer toFIG. 2 and the like described below). Thewavelength conversion substances 30 are substances that absorb light having a specified wavelength to convert the wavelength, and play a role in converting light in a wavelength region hardly contributing to power generation into light in a wavelength region contributing greatly to power generation. - In this embodiment, a plurality of the
solar cells 11 are disposed on substantially the same plane. The adjacentsolar cells 11 are connected in series bywiring materials 15, thereby forming a string of thesolar cells 11. For example, eachwiring material 15 bends in the module thickness direction between the adjacentsolar cells 11, and is mounted on an electrode on the light receiving surface side of one of thesolar cells 11 and an electrode on the rear surface side of the othersolar cell 11 by an adhesive or the like. - The
solar cells 11, thefirst protection member 12, thesecond protection member 13, and theencapsulant layer 14 constitute asolar cell panel 16. Thesolar cell panel 16 is a plate-like body in which a string of thesolar cells 11 are disposed between the respective protection members, and has, for example, a substantially rectangular shape in plan view (when viewed from the direction perpendicular to the light receiving surface). Aframe 17 is preferably mounted on an end edge of thesolar cell panel 16. Theframe 17 protects the end edge of thesolar cell panel 16, and is utilized when thesolar cell module 10 is installed on a roof or the like. - The
solar cells 11 each include a photoelectric conversion section that generates carriers by receiving light. Eachsolar cell 11 has a light receiving surface electrode formed on the light receiving surface of the photoelectric conversion section and a rear surface electrode formed on a rear surface, as electrodes for collecting the carriers generated in the photoelectric conversion section. However, the structure of eachsolar cell 11 is not limited to the above, and may be, for example, a structure in which an electrode is formed only on the rear surface of the photoelectric conversion section. The rear surface electrode is preferably formed to have a larger area than the light receiving surface electrode, and it can be said that the surface having a lager electrode area (or a surface with an electrode formed thereon) is the “rear surface” of thesolar cell 11. - The photoelectric conversion section has, for example, a semiconductor substrate, an amorphous semiconductor layer formed on the substrate, and a transparent conductive layer formed on the amorphous semiconductor layer. Examples of a semiconductor constituting the semiconductor substrate can include crystalline silicon (c-Si), gallium arsenide (GaAs), indium phosphide (InP) and the like. Examples of an amorphous semiconductor constituting the amorphous semiconductor layer can include an i-type amorphous silicon, an n-type amorphous silicon, a p-type amorphous silicon, and the like. The transparent conductive layer is preferably formed of transparent conductive oxide in which tin (Sn), antimony (Sb) or the like is doped in metal oxide such as indium oxide (In2O3) and zinc oxide (ZnO).
- In this embodiment, an n-type single crystal silicon substrate is applied to the semiconductor substrate. The photoelectric conversion section has a structure in which an i-type amorphous silicon layer, a p-type amorphous silicon layer, and a transparent conductive layer are sequentially formed on the light receiving surface of the n-type single crystal silicon substrate, and an i-type amorphous silicon layer, an n-type amorphous silicon layer, and a transparent conductive layer are sequentially formed on the rear surface of the substrate. Alternatively, the p-type amorphous silicon layer may be formed on the rear surface side of the n-type single crystal silicon substrate, and the n-type amorphous silicon layer may be formed on the light receiving surface side of the substrate. That is, the photoelectric conversion section has a junction of semiconductors having different optical gaps (heterojunction). An amorphous silicon layer (thickness: several nm to several tens of nm) forming a heterojunction generally absorbs light having a wavelength of 600 nm or less.
