Thin film type semi-rigid solar cell array and manufacturing method thereof

A technology for solar cell arrays and manufacturing methods, which is applied to circuits, photovoltaic power generation, electrical components, etc., and can solve the problems of heavy semi-rigid solar cell arrays, complicated manufacturing processes, and low production efficiency of semi-rigid solar cell arrays. Lightweight, fewer connection points, less risk of failure

Active Publication Date: 2014-12-24
SHANGHAI INST OF SPACE POWER SOURCES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] The problem that the present invention solves is that the production method of existing semi-rigid solar cell array has low production efficiency and the problem of complicated manufacturing process, and another problem that the present invention solves is the problem that existing semi-rigid solar cell array is heavier; To solve the problem, the present invention provides a thin-film semi-rigid solar cell array and its manufacturing method

Method used

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  • Thin film type semi-rigid solar cell array and manufacturing method thereof
  • Thin film type semi-rigid solar cell array and manufacturing method thereof
  • Thin film type semi-rigid solar cell array and manufacturing method thereof

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Embodiment 1

[0046] Such as figure 1 As shown, the thin-film semi-rigid solar cell array includes a substrate 1, a solar cell module 2 laid on one surface of the substrate 1, a connecting piece 3 arranged on the same surface of the substrate 1, and an inner plate arranged on the other surface of the substrate 1. cable 4. In this embodiment, the substrate 1 is made of lightweight film material or sheet material, such as glass fiber, carbon fiber, polyimide, etc., to reduce the weight of the cell array. The connection piece 3 , the intra-board cable 4 and the inter-board cable 6 are all thin metal sheets with a specific shape laid on the substrate. The connecting piece 3, the intra-board cable 4 and the inter-board cable 6 are made of metal materials that are easy to weld, have low resistance, soft quality and good toughness, preferably silver, copper or valveable alloy. The frame 5 is made of lightweight rigid material, such as aluminum alloy and carbon fiber composite material. Laying c...

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Abstract

The invention discloses a thin film type semi-rigid solar cell array and a manufacturing method of the thin film type semi-rigid solar cell array. The cell array comprises a substrate, solar cell components, connecting sheets, cables in the substrate and a frame, the substrate is made of light thin film materials or thin plate materials, the solar cell components are arranged on the front face of the substrate, the connecting sheets are metal sheets laid on the front face of the substrate, one end of each cable in the substrate is wound around the edge of the substrate to be connected with the corresponding connecting sheet, the frame is made of light rigid materials, and the substrate is fixed to the frame. Due to the fact that the substrate of the semi-rigid solar cell array is made of the light thin film materials or thin plate materials, the connecting sheets and the cables in the substrate are all metal sheets laid on the substrate, and the frame is made of the light rigid materials, the thin film type semi-rigid solar cell array has the advantages of being light, small in thickness and high in strength. In addition, the solar cell components, the cables in the substrate and the connecting sheets can be automatically laid, and therefore production efficiency is high, and manufacturing is easy.

Description

[0001] technical field [0002] The invention relates to power supply technology in the aerospace field, in particular to a thin-film semi-rigid solar cell array and a manufacturing method thereof. Background technique [0003] Most of the spacecraft are powered by solar cell arrays. The electric energy generated by the solar cell strings on the solar cell array is transmitted to the interior of the spacecraft through cables for use by the spacecraft. At present, the most widely used is the rigid solar cell array. The solar cell array uses an aluminum honeycomb rigid substrate. Although the rigidity of the solar cell array is good, it has the disadvantage of heavy weight. [0004] In order to overcome this shortcoming, a semi-rigid solar cell array has been developed at home and abroad. This cell array is laid with a flexible glass fiber mesh on a rigid frame, and the solar cell modules are installed on the grid of the glass fiber mesh by hooking. , install components such ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/042H01L31/048H01L31/18
CPCH01L31/188Y02E10/50Y02P70/50
Inventor 雷刚陈萌炯韦祎王志彬程志君金超
Owner SHANGHAI INST OF SPACE POWER SOURCES
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