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Large-area unfoldable solar energy turnover plate

A solar energy, large-area technology, applied in the directions of astronautical equipment, astronautical aircraft, aircraft, etc., to achieve the effects of precise motion trajectory, smooth motion, strong flexibility and adaptability

Active Publication Date: 2016-05-04
GUANGXI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, there is no innovative invention design of a solar flap that can be deployed in a large area and flipped flexibly, and has high controllability

Method used

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  • Large-area unfoldable solar energy turnover plate
  • Large-area unfoldable solar energy turnover plate
  • Large-area unfoldable solar energy turnover plate

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Experimental program
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Effect test

Embodiment Construction

[0028] The technical solutions of the present invention will be further described below in conjunction with the drawings and embodiments.

[0029] Such as figure 1 , figure 2 , image 3 , Figure 5 and Figure 6 As shown, the large-area expandable solar panel of the present invention has a specific structure and connection relationship as follows:

[0030] The base 12 of the solar flap is welded on the satellite main body 13, the second side bar 32 is connected with the base 12 by the twelfth cylindrical pin 36, the first side bar 8 is connected with the second side bar 32 by the ninth cylindrical pin 33, The first rotating plate 7 and the second rotating plate 6 are installed on the ninth cylindrical pin 33, and can rotate around the ninth cylindrical pin 33, the second cylindrical pin 16 is welded on the top of the first side bar 8, and the compound hinge 5 is composed of a compound hinge The first rotating body 30, the second rotating body 31 of the compound hinge, th...

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PUM

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Abstract

The invention discloses a large-area unfoldable solar energy turnover plate. A base of the solar energy turnover plate is welded to a satellite main body, a second side rod is connected with the base through a twelfth cylindrical pin, a first side rod is connected with the second side rod through a ninth cylindrical pin, a first rotating plate and a second rotating plate are mounted on the ninth cylindrical pin and can rotate around the ninth cylindrical pin, the second cylindrical pin is welded to the top of the first side rod, and a combined hinge is formed by combining a first rotating body of the combined hinge, a second rotating body of the combined hinge, a third rotating body of the combined hinge and a fourth rotating body of the combined hinge. The metamorphic mechanism form is adopted for the solar energy turnover plate, greater controllability is achieved, the solar energy turnover plate has the secondary unfolding function, the angle of the solar energy plate can be adjusted flexibly, and sunlight is better received.

Description

technical field [0001] The invention relates to the field of aerospace machinery, in particular to a large-area expandable solar flap. Background technique [0002] In recent years, with the continuous development of human society, people's dependence on satellites has become stronger and stronger. Satellites for various purposes have been sent into space by humans, and some are equipped with astronomical observation equipment to conduct Astronomical observation; some are equipped with communication relay equipment, used to relay radio, television, data communication, telephone and other communication signals; some are equipped with scientific research equipment, which can be used for scientific research and special production under the condition of space without gravity, so , the status of satellites is becoming more and more important, but the premise that satellites need to complete these tasks is a continuous energy supply, which comes from solar flaps, so the status of ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/22
CPCB64G1/222
Inventor 王汝贵廖益丰张成东
Owner GUANGXI UNIV
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