Solar array and preparation method and application thereof

A solar array and printed circuit technology, applied in the field of solar cells, can solve the problems of large volume, weight and complex structure of solar arrays, achieve the effects of multiple payloads, reduce electrical connection procedures, and realize large-scale automated production

Active Publication Date: 2022-04-19
北京博瑞原子空间能源科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are problems of complex structure and the volume and weight of the final solar array

Method used

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  • Solar array and preparation method and application thereof
  • Solar array and preparation method and application thereof
  • Solar array and preparation method and application thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0103] This embodiment is a solar array and its preparation method.

[0104] The solar array of this embodiment includes FPC and flexible CIC cells arranged in sequence.

[0105] In this embodiment, some areas of the FPC are arranged sequentially as follows: figure 2 The following structure is shown:

[0106] Bottom layer 104 , glue layer 105 , printed circuit 106 , glue layer 105 and top layer 107 .

[0107] Wherein, the bottom layer 104 is made of polyimide with a thickness of 25 μm;

[0108] The material of the adhesive layer 105 is silica gel, and the thickness is 10 μm;

[0109] The printed circuit layer 106 is made of copper with a thickness of 25 μm;

[0110] The material of the adhesive layer 105 is silica gel, and the thickness is 10 μm;

[0111] The top layer 107 is made of polyimide with a thickness of 25 μm;

[0112] The glue layer 105 is made of silica gel and has a thickness of 10 μm.

[0113] The schematic diagram of the structure of the neutron circuit ...

Embodiment 2

[0135] This embodiment is a solar array and its preparation method.

[0136] The solar array of this embodiment includes FPC and flexible CIC cells arranged in sequence.

[0137] In this embodiment, some areas of the FPC are sequentially set as follows: figure 2 The following structure is shown:

[0138] Bottom layer 104 , glue layer 105 , printed circuit 106 , glue layer 105 and top layer 107 .

[0139] Wherein, the bottom layer 104 is made of polyimide with a thickness of 50 μm;

[0140] The material of the adhesive layer 105 is silica gel, and the thickness is 20 μm;

[0141] The printed circuit layer 106 is made of copper with a thickness of 50 μm;

[0142] The material of the adhesive layer 105 is silica gel, and the thickness is 20 μm;

[0143] The top layer 107 is made of polyimide with a thickness of 50 μm;

[0144] The material of the adhesive layer 105 is silica gel, and the thickness is 20 μm.

[0145] The schematic diagram of the structure of the neutron ci...

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Abstract

The invention discloses a solar array and a preparation method and application thereof. The solar array comprises an FPC and a plurality of flexible CIC batteries which are arranged in sequence. The FPC comprises a bottom layer, a printed circuit layer and a top layer which are arranged in sequence. A plurality of sub-circuits are arranged in the printed circuit layer; a plurality of positive electrode bonding pads and a plurality of negative electrode bonding pads are arranged on the sub-circuit; the positive electrode pads of the sub-circuits are connected through a wire and then current is led out to the negative electrode pad. And the sub-circuit and the flexible CIC battery are correspondingly arranged. According to the invention, the full flexibility of the solar cell array is realized, so that the solar cell array has smaller folding volume and lighter weight, and the folding volume is reduced by about 80% compared with a rigid solar array; and the weight is reduced to 30%. And the satellites with the same volume and weight have higher power and carry more effective loads, so that the cost of the satellites and the launching cost are saved.

Description

technical field [0001] The invention relates to the technical field of solar cells, in particular to a solar array and its preparation method and application. Background technique [0002] At present, the technology adopted by domestic spacecraft solar cell arrays is generally rigid array technology, and rigid substrates and rigid solar cells are their basic components. [0003] In the related art, a flexible solar array technology composed of a flexible substrate and a rigid CIC battery is used. The electrical connection process is as follows: first, the CIC batteries are connected in series according to the designed number of interconnection plates to form a string, and bus bars are welded at both ends, and then the external cables are welded to the bus bars to draw out electric energy; CIC, bus bars and external cables are all Bonded to the substrate. There are problems of complex structure and large volume and weight of the finally manufactured solar array. [0004] T...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/05H01L31/0392H01L31/18H05K1/18
CPCH01L31/0504H01L31/18H01L31/03928H05K1/189H05K2201/05Y02E10/50
Inventor 胡文涛杨文奕马涤非
Owner 北京博瑞原子空间能源科技有限公司
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