The present disclosure relates to the field of solar energy technologies, and more particularly, to a solar panel.
A solar panel is short for a solar cell panel, which is a core part of a solar power system. An operation principle of the solar panel is to generate power by absorbing sunlight and directly supply power to an application product, or charge a battery and then supply power to the application product from the battery.
Embodiments of the present disclosure provide a solar panel.
The solar panel according to embodiments of the present disclosure includes a cell configured to receive radiations and generate power.
The solar panel according to an embodiment includes a frame, a front plate, a back plate, and a cell. The frame has an accommodation opening. The front plate is located at one of two opposite sides of the frame. The back plate is located at another one of the two opposite sides of the frame. The accommodation opening is enclosed by the front plate, the back plate and the frame to form an enclosed space, and the cell is disposed in the enclosed space.
Embodiments of the present disclosure provide a solar panel. The solar panel includes at least one power generation assembly and a wire. Each of the at least one power generation assembly includes a rigid frame, a cell, a back plate, an insulation plate. The rigid frame has an accommodation opening. The cell is disposed at the accommodation opening. The back plate is disposed at the accommodation opening and located on the cell. An adhesive film is arranged between the back plate and the cell. The insulation plate covers an end surface of the rigid frame close to the back plate. The wire is arranged between the back plate and the insulation plate.
Embodiments of the present disclosure provide a solar panel. The solar panel includes a battery layer, and a front plate and a back plate that are respectively stacked at a front side and a back side of the battery layer. The battery layer includes the rigid frame and a battery string. The rigid frame includes a plurality of vertical frame bars and a plurality of horizontal bars. The plurality of vertical frame bars are cross-connected to the plurality of transverse frame bars to define a plurality of accommodation openings. The battery string includes a plurality of cells accommodated at the accommodation openings. The plurality of vertical frame bars is detachably connected to the plurality of transverse frame bars.
Additional aspects and advantages of the present disclosure will be given at least in part in the following description, or become apparent at least in part from the following description, or can be learned from practicing of the present disclosure.
The above and/or additional aspects and advantages of the present disclosure will become more apparent and more understandable from the following description of embodiments taken in conjunction with the accompanying drawings, in which:
The embodiments of the present disclosure will be described in detail below with reference to examples thereof as illustrated in the accompanying drawings, throughout which same or similar elements are denoted by same or similar reference numerals.
In addition, the embodiments described below with reference to the drawings are illustrative merely, and are intended to explain, rather than limiting, the present disclosure.
According to the embodiment of the present disclosure, the cell 12 of the solar panel is disposed at the accommodation opening of the rigid frame 11. The rigid frame 11 can protect the cell 12 in an encapsulating direction, and thus can improve impact resistance, bending resistance, and mechanical strength. Meanwhile, compared with a traditional external metal frame, the rigid frame is lighter in weight, and can reduce a shielding of the edges. Therefore, an operation of the cell 12 cannot be interfered.
The front plate 15 may be made of an insulating transparent material of mechanical toughness, such as polyethylene terephthalate (PET) and PET composites, or a thin glass. In this way, a solar energy conversion rate of the power generation assembly 1100 can be improved to meet power demand of users.
The back plate 13 may be made of a support material of mechanical toughness, such as a glass fiber plate, the PET and PET composites, and the thin glass. In this way, the back plate can support the cell 12 to better protect the cell 12.
The insulation plate 14 may be made of an anti-puncture material of mechanical strength, such as the glass fiber plate, and the PET and PET composites. In this way, it is possible to prevent the broken wire 1200 from puncturing the insulation plate 14, and thus power leakage of the solar panel can be avoided.
The front film 1300 is made of a transparent flexible material selected from fluorine-containing materials such as ethylene-tetra-fluoro-ethylene (ETFE), polyvinylidene difluoride (PVDF), Poly (vinyl formal) (PVF), ethylene-chlorotrifluoroethylene copolymer (ECTFE), and the like. These materials have characteristics of aging resistance and can prolong a service life of the solar panel. Further, the back film 1400 is made of a transparent flexible material selected from the fluorine-containing materials such as ETFE, PVDF, PVF, ECTFE, and the like. These materials have the characteristic of aging resistance and can prolong the service life of the solar panel. In addition, the back film 1400 may also be made of an opaque cloth material.
