A semi-rigid solar cell module structure and a preparation method thereof

A solar cell and module structure technology, applied in the field of space solar cell arrays, can solve problems such as high reliability connection, and achieve the effects of small mechanical response, reliable structural connection, and reliable structure

Active Publication Date: 2019-01-18
SHANGHAI INST OF SPACE POWER SOURCES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to overcome the deficiencies of the prior art, the present invention is to develop a semi-rigid solar cell module stru

Method used

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  • A semi-rigid solar cell module structure and a preparation method thereof
  • A semi-rigid solar cell module structure and a preparation method thereof
  • A semi-rigid solar cell module structure and a preparation method thereof

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Embodiment Construction

[0030] The present invention will be described in more detail below with reference to the accompanying drawings of the embodiments of the present invention. However, this invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. In these drawings, the size and relative sizes of layers and regions may be exaggerated for clarity.

[0031] Now, the present invention will be further explained by describing preferred specific embodiments according to the present invention in detail.

[0032] like figure 1 As shown, the present invention provides a semi-rigid solar cell module structure, which is composed of solar cells 2, interconnection sheets (5-1, 5-2), module connection sheets 4, diodes 6 and glass cover sheets. The cover glass includes an...

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Abstract

The invention discloses a semi-rigid solar cell module structure and a preparation method thereof. The module structure comprises a solar cell, an interconnecting sheet, a module connecting sheet, a diode and a glass cover sheet. The glass cover sheet comprises an upper glass cover sheet and a lower glass cover sheet. The lower glass cover sheet is of an abnormal structure. The upper glass cover sheet is of the same structure as the solar cell, and the solar cell is enclosed between the upper glass cover sheet and the lower glass cover sheet. The solar cell, the diode and the module connectingpiece are connected through the interconnecting piece. The solar cell module provided by the invention has the advantages of high integration, reliable structure, small mechanical response of the solar cell module, and the diode does not occupy the power generation area of the solar cell, thus improving the space power generation capacity of the solar cell array and improving the space application capacity of the solar cell array.

Description

technical field [0001] The invention relates to the technical field of space solar battery arrays, in particular to a method for designing a semi-rigid solar battery circuit for spacecraft. Background technique [0002] A solar cell is a semiconductor device that uses the photovoltaic effect to directly convert light energy into electrical energy. A power supply system composed of solar cell circuits can provide energy for spacecraft, and semi-rigid solar cell circuits are one of them. The semi-rigid solar cell module is different from the flexible solar cell array and the semi-rigid solar cell array. The module itself is double-sided sealed with a glass cover, and the module and the substrate or substrate are connected together through the glass cover. However, the solar cell and the bypass diode are connected in the same way. Usually, the bypass diode is placed at the corner of the solar cell, and the solar cell and the bypass diode are integrated through the interconnect...

Claims

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Application Information

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IPC IPC(8): H01L31/044H01L31/048H01L31/05H01L31/18
CPCH01L31/044H01L31/0488H01L31/0504H01L31/188Y02E10/50Y02P70/50
Inventor 王志彬陈萌炯马聚沙王凯吴志渊姜德鹏刘婧陆剑锋马季军
Owner SHANGHAI INST OF SPACE POWER SOURCES
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