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Method for manufacturing solar module

A technology of solar cells and manufacturing methods, applied in the direction of electrical components, final product manufacturing, sustainable manufacturing/processing, etc., can solve the problems of long scraping time, troublesome maintenance, affecting production capacity, etc., to avoid exposure to atmospheric environment, reduce Cost of production equipment and effect of improving productivity

Inactive Publication Date: 2011-04-20
吴静怡 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] However, this manufacturing method must use laser scraping machine and mechanical force scraping machine to define the effective area of ​​the battery module because the materials must be mixed and coated, and the substrate needs to be heated at high temperature. Expensive, cumbersome to maintain and take a long time to scrape, which affects its productivity
Furthermore, during the process of laser line drawing, local high temperature is generated in the scraping area, and the external oxygen or nitrogen may produce oxides or nitrides with the metal electrodes under this condition, resulting in an increase in contact resistance, which in turn leads to a decrease in the efficiency of the battery module.

Method used

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Embodiment Construction

[0032] In order to make the above and other objects, features, and advantages of the present invention more apparent, a detailed description will be given below with reference to the accompanying drawings.

[0033] image 3 One embodiment of the method for manufacturing a solar cell module having a copper indium gallium selenide (CIGS) thin film according to the present invention is shown. combine Figure 4As shown, in step 200, a substrate 252 is provided, and the substrate 252 is cleaned in advance. In step 202, a first mesh cover 270 is disposed above the substrate 252, wherein the first mesh cover 270 includes a plurality of first openings 272 arranged in an array to define a plurality of The first coating area 274 . The first mesh cover 270 can be made of metal.

[0034] combine Figure 5 , in step 204 , a plurality of bottom electrodes 254 are respectively sputtered to form on the first coating area 274 , wherein the bottom electrodes 254 are located above the subst...

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Abstract

The invention relates to a method for manufacturing a solar module. In the manufacturing method, an effective coating area is defined by a mesh cover; by using the mesh cover, each layer of film of the solar module can be directly and continuously formed under a vacuum environment, and the effective area of the solar module is not needed to be defined by a laser scraper, a mechanical scraper and other equipment. Therefore, the equipment cost and scraping process of the laser scraper and the mechanical scraper can be saved. The manufacturing method is particularly applied to a solar cell with a copper indium gallium selenium compound semiconductor film, and procedures in the production process can be reduced; therefore, the capacity efficiency can be improved.

Description

technical field [0001] The present invention relates to a method of manufacturing a thin-film solar cell module by using a metal mesh to define a coating area, in particular, a method for manufacturing a solar cell module of a copper indium gallium selenide (CIGS) semiconductor thin film. Sputtering film formation does not need to go through the process of laser scribing and mechanical scribing, thereby reducing the production process procedures and improving production efficiency. Background technique [0002] In recent years, copper indium gallium diselenide solar cells (Copper Indium Gallium Diselenide Solar Cell, hereinafter referred to as CIGS Solar Cell) have been developed since 1997 when the University of Maine (University of Maine) proposed that the battery efficiency is about 6%. The Energy Research Institute (NREL) published the best battery efficiency of 19.9% ​​in 2008, which has high efficiency and long-term stable performance. Therefore, the application range ...

Claims

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Application Information

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IPC IPC(8): H01L31/18C23C14/34C23C14/04C23C14/06
CPCY02P70/50
Inventor 吴静怡
Owner 吴静怡
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