An adhesive film 1600 is arranged between the front film 1300 and the front plate 15 to increase connection strength between the front film 1300 and the front plate 15. An adhesive film 1600 is arranged between the back film 1400 and the insulation plate 14 to increase connection strength between the back film 1400 and the insulation plate 14.
Referring to
Continuing to refer to
Further, each of the the handle structures 1800 has a gripping groove. Each of the front film 1300 and the back film 1400 has a through groove corresponding to the gripping groove. A shape of the through groove matches with a shape of the gripping groove. The user can carry the solar panel directly by means of the gripping grooves.
Continuing to refer to
In
After the solar panel is repeatedly folded and unfolded at the bendable region 1700, a part of the wire 1200 located at the bendable region 1700 is prone to be broken or fractured.
In some embodiments, two sides of the part of the wire 1200 located in the bendable region 1700 are covered with the insulation film 1500. In this way, the two sides of the wire 1200 can be better protected, and thus it is possible to prevent the front film 1300 and the back film 1400 from being punctured due to the broken wire 1200. Therefore, power leakage of the solar panel can be avoided.
The part of the wire 1200 located in the bendable region 1700 is made of scattered braided copper wires to reduce a bending force applied to the wire 1200 in the bendable region 1700, which can prolong a service life of the wire 1200 and avoid the power leakage due to the puncture of the front film 1300 or the back film 1400 by the broken wire 1200.
As shown in
In an exemplary embodiment, the solar panel of the embodiment is internally provided with a rigid frame 24 and a power generation module composed of a cell layer 21, a front plate layer 22, and a back plate layer 23. The cell layer 21 is configured to receive light radiations and generate power. The front plate layer 22 and the back plate layer 23 can protect the cell layer 21 from a front side and a back side, respectively. The cell layer 21 is disposed at the accommodation opening 241 of the rigid frame 24. The rigid frame 24 can protect the cell layer 21 in an encapsulating direction, and thus can improve impact resistance, bending resistance, and mechanical strength. Meanwhile, compared with a traditional external metal frame, the rigid frame is lighter in weight, and can reduce a shielding of the edges. Therefore, an operation of the cell layer 21 cannot be interfered.
In some embodiments, the entire power generation module is accommodated at the accommodation opening 241 as a whole. That is, the front plate layer 22, the cell layer 21 and the back plate layer r23 are all accommodated at the accommodation opening 241.
In some embodiments, the cell layer 21 includes at least two cells 211. The front plate layer 22 includes a front plate unit 221, and the back plate layer 23 includes a back plate unit 231. The accommodation opening 241 is formed at the rigid frame 24. A sub-power generation module includes the cell 211, the front plate unit 221, and the back plate unit 231 that are stacked together. At least one sub-power generation module correspondingly has one accommodation openings 241. In this embodiment, the cell layer 21 includes four cells 211 arranged in a matrix pattern. An integrated front plate unit 221 and an integrated back plate unit 231 are respectively arranged at a front surface and a back surface of the four cells 21L In an exemplary embodiment, when the solar panel has a small size (generally less than 0.1 m 2), the rigid frame 24 is designed into a single accommodation opening structure, and the sub-power generation modules are disposed in the single accommodation opening 241 of the rigid frame 24.
In some embodiments, the cell layer 21 includes a plurality of double-sided crystalline silicon chips. Each of the cells 211 is provided with the double-sided crystalline silicon chip. The double-sided crystalline silicon chip can receive light radiations from two opposite sides and generating power. Therefore, power generation per unit weight of the cell layer 21 can be increased.
In some embodiments, the rigid frame 24 is made of a high temperature resistant polymer material or a metal material such as a polyimide polymer, an aromatic polyamide polymer, an aluminum alloy. In this way, the the rigid frame 24 has a lighter weight than a traditional external metal frame and the double-sided operation of the cell 211 would not be interfered while improving impact resistance, bending resistance and mechanical strength. When mounting the solar panel, the cell 211 can be laminated after being correspondingly disposed at the accommodation opening 241. In this case, the the integrated can be omitted and manufacturing is simple.
In some embodiments, the rigid frame 24 has a thickness greater than or equal to a thickness of the cell layer 21, which can improve protection reliability.
In some embodiments, the thickness of the rigid frame 24 is greater than or equal to a thickness of the power generation module, which can further improve the protection reliability.
In some embodiments, the thickness of the rigid frame 24 ranges from 0.5 mm to 3 mm, and a width of the rigid frame 24 ranges from 5 mm to 30 mm.