- For the
first protection member 12, a member having transparency such as a glass substrate, a resin substrate and a resin film can be used. Among these, from a viewpoint of fire resistance, durability, and the like, the glass substrate is preferably used. The thickness of the glass substrate is not particularly limited, but is preferably about 2 mm to 6 mm. - For the
second protection member 13, a transparent member which is the same as thefirst protection member 12 may be used, or an opaque member may be used. In this embodiment, a resin film is used as thesecond protection member 13. The resin film is not particularly limited, but is preferably a polyethylene terephthalate (PET) film. From a viewpoint of lowering moisture permeability and the like, in the resin film, an inorganic compound layer of silica or the like, or a metal layer of aluminum or the like may be formed in a case where it is not assumed that light is incident from the rear surface side. The thickness of the resin film is not particularly limited, but is preferably about 50 μm to 300 μm. - The
encapsulant layer 14 plays a role in preventing moisture and the like from coming into contact with thesolar cells 11. Theencapsulant layer 14 is also called a sealing layer (sealant). Theencapsulant layer 14 is formed, for example, by a lamination step described below, by use of two respective resin sheets constituting the encapsulant layers 14 a, 14 b. In this embodiment, the encapsulant layers 14 a, 14 b are closely adhered to each other between thesolar cells 11, and between ends of thesolar cell panel 16 and thesolar cells 11 near the ends. The thickness of theencapsulant layer 14 is not particularly limited, and the thickness of each of the encapsulant layers 14 a, 14 b is preferably about 100 μm to 600 μm. - Hereinafter, the
encapsulant layer 14 containing thewavelength conversion substances 30 will be further described in detail with reference toFIG. 2 .FIG. 2 is a sectional view of thesolar cell panel 16. InFIG. 2 , thewavelength conversion substances 30 are illustrated by white circles. - As illustrated in
FIG. 2 , thewavelength conversion substances 30 are contained in theencapsulant layer 14 a provided on at least the light receiving surface side of thesolar cells 11. That is, thewavelength conversion substances 30 may be contained only in theencapsulant layer 14 a (in this case, the concentration of thewavelength conversion substances 30 satisfies, of course, concentration inencapsulant layer 14 a>concentration inencapsulant layer 14 b). Thewavelength conversion substances 30 may be contained in theencapsulant layer 14 b provided on the rear surface side of thesolar cells 11, but the concentration of thewavelength conversion substances 30 in theencapsulant layer 14 a is higher than the concentration of thewavelength conversion substances 30 in theencapsulant layer 14 b. When thewavelength conversion substances 30 are inorganic wavelength conversion substances, the concentration of thewavelength conversion substances 30 in theencapsulant layer 14 a is, for example, 0.1 weight percent to 15 weight percent, and more preferably 1.5 weight percent to 10 weight percent. In a case of organic wavelength conversion substances, the concentration of thewavelength conversion substances 30 is, for example, 0.02 weight percent to 2.0 weight percent, and more preferably 0.05 weight percent to 0.8 weight percent. - Resin constituting the encapsulant layer 14 (encapsulant layers 14 a, 14 b) is preferably excellent in adhesion to the respective protection members and the
solar cells 11, and highly impermeable to moisture. More specifically, examples of the resin constituting the encapsulant layer include olefin based resin obtained by polymerizing at least one selected from α-olefin of 2-20C (for example, a random or block copolymer of polyethylene, polypropylene, ethylene, and other α-olefin), ester-based resin (for example, polycondensate of polyol and polycarboxylic acid or acid anhydride/acid lower alkyl ester thereof), urethane-based resin (for example, a polyaddition product with polyisocyanate and active hydrogen-containing compounds (such as diol, polyol, dicarboxylic acid, polycarboxylic acid, polyamine, polythiol)), epoxy-based resin (for example, opening polymer of polyepoxide, a polyaddition product with polyepoxide and the above active hydrogen-containing compound), and a copolymer of α-olefin, and vinyl carboxylate, acrylic ester, or other vinyl monomer. - Among these, the resin constituting the encapsulant layer is particularly preferably olefin based resin (particularly, a polymer containing ethylene), and a copolymer of α-olefin and vinyl carboxylate. As the copolymer of α-olefin and vinyl carboxylate, ethylene-vinyl acetate copolymer (EVA) is particularly preferable. However, a combination of resin constituting the
encapsulant layer 14 a (hereinafter, sometimes referred to as “resin 14 a”), and resin constituting theencapsulant layer 14 b (hereinafter, sometimes referred to as “resin 14 b”) needs to satisfy the following relation. - For the
