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Method for reliably connecting flexible thin-film solar cell and airship envelop

A technology of solar cells and flexible films, applied in circuits, photovoltaic power generation, electrical components, etc., to achieve strong wind resistance, broad military and civilian application prospects, and effective power supply

Active Publication Date: 2013-01-30
湖南航天远望科技有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the application of solar cell arrays on airships, there are problems of thermal coupling between solar cells and the skin of the airship, problems of assembling solar cells into arrays, and problems of connection between solar cell arrays and skins

Method used

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  • Method for reliably connecting flexible thin-film solar cell and airship envelop
  • Method for reliably connecting flexible thin-film solar cell and airship envelop
  • Method for reliably connecting flexible thin-film solar cell and airship envelop

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Embodiment 1

[0031] see Figure 1 to Figure 3 A method for reliably connecting a flexible thin-film solar cell to an airship skin comprises the following steps:

[0032] (1) Divide the airship skin 1 into several areas that need to be connected with flexible thin-film solar cells 7, and set two parallel lateral connection curtains 4 with A stainless steel grommets 6 in each area;

[0033] (2) On the airship skin 1 where the flexible thin-film solar cell 7 needs to be connected, several Velcro fasteners 2 for connecting the multi-layer heat insulation component 5 are arranged;

[0034] (3) Set several B velcros 3 corresponding to A velcro 2 on the multi-layer heat insulation component 5, and connect the multi-layer heat insulation component 5 to the airship cover through A velcro 2 and B velcro 3 Pi1 tight junctions;

[0035] (4) Set B stainless steel grommets 12 on the edges of both sides of the flexible thin-film solar cell 7;

[0036] (5) Pass the brocade rope 9 through the B stainles...

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Abstract

The invention discloses a method for reliably connecting a flexible thin-film solar cell and an airship envelop. According to the method, solar cells are interconnected through brocade silk ropes which penetrate through stainless steel buttonholes, thereby realizing assembly in an array manner; the solar cells and lateral connecting cord fabrics welded on the airship envelop are connected with each other through the brocade silk ropes which penetrate through the stainless steel buttonholes, thereby realizing the reliable connection between a solar cell array and the envelop; and a multi-layer thermal insulation assembly is closely connected with the airship envelop by employing nylon fasteners (groups), thereby realizing the isolation of waste heat of the solar cells and solving the problem of thermal coupling between the solar cells and the airship envelop. The connecting method can be widely applied to various airship platforms which generate power by solar energy and has wide military and civil application prospect.

Description

technical field [0001] The invention relates to the application of flexible thin-film solar cells on airships, in particular to the connection technology between flexible thin-film solar cells and airship skins. Background technique [0002] According to literature reports, at present, the following two methods are mainly used for the connection of flexible thin-film solar cells and airship skin abroad: "boat skin integration" and "hanging connection". However, there are no domestic reports on the application of flexible thin-film solar cells on airships and related connection methods. In the application of solar cell arrays on airships, there are problems of thermal coupling between solar cells and the skin of the airship, problems of assembling solar cells into arrays, and problems of connection between solar cell arrays and skins. Contents of the invention [0003] The invention aims to overcome the problems existing in the prior art, and provides a method for reliably...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/44H01L31/052
CPCY02E10/50
Inventor 陈琦周湘杰邓波彭疆
Owner 湖南航天远望科技有限公司
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