A solar cell module fixing structure and fixing method of a string-type semi-rigid plate

A technology of solar cells and fixed structures, applied in the field of spacecraft power supply, can solve problems such as unusability, and achieve the effect of firm bonding
CN105515503BActive Publication Date: 2018-01-16中电科蓝天科技股份有限公司

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
中电科蓝天科技股份有限公司
Publication Date
2018-01-16

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Abstract

The invention, which belongs to the technical field of the spacecraft power supply, discloses a solar cell module fixation structure of a string-tightening type semi-rigid board and a fixation method thereof. The fixation structure comprises a string-tightening type semi-rigid substrate and a solar cell module; and a tightened string is arranged on the string-tightening type semi-rigid substrate. The solar cell module fixation structure is characterized in that the tightened string is formed by a horizontal tightened string and a longitudinal tightened string; fixed buckles are fixed at tightened string intersection points of the horizontal tightened string and the longitudinal tightened string; cross-shaped grooves are formed in the lower surfaces of the fixed buckles; the tightened string intersection points of the horizontal tightened string and the longitudinal tightened string are fixed in the cross-shaped grooves by adhesives; and the lower surfaces of the fixed buckles are fixed on the solar cell module by adhesives. On the basis of the technical scheme, the reliability is high; the tightened string intersection points can be fixed effectively in an omnibearing mode; and firm bonding of the solar cell module and the tightened string of the string-tightening type semi-rigid substrate is realized.
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Description

technical field

[0001] The invention belongs to the technical field of spacecraft power supplies, and in particular relates to a solar cell module fixing structure and a fixing method of a string-type semi-rigid plate. Background technique

[0002] At present, solar panels for spacecraft are divided into two types: rigid panels and semi-rigid panels, and semi-rigid substrates are further divided into grid-type and string-type. The rigid plate structure is a carbon fiber layer pasted on both sides of the aluminum honeycomb core, and a layer of polyimide film is covered on the solar cell installation surface; the grid-type semi-rigid structure is a carbon fiber frame with a flexible glass fiber grid, and the grid is relatively dense. The hole area is generally 1cm 2 ;The string-type semi-rigid structure is a carbon fiber frame with flexible strings that cross vertically, horizontally and vertically. The strings are relatively sparse, and the area of ​​the string holes is gene...

Claims

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