resin 14 b, resin having a smaller diffusion coefficient of thewavelength conversion substances 30 than the diffusion coefficient of theresin 14 a is used. The diffusion coefficient is a factor of proportionality which regulates the speed of diffusion appearing in Fick's laws of diffusion. The diffusion coefficient of thewavelength conversion substances 30 can be calculated by overlapping of a layer constituted from resin which contains thewavelength conversion substances 30 and which is to be measured, and an olefin based resin layer which does not contain thewavelength conversion substances 30, and obtaining the outflow speed of thewavelength conversion substances 30 from the resin layer to be measured. The outflow speed can be obtained by quantity by Gas Chromatography, or transmission spectrum measurement. The diffusion coefficient of thewavelength conversion substances 30 is made to satisfy diffusion coefficient ofresin 14 b<diffusion coefficient ofresin 14 a, so that thewavelength conversion substances 30 contained in theencapsulant layer 14 a can be inhibited from being diffused into theencapsulant layer 14 b. - The diffusion coefficient of the
wavelength conversion substances 30 in theresin 14 a is, for example, 1×10−12 to 1×10−10 (m2/s) at 120° C. The diffusion coefficient of thewavelength conversion substances 30 in theresin 14 b is, for example, 1×10−13 to 1×10−11 (m2/s) at 120° C. - The
resin 14 b preferably has a higher storage elastic modulus at 25° C. to 90° C. (hereinafter, simply referred to as a “storage elastic modulus”) than that of theresin 14 a. The storage elastic modulus is a ratio of elastic stress of the same phase as strain, and is represented by a real part of a complex modulus of elasticity. The larger a numeral value of the storage elastic modulus, the higher the elasticity of resin. The storage elastic modulus of each 14 a, 14 b can be measured by use of a dynamic viscoelasticity measuring device. The storage elastic modulus satisfies the relation storage elastic modulus ofresin resin 14 b>storage elastic modulus ofresin 14 a, so that the diffusion coefficient of thewavelength conversion substances 30 easily satisfies diffusion coefficient ofresin 14 b<diffusion coefficient ofresin 14 a. The storage elastic modulus (value at a frequency of 10 Hz in a tension mode at 25° C.) of theresin 14 a is preferably 1×107 to 1×108 (Pa), and the storage elastic modulus of theresin 14 b in the same condition is 1×108 to 1×109 (Pa). - The
resin 14 b preferably has a smaller intermolecular void size at 25° C. to 90° C. than that of theresin 14 a. In other words, theresin 14 b preferably has a smaller free volume at 25° C. to 90° C. than that of theresin 14 a. The intermolecular void size means size of a void part which is not occupied by molecules (atoms). The intermolecular void size of each 14 a, 14 b can be measured by use of a positron annihilation method. The intermolecular void size satisfies void size ofresin resin 14 b<void size ofresin 14 a, so that the diffusion coefficient of thewavelength conversion substances 30 easily satisfies void size ofresin 14 b<void size ofresin 14 a. The intermolecular void size of theresin 14 a is preferably 0.08 nm3 to 0.12 nm3, and the intermolecular void size of theresin 14 b is preferably 0.05 nm3 to 0.09 nm3. - As long as the combination of the
14 a, 14 b satisfies the above relation, the combination is not particularly limited. The following is an example of the combination.resins - Example 1
resin 14 a; low-density polyolefin,resin 14 b: high-density polyolefin - Example 2
resin 14 a; low molecular weight polyolefin,resin 14 b: high molecular weight polyolefin - Example 3
resin 14 a; low molecular weight EVA,resin 14 b: high molecular weight EVA - The
wavelength conversion substances 30 absorb, for example, ultraviolet light which is light having a wavelength shorter than 380 nm, and convert the ultraviolet light into light having a longer wavelength (e.g., 400 nm to 800 nm). In this case, thewavelength conversion substances 30 contribute to inhibition of deterioration of component materials due to the ultraviolet light. Thewavelength conversion substances 30 are preferably substances that absorb ultraviolet light to emit visible light, but may be substances that absorb visible light or infrared light. Generally, thewavelength conversion substances 30 convert light having a shorter wavelength into light having a longer wavelength, but may convert light having a longer wavelength into light having a shorter wavelength, namely, cause so-called up-conversion light emission. The preferable conversion wavelength varies depending on the type of thesolar cells 11. - In this embodiment, the
