Flexible solar cell module and preparation method and application thereof
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A technology of flexible solar cells and solar cells, which is applied in the field of solar cells and can solve problems such as low surface density
Active Publication Date: 2017-01-04
48TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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Problems solved by technology
[0006] The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art, to provide a low surface density, good bending and flexibility, adaptable to fit the curved surface of the airfoil, good reliability, no warping, cracking, etc. A flexible solar cell module with encapsulation problem, and correspondingly provide a preparation method of the flexible solar cell module and its application on space vehicles such as solar drones
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Embodiment 1
[0034] like figure 1 As shown, a flexible solar cell module of the present invention includes an upper skin 1, a first packaging adhesive film 21, a flexible solar cell array, a second packaging adhesive film 22, a support member, The third packaging adhesive film 23 and the lower skin 6 are supported by polymethacrylimide foam board 5 .
[0035] The thickness of polymethacrylimide foam board 5 is preferably 0.5mm~3mm, and the density is preferably 30 Kg / m 3 ~100Kg / m 3 , compressive strength 0.3MPa~7.5MPa, compressive modulus 20MPa~200MPa, tensile strength 0.8MPa~8MPa, tensile modulus 40MPa~400MPa, torsional shear strength 0.4MPa~7MPa, torsional shear modulus 10MPa~200MPa.
[0036] In the present embodiment, the thickness of polymethacrylimide foam board 5 is 0.5mm, and density 50 Kg / m 3 ~100Kg / m 3 , Compressive strength 1.0MPa, compressive modulus 44MPa, tensile strength 1.7MPa, tensile modulus 74MPa, torsional shear strength 0.92MPa, torsional shear modulus 23MPa.
[00...
Embodiment 2
[0048] like image 3 As shown, a flexible solar cell assembly of the present invention includes an upper skin 1, a first packaging film 21, a flexible solar cell array, a second packaging film 22, a lower skin 6. The third encapsulation film 23 and a supporting member, the supporting member is a polymethacrylimide foam board 5 .
[0049] In the present embodiment, the thickness of polymethacrylimide foam board 5 is 0.5mm, and density 50 Kg / m 3 ~100Kg / m 3 , Compressive strength 32MPa, compressive modulus 0.44MPa, tensile strength 23MPa, tensile modulus 0.88MPa, torsional shear strength 0.48MPa, torsional shear modulus 13MPa.
[0050] In this embodiment, the flexible solar cell array includes a plurality of crystalline silicon solar cell sheets 3 and photovoltaic ribbons 4 , and adjacent crystalline silicon solar cell sheets 3 are connected by photovoltaic ribbons 4 , finally forming a flexible solar cell array.
[0051] In this embodiment, the thickness of the crystalline si...
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Abstract
The invention discloses a flexible solar cell module and a preparation method and application thereof. The flexible solar cell module comprises upper skin, a first packaging adhesive film, a flexible solar cell array, a second packaging adhesive film, a supporting member, a third packaging adhesive film, and lower skin in a hot-pressing packaging in order from up to down, and the supporting member is a polymethacrylimide foam board. The preparation method comprises the steps of stacking the upper skin, the first packaging adhesive film, the flexible solar cell array, the second packaging adhesive film, the supporting member, the third packaging adhesive film, and the lower skin in order from up to down, and performing lamination. The flexible solar cell module is advantaged by low surface density, good bending and flexibility, suitability for being attached to airfoil curved surface, good reliability, no packaging problems such as warping, fragmentation, etc., and wide application in spacecrafts such as solar unmanned aerial vehicles, etc.
Description
technical field [0001] The invention belongs to the technical field of solar cells, and in particular relates to a flexible solar cell component for space, a preparation method and application thereof. Background technique [0002] High-altitude and long-endurance solar-powered drones have the advantages of high flight altitude, long working hours, wide coverage, flexible use, low operating costs, and no environmental pollution. The platform has a very broad application prospect. It uses solar radiation energy as power to continuously fly unmanned aerial vehicles at high altitudes for long periods of time. It uses photovoltaic cells to convert solar energy into electrical energy, and drives propellers to rotate through electric motors to generate flight power. During the day, solar-powered UAVs rely on solar cells laid on the surface of the body to convert absorbed solar radiation into electrical energy, maintain the operation of the power system, avionics and payloads, and...
Claims
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Application Information
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Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/048H02S30/10H01L31/18
CPCH01L31/0481H02S30/10Y02E10/50Y02P70/50
Inventor 周洪彪张建国杨晓生黄齐鸣
Owner 48TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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