In some embodiments, each of the front plate layer 22 and the back plate layer 23 is made of a transparent polymer material or an ultra-thin glass such as polycarbonate (PC), polyester resin (PET), or PET film material containing a coating layer. The front plate layer 22 and the back plate layer 23 may also be made of a transparent flexible material with good mechanical strength, such as expandable polyethylene (EPE), composite phenolic foam (FPF), double-sided fluorine-containing back plate (KPK).
In some embodiments, the thickness of each of the front plate layer 22 and the back plate layer 23 range from 0.2 mm to 1 mm.
In some embodiments, the solar panel further includes a front film layer 25 and a back film layer 26. The front film layer 25 and the back film layer 26 are respectively attached to a front surface and a back surface of the power generation module. In one embodiment, the front film layer 25 is arranged at a side of the front plate layer 22 away from the cell layer 21, and the back film layer 26 is arranged at a side of the back plate layer 23 away from the cell layer 21 each of the front film layer 25 and the back film layer 26 has a transparent structures for protecting the inner power generation module.
In some embodiments, the front film layer 25 and the back film layer 26 are made of a fluorine-containing film material such as ethylene-tetrafluoroethylene copolymer (ETFE), ethylene-chlorotrifluoroethylene copolymer (ECTFE).
In some embodiments, the front film layer 25 and the back film layer 26 are made of a same material. In one embodiment, the back film layer 26 is made of polyester resin (PET) with a predetermined mechanical strength, which can better bond the sub-power generation modules in the rigid frame 24 and provide supporting and better edge protection.
In some embodiments, the front plate layer 22 and the back plate layer 23 are respectively bonded to the cell layer 21 by a first encapsulation adhesive film 27. The front film layer 25 and the back film layer 26 are respectively bonded to the power generation module by a second encapsulation adhesive film 28.
Further, the front film layer 25 and its corresponding the second encapsulation adhesive film 28 are subjected to physical embossing at a high temperature, and the back film layer 26 and its corresponding the second encapsulation adhesive film 28 are subjected to physical embossing at a high temperature. As a result, rough surfaces are respectively formed on the front film layer 25 and the back film layer 26. On the one hand, the rough surfaces serves as a light trapping structure, and on the other hand, the rough surfaces can protect the inner layer structure in the solar panel from being scratched. In addition, it is possible to assist in limiting the cell layer 21 to confine the cell 211 at the accommodation opening 241 of the rigid frame 24.
In some embodiments, the first encapsulation adhesive film 27 and the second encapsulation adhesive film 28 may be made of EVA plastic, POE plastic, polyvinyl butyral (PVB), thermoplastic polyolefin (TPO) or benzoyl peroxide (BPO). Each of the first encapsulation adhesive film 27 and the second encapsulation adhesive film 28 has a colorless and transparent structure.
A solar panel according to a second embodiment of the present disclosure will be described below. As shown in
In some embodiments, the power generation module is divided into a plurality of sub-power generation modules, and each of the plurality of sub-power generation modules is disposed at the accommodation openings 241 of the rigid frame 24 in one-to-one correspondence. In this way, a size of each front plate unit 221 and each back plate unit 231 can be reduced. As a result, bending and deformation of the front plate unit 221 and the back plate unit 231 of large size can be avoided. The front plate unit 221 and the back plate unit 231 can be compatible with more materials such as ultra-thin glass. Further, since the ultra-thin glass has high flatness, a rigidity of the glass can improve impact resistance of the front surface and the back surface of the cell, thereby improving bending resistance of the solar panel.
In other embodiments, two or more self-generating modules may also be disposed at the accommodation opening 241 of the rigid frame 24.
In some embodiments, the first encapsulation adhesive film 27 includes a plurality of sub-encapsulation adhesive films 271, and the plurality of sub-encapsulation adhesive films 271 are constructed into an elongated structure matching with each of the front plate unit 221 and the back plate unit 231. The front plate unit 221 and the back plate unit 231 are respectively bonded to the cell 211 by the corresponding sub-encapsulation adhesive film 271.
A solar panel according to a third embodiment of the present disclosure will be described below. As shown in
A solar panel according to a fourth embodiment of the present disclosure will be described below. As shown in
In some embodiments, each of the sub-power generation modules includes a cell 211, a front plate unit 221, and a back plate unit 231. In this way, it is possible to further reduce the size of each front plate unit 221 and each back plate unit 231.