solar cells 11 each have a heterojunction layer (amorphous semiconductor layer), and therefore thewavelength conversion substances 30 preferably absorb light having energy larger than a band gap of the heterojunction layer to convert the wavelength. That is, thewavelength conversion substances 30 preferably convert the light having the wavelength absorbed in the heterojunction layer. For example, thewavelength conversion substances 30 are used to absorb light having a wavelength λα absorbed by an amorphous semiconductor layer and to convert the light having a wavelength λα into light having a wavelength λβ which is not absorbed in the semiconductor layer. The wavelength λα is 600 nm or less. - Specific examples of the
wavelength conversion substances 30 include semiconductor nanoparticles (quantum dots), inorganic compounds such as a luminescent metal complex, and organic compounds such as an organic fluorescence dye. Examples of the semiconductor nanoparticles can include zinc oxide (ZnO) nanoparticles, cadmium selenide (CdSe) nanoparticles, cadmium telluride (CdTe) nanoparticles, gallium nitride (GaN) nanoparticles, yttrium oxide (Y2O3) nanoparticles, and indium phosphide (InP) nanoparticles. Examples of the luminescent metal complex can include Ir complexes such as [Ir(bqn)3](PF6)3, [Ir(dpbpy)3](PF6)3, Ru complexes such as [Ru(bqn)3](PF6)3, [Ru(bpy)3](ClO4)2, Eu complexes such as [Eu(FOD)3]phen, [Eu(TFA)3]phen, and Tb complexes such as [Tb(FOD)3]phen, [Tb(HFA)3]phen. Examples of the organic fluorescence dye can include a rhodamine dye, a coumarin dye, a fluorescein dye, and a perylene dye. - The
wavelength conversion substances 30 substantially uniformly disperse into, for example, theencapsulant layer 14 a. Theencapsulant layer 14 a may contain ultraviolet light absorbing substances that absorb ultraviolet light and do not emit light. In this case, there may be an uneven concentration distribution of thewavelength conversion substances 30 in theencapsulant layer 14 a. For example, the concentration of thewavelength conversion substances 30 near thefirst protection member 12 may be made higher than the concentration of thewavelength conversion substances 30 near thesolar cells 11. Additionally, two or more kinds of thewavelength conversion substances 30 may be added to theencapsulant layer 14 a, or there may be an uneven concentration distribution of eachwavelength conversion substance 30 in theencapsulant layer 14 a. - The
solar cell module 10 having the above configuration can be manufactured by laminating the string of thesolar cells 11 connected by thewiring materials 15 by use of resin sheets constituting thefirst protection member 12, thesecond protection member 13, and theencapsulant layer 14. In a laminating device, for example, thefirst protection member 12, the resin sheet constituting theencapsulant layer 14 a, the string of thesolar cells 11, the resin sheet constituting theencapsulant layer 14 b, and thesecond protection member 13 are sequentially laminated on a heater. The resin sheet constituting theencapsulant layer 14 a contains thewavelength conversion substances 30 therein. This laminated body is heated to about 150° C., for example, in a vacuum state. Thereafter, the laminated body continues to be heated under atmospheric pressure while respective components are pressed onto the heater side, and the resin composition of the resin sheet is crosslinked, so that thesolar cell panel 16 is obtained. Finally, theframe 17 and the like are mounted on thesolar cell panel 16, so that thesolar cell module 10 is obtained. - As described above, according to the
solar cell module 10 having the above configuration, thewavelength conversion substances 30 in theencapsulant layer 14 a disposed on the light receiving surface side of thesolar cells 11 can be inhibited from being diffused into theencapsulant layer 14 b disposed on the rear surface side of thesolar cells 11. That is, in thesolar cell module 10, the high concentration of thewavelength conversion substances 30 is maintained in theencapsulant layer 14 a upon which a large quantity of light is incident, for a long period. Consequently, it is possible to improve efficiency of utilization of incident light, and improve photoelectric conversion efficiency. - Hereinafter, with reference to
FIG. 3 andFIG. 4 , asolar cell module 50 of a second embodiment will be described in detail.FIG. 3 is a sectional view of asolar cell panel 51 constituting thesolar cell module 50.FIG. 4 is a plan view illustrating an extracteddiffusion inhibiting layer 52 constituting thesolar cell module 50. Hereinafter, differences from the first embodiment will be mainly described, with components similar to the components of the first embodiment being denoted by the same reference numerals, and repeated description omitted (the same applies to a third embodiment). - As illustrated in
FIG. 3 , thesolar cell module 50 is different from thesolar cell module 10 in that thediffusion inhibiting layer 52 which inhibits diffusion ofwavelength conversion substances 30 is provided between anencapsulant layer 14 a and anencapsulant layer 14 b. Thediffusion inhibiting layer 52 is preferably interposed between both layers over substantially the whole area such that theencapsulant layer 14 a is not in contact with theencapsulant layer 14 b. Thediffusion inhibiting layer 52 is provided, for example, between voids of adjacentsolar cells 11, between ends of thesolar cell panel 51 and thesolar cells 11 near the ends. - The
