Automatic arrangement and mounting device and method for solar cell modules

A solar cell module and automatic technology, which is applied in the field of aerospace power supply, can solve the problems of difficulty in automatic placement, low precision of placement, and low production efficiency, so as to avoid glue shortage, high precision of placement and high work efficiency Effect

Active Publication Date: 2019-09-24
SHANGHAI INST OF SPACE POWER SOURCES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the placement process of solar cell arrays for space still relies on manual operation, which has the problems of low placement accuracy and low production efficiency.
Due to the great difference in the design status of solar cell array products among various models, the specifications of space-use solar cell array products vary widely, and there are protruding pressing points on the substrate at different positions. It is very difficult for the solar cell array to realize the automatic placement of solar modules

Method used

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  • Automatic arrangement and mounting device and method for solar cell modules
  • Automatic arrangement and mounting device and method for solar cell modules
  • Automatic arrangement and mounting device and method for solar cell modules

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Embodiment Construction

[0033] In order to describe the technical content, structural features, achieved goals and effects of the present invention in detail, the following will be described in detail in conjunction with the embodiments and accompanying drawings.

[0034] like figure 1 , the solar cell module automatic placement equipment of the present invention includes a base 1, a workbench 2, a feeding table 3, a first gantry system 4, a gluing device 5, a second gantry system 6, a patch device 7, and a computer control system 8 and other parts, wherein the workbench 2 is installed in the middle above the base, the loading table 3 is installed above the base 1 close to the edge of one side, and the first gantry system 4 and the second gantry system 6 are respectively installed on the top of the base 1 On both sides of the edge, the first gantry system 4 and the second gantry system 6 are set in a parallel state, the gluing device 5 is installed on the first gantry system 4, and the patch device 7...

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Abstract

The invention relates to an automatic arrangement and mounting device and method for solar cell modules, and belongs to the technical field of aerospace power supplies. The device comprises a base 1, a workbench 2, a feeding table 3, a gantry system 4, a glue coating device 5, a camera 6, a cell mounting device 7, a computer control system 8 and the like, wherein the workbench 2 is installed on the base 1 at the middle position, the feeding table 3 is installed on the base 1 at the position close to one side edge, the gantry system is installed at two side edges of the base 1, and the glue coating device 5, the camera 6 and the cell mounting device 7 are all installed on the gantry system 4; the glue coating device 5 can perform two-dimensional movement above the workbench 2 under the driving of the gantry system 4, and the camera 6 and the cell mounting device 7 can perform two-dimensional movement above the workbench 2 and the feeding table 3 under the driving of the gantry system 4. The device of the invention realizes the automatic arrangement and mounting of solar cell arrays of different specifications, and has the advantages of high adaptability, high arrangement and mounting precision and the like.

Description

technical field [0001] The invention relates to an automatic placement device and method for solar battery components, belonging to the technical field of aerospace power supplies. Background technique [0002] In the manufacturing process of solar cell arrays for space, it is necessary to paste the solar cell components on the specific position of the substrate according to the design drawings. When pasting, the silicone rubber is first coated on the substrate, and then the solar cell components are placed on the silicone rubber. And exert a certain pressure on the solar cell components to ensure firm bonding. At present, the placement process of solar cell arrays for space still relies on manual operation, which has the problems of low placement accuracy and low production efficiency. Due to the great difference in the design status of solar cell array products among various models, the specifications of space-use solar cell array products vary widely, and there are protr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/18H01L31/048
CPCH01L31/048H01L31/1876Y02E10/50Y02P70/50
Inventor 雷刚范襄沈静曼王凯金超陆剑峰马聚沙符春娥
Owner SHANGHAI INST OF SPACE POWER SOURCES
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