In some embodiments, the first encapsulation adhesive film 27 includes a plurality of sub-encapsulation adhesive films 271 arranged in a matrix pattern. The front plate unit 221 and the back plate unit 231 are respectively bonded to cell 211 by the corresponding sub-encapsulation adhesive films 271.
A solar panel according to a fifth embodiment of the present disclosure will be described below. As shown in
A solar panel according to a sixth embodiment of the present disclosure will be described below. As shown in
In an exemplary embodiments, in the solar panel according to the present embodiment, the at least one glass fiber reinforcement layer 32 is arranged between one of the two protective layer 33 and the cell layer 31. The cell layer 31 is configured to receive light radiations and generate power. The protective layer 33 is configured to protect an inner layer structure. The Mass fiber reinforcement layer 32 subjected to high-temperature hot pressing is transparent. The protective layer 33 also has a transparent structure to allow for transmission without affecting an operation of the cell layer 31. The glass fiber reinforcement layer 32 is made by mixing the glass fiber and the impregnated adhesive. On the one hand, the glass fiber reinforcement layer 32 can improve impact resistance of the cell layer 31 and bending resistance of the solar panel. On the other hand, since each of the glass fiber and the the impregnated adhesive for forming the glass fiber reinforcement layer 32 has a small density, influence on self-weight of the solar panel is less, and portability of the solar panel can be ensured. In addition, the glass fiber reinforcement layer 32 can initially fix the cell layer 31 due to its predetermined viscosity. Therefore, it is possible to prevent the cell layer 31 from being displaced during a laminating operation.
In some embodiments, two glass fiber reinforcement layers 32 is provided. The two glass fiber reinforcement layers 32 are respectively arranged at two sides of the cell layer 31. The two glass fiber reinforcement layers 32 can enhance the impact resistance of the cell layer 31 respectively from two sides, thereby further improving the impact resistance.
In some embodiments, the glass fiber reinforcement layer 32 is constructed into an integrated mesh structure.
In some embodiments, the impregnated adhesive includes at least one of EVA (ethylene vinyl acetate copolymer) plastic, POE (high polymer of ethylene and butene, or high polymer of ethylene and octene) plastic, and polyester resin.
In some embodiments, the cell layer 31 includes a plurality of double-sided crystalline silicon chips. The plurality of double-sided crystalline silicon chips is capable of receiving light radiations from two opposite sides and generating power, and thus amount of power generation per unit weight of that cell layer 31 can be improved.
In some embodiments, the cell layer 31 includes a plurality of cells 311. Each of the plurality of the cells 311 has a double-sided crystalline silicon chip. The solar panel further includes a rigid frame 35. The rigid frame 35 is constructed into a frame structure. The rigid frame 35 has a plurality of accommodation openings 351 arranged in a matrix pattern. The accommodation openings 351 are configured to accommodate the cells 311. The rigid frame 35 is made of a high temperature resistant polymer material or a metal material such as polyimide polymer, aromatic polyamide polymer, or aluminum alloy. The rigid frame 35 can protect the cell layer 31 in an encapsulating direction, and thus impact resistance, bending resistance, and mechanical strength can be improved. Meanwhile, compared with a traditional external metal frame, the rigid frame is lighter in weight, and can reduce a shielding of the edges. Therefore, a double-sided operation of the cell 311 cannot be interfered. When mounting the solar panel, the cells 311 is correspondingly disposed at the accommodation opening 351 and then is laminated. In this case, the integrated frame can be omitted and manufacturing is simple.
In some embodiments, the rigid frame 35 has a thickness great than or equal to a total thickness of the plurality of cells 311.
In some embodiments, the thickness of the rigid frame 35 ranges from 0.5 mm to 3 mm, and a width of the rigid frame 35 ranges from 5 mm to 30 mm.
In some embodiments, the glass fiber reinforcement layer 32 and the protective layer 33 are bonded to each other by an encapsulation adhesive film 36.
Further, the protective layer 33 and its corresponding encapsulation adhesive film 36 are subjected to physical embossing at a high temperature. As a result, a rough surface is formed on the protective layer 33. On the one hand, the rough surface serves as a light trapping structure, and on the other hand, the rough surfaces can protect the inner layer structure in the solar panel from being scratched. In addition, it is possible to assist in limiting the cell layer 31 to confine the cell 311 at the accommodation opening 351 of the rigid frame 35.