diffusion inhibiting layer 52 is formed of a material having a smaller diffusion coefficient of thewavelength conversion substances 30 than that of theresin 14 a. In this embodiment, thediffusion inhibiting layer 52 is formed by use of a resin sheet which does not have a metal layer and an inorganic compound layer, and a resin constituting the diffusion inhibiting layer 52 (hereinafter, sometimes referred to as “resin 52”) haswavelength conversion substances 30 of smaller diffusion coefficient than in theresin 14 a. Theresin 52 preferably has a higher storage elastic modulus than that of theresin 14 a, and preferably a smaller intermolecular void size than that of theresin 14 a. The relation of theresin 14 a and theresin 52 is the same as the relation of theresin 14 a and theresin 14 b in the first embodiment, for example. Furthermore, theresin 52 preferably haswavelength conversion substances 30 of smaller diffusion coefficient than in theresin 14 b. - As illustrated in
FIG. 4 , thediffusion inhibiting layer 52 is formed of a resin sheet formed with throughholes 53 at portions where thesolar cells 11 are disposed, and the resin sheet is preferably provided to be interposed between a resin sheet constituting theencapsulant layer 14 a and a resin sheet constituting theencapsulant layer 14 b. In this embodiment, thesolar cells 11 each have a shape formed by obliquely cutting four corners of a substantial square in plan view, and the throughholes 53 each have a shape which is substantially the same as thesolar cell 11. The through holes 53 are formed to correspond to the number of the solar cells 11 (eight in the example illustrated inFIG. 4 ). In thediffusion inhibiting layer 52, the throughholes 53 may be formed so as to be larger than thesolar cells 11 and may be provided so as not to overlap with thesolar cells 11. However, the throughholes 53 are preferably formed so as to be slightly smaller than thesolar cells 11 and so as not to overlap with the end edges of thesolar cells 11. - According to the
solar cell module 50 having the above configuration, similarly to thesolar cell module 10, thewavelength conversion substances 30 in theencapsulant layer 14 a can be inhibited from being diffused on the rear surface side of thesolar cells 11. Furthermore, in a case of thesolar cell module 50, thediffusion inhibiting layer 52 inhibits diffusion of thewavelength conversion substances 30, and therefore design freedom of theencapsulant layer 14 b is improved compared to the case of thesolar cell module 10. - Hereinafter, with reference to
FIG. 5 , asolar cell module 60 of a third embodiment will be described in detail.FIG. 5 is a sectional view of asolar cell panel 61 constituting thesolar cell module 60, and illustrates a void portion between adjacentsolar cells 11. - As illustrated in
FIG. 5 , thesolar cell module 60 is similar to thesolar cell module 50 in that adiffusion inhibiting layer 62 which inhibits diffusion ofwavelength conversion substances 30 is provided between anencapsulant layer 14 a and anencapsulant layer 14 b. On the other hand, thesolar cell module 60 is different from thesolar cell module 50 in that thediffusion inhibiting layer 62 is constituted by aresin layer 63 and ametal layer 64. Resin constituting theresin layer 63 is not particularly limited, and may be, for example, resin similar to the 14 a, 14 b.resin - Metal constituting the
metal layer 64 of thediffusion inhibiting layer 62 has a diffusion coefficient of thewavelength conversion substances 30 which is substantially zero (smaller diffusion coefficient of thewavelength conversion substances 30 than in theresin 14 a). Therefore, thediffusion inhibiting layer 62 is interposed between theencapsulant layer 14 a and theencapsulant layer 14 b over substantially the whole area, so that it is possible to significantly inhibit diffusion of thewavelength conversion substances 30 to theencapsulant layer 14 b. The metal constituting themetal layer 64 has a higher storage elastic modulus than that of theresin 14 a. - In the example illustrated in
FIG. 5 , on the light receiving surface side of thesolar cells 11, thediffusion inhibiting layer 62 is disposed so as to overlap with end edges of thesolar cells 11. Thediffusion inhibiting layer 62 may be disposed on the rear surface side of thesolar cells 11. In either case, from a viewpoint of insulation securement, thediffusion inhibiting layer 62 is disposed such that theresin layer 63 is on thesolar cell 11 side. Themetal layer 64 functions as, for example, a reflection layer which diffuses and reflects incident light passing from voids between thesolar cells 11 to the rear surface side, and allows the light to be incident upon thesolar cells 11 again. In order to facilitate diffusion and reflection of light, irregularities may be formed on a surface of themetal layer 64. - The design of each embodiment can be suitably changed without departing from the object of the present disclosure.
