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