In some embodiments, the protective layer 33 is made of a fluorine-containing film material such as ETFE (ethylene-tetrafluoroethylene copolymer), ECTFE (ethylene-chlorotrifluoroethylene copolymer).
In some embodiments, the encapsulation adhesive film 36 may be made of EVA plastic, POE plastic, PVB (polyvinyl butyral), TPO (thermoplastic polyolefin) or BPO (benzoyl peroxide). The encapsulation adhesive film 36 has a colorless transparent structure.
A solar panel according to a seventh embodiment of the present disclosure will be described below. As shown in
A solar panel according to an eighth embodiment of the present disclosure will be described below. As shown in
A solar panel according to a ninth embodiment of the present disclosure will be described below. As shown in
In some embodiments, the carrying layer 34 is made of PC (polycarbonate), PET, or a PET film material containing a coating layer, or the carrying layer 34 may also be made of a transparent flexible material with good mechanical strength, such as EPE (expandable polyethylene), FPF (compounded phenolic foam), KPK (double-sided fluorine-containing back plate).
In some embodiments, the carrying layer 34 has a thickness ranging from 0.2 mm to 1 mm.
A solar panel according to a tenth embodiment of the present disclosure will be described below. As shown in
In the solar panel according to the embodiments, as shown in
In some embodiments, according to the solar panel of this embodiment, the hard rigid frame 4100 is arranged between the front plate 4300 and the back plate 4400, and the battery string 4200 is disposed at the accommodation openings 4130 of the rigid frame 4100. The rigid frame 4100 has a high support strength, and thus damage to the battery string 4200 due to bending deformation of the solar panel can be reduced, thereby protecting the battery string 4200 and improving the mechanical strength without more layers and adding the glass fiber material. As a result, an overall weight and costs can be lowered. The rigid frame 4100 is composed of the plurality of the vertical frame bars 4110 and the plurality of the transverse frame bars 4120 that are detachably connected to each other. Compared with an integrated frame structure, the solar panel not only has lower production costs, but also is easy to be assembled with products of different shapes, size, and thicknesses, therefore, the solar panel has higher flexibility in use.
Illustratively, each of the plurality of the vertical frame bars 4110 and each of the plurality of the transverse frame bars 4120 has a thickness greater than or equal to a thickness of the battery string 4200. In this way, surface strength of the solar panel can be enhanced. In this embodiment, the thickness of each of the plurality of the vertical frame bars 4110 and the plurality of the transverse frame bars 4120 is greater than the thickness of the battery string 4200. Thus, it is possible to prevent a normal force from being applied to the battery string 4200.
Illustratively, as shown in
Illustratively, as shown in
Illustratively, the vertical frame bars 4110 include several inner vertical frame bars 4111 and two side vertical frame bars 4112 that are transversely arranged side by side. The inner vertical frame bars 4111 are disposed at the vertical gaps 4203. The two side vertical frame bars 4112 are arranged side by side at a left side and a right side of the inner vertical frame bars 4111. The side vertical frame bars 4112 are located at a left and a right side of the battery string 4200 to wrap the left and right sides of battery string 4200, thereby protecting the left and right sides of the solar panel.
Illustratively, the transverse frame bars 4120 include several inner transverse frame bars 4121 and at least two side transverse frame bars 4122 that are arranged vertically side by side. At least one of the inner transverse frame bars 4121 is disposed at the transverse gaps 4204. The two side transverse frame bars 4122 are arranged side by side at an upper side and a lower side of the inner transverse frame bars 4121. The side transverse frame bars 4122 are located at an upper side and a lower side of battery string 4200 to wrap the upper and lower sides of battery string 4200, thereby protecting the upper and lower sides of the solar panel.
In this embodiment, as shown in
Illustratively, as shown in
Illustratively, as shown in
In other embodiments of the present disclosure, the transverse gap 4204 may also be provided for the inner transverse frame bars 4121 of a single layer, and each of side transverse frame bars 4122 at the upper sides and the lower sides of the battery string 4200 may also be a side transverse frame bar of a single layer. A thickness of each of the inner transverse frame bar 4121 and the side transverse frame bar 4122 is smaller than a thicknesses of each of the inner vertical frame bar 4111 and the side vertical frame bar 4112. In this way, the welding strip 4202 can be easily pulled, and thus it is possible to provide more room for the current collecting wire.