- For example, the
diffusion inhibiting layer 52 is provided by use of the resin sheet having the throughholes 53 in the above embodiment, but may be a diffusion inhibiting layer by use of a resin sheet having no through hole, or by disposing a plurality of strip-shaped sheets in the voids between thesolar cells 11. Additionally, the diffusion inhibiting layer may have an inorganic compound layer of silica or the like, in place of themetal layer 64. -
- 10, 50, 60 Solar cell module
- 11 Solar cell
- 12 First protection member
- 13 Second protection member
- 14, 14 a, 14 b Encapsulant layer
- 15 Wiring material
- 16, 51, 61 Solar cell panel
- 17 Frame
- 30 Wavelength conversion substance
- 52, 62 Diffusion inhibiting layer
- 53 Through hole
- 63 Resin layer
- 64 Metal layer
Claims (11)
1. A solar cell module comprising:
a solar cell;
a first protection member provided on a light receiving surface side of the solar cell;
a second protection member provided on a rear surface side of the solar cell;
an encapsulant layer that includes a first encapsulant layer disposed between the solar cell and the first protection member, and a second encapsulant layer disposed between the solar cell and the second protection member, and seals the solar cell; and
a wavelength conversion substance that is contained in at least the first encapsulant layer, wherein
concentration of the wavelength conversion substance in the first encapsulant layer is higher than concentration of the wavelength conversion substance in the second encapsulant layer, and ()
a diffusion inhibiting layer constituted from a material having a smaller diffusion coefficient of the wavelength conversion substance than he diffusion coefficient of resin constituting the first encapsulant layer is provided between the first encapsulant layer and the second encapsulant layer.
2. The solar cell module according to claim 1 , wherein the material constituting the diffusion inhibiting layer has a higher storage elastic modulus at 25° C. to 90° C. than that of the resin constituting the first encapsulant layer.
3. The solar cell module according to claim 1 , wherein the material constituting the diffusion inhibiting layer has a smaller intermolecular void size at 25° C. to 90° C. than that of the resin constituting the first encapsulant layer.
4. The solar cell module according to claim 1 , wherein
the wavelength conversion substance is an inorganic semiconductor nanoparticle.
5. The solar cell module according to claim 1 , wherein the wavelength conversion substance is a luminescent metal complex.
6. The solar cell module according to claim 1 , wherein the wavelength conversion substance is a fluorescence dye.
7. The solar cell module according to claim 1 , wherein
concentration of the wavelength conversion substance in a first region of the first encapsulant layer closer to the first protection member is higher than in a second region of the first encapsulant layer closer to the solar cell.
8. The solar cell module according to claim 1 , wherein
a front surface side of the diffusion inhibiting layer has concave-convex pattern arranged in width direction of the diffusion inhibiting layer, and the front surface side is faces the first encapsulant layer.
9. The solar cell module according to claim 1 , wherein
the diffusion inhibiting layer comprising a metal layer at a front surface side of the diffusion inhibiting layer, and the front surface side is faces the first encapsulant layer.
10. The solar cell module according to claim 9 , wherein
the resin layer of the diffusion inhibiting layer is arranged between the metal layer and the solar cell, and the metal layer and the solar cell are insulated each other.
11. The solar cell module according to claim 1 , wherein
the diffusion inhibiting layer comprising an inorganic compound layer at the front surface side of the diffusion inhibiting layer.
