Solar cell module and preparation method thereof

A technology for solar cells and solar cells, applied in the field of solar photovoltaics, can solve the problems that space cells and ground components cannot be directly applied to stratospheric aircraft, and achieve the effects of shortening the preparation time, simplifying the production process, and achieving high-efficiency and low-temperature characteristics.

Active Publication Date: 2008-12-10
BEIHANG UNIV
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  • Abstract
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Problems solved by technology

[0003] The object of the present invention is to provide a light-weight and high-efficiency solar cell module and its preparation method. The solar cell module can reduce its own weight as much as possible while maintaining the high-efficiency output characteristics of the cell module, which is beneficial to the development of aircrafts in the stratosphere. application to solve the problem that space batteries and ground components in the prior art cannot be directly applied to stratospheric aircraft

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  • Solar cell module and preparation method thereof
  • Solar cell module and preparation method thereof
  • Solar cell module and preparation method thereof

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Embodiment Construction

[0031] Combine below figure 1 , 2 , 3, the solar cell module among the present invention and preparation method thereof are described further:

[0032] A kind of solar cell component of the present invention, as figure 1 , as shown in 2, it is composed of surface packaging film 1, transparent adhesive film 2, solar cell sheet 3, lightweight adhesive film A4, and insulating substrate 5 stacked sequentially from top to bottom; and the insulating substrate is composed of Insulating film 6 (polyimide film is used in this embodiment), carbon fiber board 7, lightweight adhesive film B8, honeycomb core 9, embedded parts 10, lightweight adhesive film C11, carbon fiber stacked in order from top to bottom Board 12 is composed.

[0033] The surface packaging film 1 is located on the outer surface of the battery module of the present invention, and plays a role in protecting the solar cells under the condition of sufficient light transmittance; the transparent adhesive film 2 is filled...

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Abstract

The invention provides a solar module which is composed of a surface sealing film, a transparent adhesive film, a solar cell, a lightweight adhesive film A and an isolated substrate which are stacked from the top to the bottom in order; and the isolated substrate is composed of an isolated film, a carbon-fiber sheet, a lightweight adhesive film B, a honeycomb core, a lightweight adhesive film C and the carbon-fiber sheet which are stacked from the top to the bottom in order, wherein the honeycomb core inside also needs to be appropriately added embedded parts according to concrete operating requirements. The technical scheme of a preparation method of the solar module comprises following steps: (1) making use of an oven to match with a vacuum air pump to process a pre-compacting treatment for a carbon-fiber prepreg; (2) meanwhile, processing a welding sequence of the solar cell; (3) processing a cutting sequence; (4) processing a laminating technology treatment; (5) processing post treatment procedures which in order are: removing raw edges, embedding strakes, arranging a junction box, measuring high voltage, cleaning the surface, measuring photo-electrical output characteristics, classifying components, and examining the appearance. The solar module has the advantages of lightweight, high efficiency and good low-temperature characteristics, and being very suitable to being applied in the stratosphere.

Description

1. Technical field: [0001] The invention provides a solar battery component and a preparation method thereof, belonging to the technical field of solar photovoltaics. 2. Background technology: [0002] Previous solar cell components were mainly used in space or on the ground, and the cell components designed for the working environment of stratospheric aircraft have not yet appeared. With the further expansion of the field of aerospace technology, the stratospheric aircraft used in the joint of aviation and spaceflight has become the focus of research in various countries. Among these aircraft, the stratospheric aerostat has attracted the most attention. Equipped with a solar cell array and a recyclable energy storage system, the stratospheric aerostat has the advantages of high flight altitude, long service life, regional residence, and low environmental pollution. It can be used for communication relay, early warning, detection and monitoring, High-altitude technology ver...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/048H01L31/0203H01L31/18
CPCY02E10/50Y02P70/50
Inventor 祝明孙康文吕明云武哲
Owner BEIHANG UNIV
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