Illustratively, each of the inner transverse frame bar 4121 and the side transverse frame bars 4122 is constructed into an elongated thin plate-like structure. The thicknesses of each of the inner transverse frame bar 4121 and the side transverse frame bar 4122 is smaller than each of the thickness of the inner vertical frame bar 4111 and the side vertical frame bar 4112.
Illustratively, the inner transverse frame bar 4121 and side transverse frame bar 4122 have the same thickness, and the inner vertical frame bar 4111 and side vertical frame bar 4112 have the same thickness.
Illustratively, the inner transverse frame bar 4121, the side transverse frame bar 4122, the inner vertical frame bar 4111, and the side vertical frame bar 4112 have different thicknesses.
In this embodiment, a width of the vertical gap 4203 ranges from 25 mm to 35 mm, and a width of the transverse gap 4204 ranges from 35 mm to 45 mm. The side vertical frame bar 4112 has a thickness of 3 mm and a width of 30 mm. The inner vertical frame bar 4111 has a thickness of 3 mm and a width ranging from 25 mm to 35 mm. A thickness of the side transverse frame bar 4122 located below the welding strip 4202 is 1.2 mm, and a thickness of the side transverse frame bar 4122 located above the welding strip 4202 is 1.6 mm A width of each of the side transverse frame bars 4122 is 30 mm. A thickness of the inner transverse frame bar 4121 located below the welding strip 4202 is 1.2 mm, and a thickness of the inner transverse frame bar 4121 located above the welding strip 4202 is 1.6 mm. A width of each of the inner transverse frame bars 4121 ranges from 35 mm to 45 mm.
Illustratively, the sub-battery string is spaced apart from the vertical frame bar 4110 and the transverse frame bar 4120. In this way, it is possible to reduce undesirable risks of fragmentation of the cells 4201 or poor lamination due to a non-uniform local pressure caused by a height difference during the lamination.
Illustratively, as shown in
In this embodiment, as shown in
Illustratively, a peripheral edge of each of the side vertical frame bars 4112 and side transverse frame bars 4122 has a chamfer for reducing stress at the edges and corners when being impacted by external forces.
Illustratively, the vertical frame bars 4110 and/or transverse frame bars 4120 has a mounting hole(s). The front plate 4300, the back plate 4400 and/or external components are connected to each other by passing a fastener through the mounting hole. In this way, on the one hand, an adhesive bonded structure of a flexible board can be removed, and an air circulation channel under the solar panel can be formed, which can improve a heat dissipation performance and power generation efficiency of the solar panel. On the other hand, it is convenient to connect external components such as handles and brackets. Therefore, a compactness of the structure can be improved.
Illustratively, as shown in
Illustratively, the rigid frame 4100 is made of a fiberboard with high mechanical strength or a metal plate with surface insulation treatment.
Illustratively, the front plate 4300 is made of a material selected from transparent insulating materials with high mechanical toughness such as PET (polyethylene terephthalate) and PET composites.
Illustratively, the back plate 4400 is made of a material selected from support material with high mechanical toughness such as glass fiber sheet, PET and PET composite materials.
Illustratively, the adhesive film 4500 is made of a photovoltaic conventional material such as EVA (ethylene vinyl acetate copolymer), POE (Poly Olefin Elastomer), PO (propylene oxide), PVB (polyvinyl butyral).
Although explanatory embodiments have been illustrated and described, it would be appreciated that the above embodiments are exemplary and cannot be construed to limit the present disclosure. In addition, changes, modifications, alternatives and varieties can be made in the embodiments by those skilled in the art without departing from scope of the present disclosure. The scope of the present disclosure shall be defined by the claims as appended and their equivalents.
Number | Date | Country | Kind |
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202210775387.2 | Jul 2022 | CN | national |
202221779611.7 | Jul 2022 | CN | national |
202223301238.7 | Dec 2022 | CN | national |
202320081870.0 | Jan 2023 | CN | national |
This application is a continuation of International Application No. PCT/CN2023/093553, filed on May 11, 2023, which claims a priority to Chinese Patent Application No. 202221779611.7 filed on Jul. 11, 2022, No. 202210775387.2 filed on Jul. 1, 2022, No. 202223301238.7 filed Dec. 9, 2022, and No. 202320081870.0 filed on Jan. 13, 2023 with China National Intellectual Property Administration, the entire contents of which are incorporated herein by reference.
Number | Date | Country | |
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Parent | PCT/CN2023/093553 | May 2023 | US |
Child | 18389824 | US |