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| US16/249,000 US20190148578A1 (en) | 2014-06-13 | 2019-01-16 | Solar cell module |
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| JP2014-122136 | 2014-06-13 | ||
| JP2014122136 | 2014-06-13 | ||
| PCT/JP2015/002621 WO2015190046A1 (en) | 2014-06-13 | 2015-05-25 | Solar cell module |
| US15/374,291 US10224448B2 (en) | 2014-06-13 | 2016-12-09 | Solar cell module |
| US16/249,000 US20190148578A1 (en) | 2014-06-13 | 2019-01-16 | Solar cell module |
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| CN104880864B (en) * | 2015-06-17 | 2018-11-16 | 合肥鑫晟光电科技有限公司 | Sealant solidification equipment and packaging method |
| KR20170053416A (en) * | 2015-11-06 | 2017-05-16 | 주식회사 엘지화학 | Semiconductor device and manufacturing method of the same |
| KR102255573B1 (en) * | 2019-08-27 | 2021-05-24 | 고려대학교 산학협력단 | Solar module |
| AU2021365997A1 (en) * | 2021-09-16 | 2024-04-11 | Mpw Technologies International Pte. Ltd. | Light-emitting solar energy collection device and manufacturing method therefor |
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| US5994641A (en) * | 1998-04-24 | 1999-11-30 | Ase Americas, Inc. | Solar module having reflector between cells |
| US20110126889A1 (en) * | 2009-09-25 | 2011-06-02 | Immunolight, Llc | Up and down conversion systems for improved solar cell performance or other energy conversion |
| US20130139868A1 (en) * | 2011-12-06 | 2013-06-06 | Nitto Denko Corporation | Wavelength conversion material as encapsulate for solar module systems to enhance solar harvesting efficiency |
| US20140319377A1 (en) * | 2011-04-20 | 2014-10-30 | Morgan Solar Inc. | Pulsed stimulated emission luminescent photovoltaic solar concentrator |
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| JP4036616B2 (en) * | 2000-01-31 | 2008-01-23 | 三洋電機株式会社 | Solar cell module |
| JP2011210891A (en) * | 2010-03-29 | 2011-10-20 | Hitachi Chem Co Ltd | Wavelength-converting solar cell sealing sheet, and solar cell module |
| JP2011238639A (en) * | 2010-05-06 | 2011-11-24 | Toppan Printing Co Ltd | Sealing material sheet for solar cell module and solar cell module |
| WO2011148951A1 (en) | 2010-05-26 | 2011-12-01 | 日立化成工業株式会社 | Wavelength conversion-type solar cell sealing material, and solar cell module |
| CN102918659B (en) * | 2010-05-31 | 2016-04-27 | 大日本印刷株式会社 | Solar module encapsulant and manufacture method thereof |
| JP5476290B2 (en) * | 2010-12-28 | 2014-04-23 | 株式会社日立製作所 | Solar cell module |
| JP2013045778A (en) * | 2011-08-20 | 2013-03-04 | Kyocera Corp | Solar cel and solar cell module |
| JP2013120926A (en) * | 2011-12-06 | 2013-06-17 | Nitto Denko Corp | Wavelength-conversion substance serving as solar module system sealant for increase of solar light-collecting efficiency |
| JP5970673B2 (en) * | 2012-03-08 | 2016-08-17 | 東洋インキScホールディングス株式会社 | Solar cell module and method for manufacturing solar cell module |
| CN102623533B (en) * | 2012-03-16 | 2014-07-23 | 友达光电股份有限公司 | Solar module capable of absorbing ultraviolet light band and manufacturing method thereof |
-
2015
- 2015-05-25 EP EP15806594.6A patent/EP3157066A4/en not_active Withdrawn
- 2015-05-25 WO PCT/JP2015/002621 patent/WO2015190046A1/en not_active Ceased
- 2015-05-25 JP JP2016527622A patent/JP6628047B2/en not_active Expired - Fee Related
-
2016
- 2016-12-09 US US15/374,291 patent/US10224448B2/en not_active Expired - Fee Related
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2019
- 2019-01-16 US US16/249,000 patent/US20190148578A1/en not_active Abandoned
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5994641A (en) * | 1998-04-24 | 1999-11-30 | Ase Americas, Inc. | Solar module having reflector between cells |
| US20110126889A1 (en) * | 2009-09-25 | 2011-06-02 | Immunolight, Llc | Up and down conversion systems for improved solar cell performance or other energy conversion |
| US20140319377A1 (en) * | 2011-04-20 | 2014-10-30 | Morgan Solar Inc. | Pulsed stimulated emission luminescent photovoltaic solar concentrator |
| US20130139868A1 (en) * | 2011-12-06 | 2013-06-06 | Nitto Denko Corporation | Wavelength conversion material as encapsulate for solar module systems to enhance solar harvesting efficiency |
Also Published As
| Publication number | Publication date |
|---|---|
| JP6628047B2 (en) | 2020-01-08 |
| EP3157066A1 (en) | 2017-04-19 |
| WO2015190046A1 (en) | 2015-12-17 |
| US20170092796A1 (en) | 2017-03-30 |
| EP3157066A4 (en) | 2017-06-21 |
| JPWO2015190046A1 (en) | 2017-04-20 |
| US10224448B2 (en) | 2019-03-05 |
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