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Single-degree-of-freedom infinitely expandable and deployable structure with quadrilateral components and application thereof

A quadrilateral, degree-of-freedom technology, applied to electrical components, antenna components, folded antennas, etc., can solve the problems of demanding geometric parameters, poor stability, unfavorable control, and difficult manufacturing process, and achieve good stability and repeatable folding and unfolding Good performance, easy to transport and store

Pending Publication Date: 2020-11-27
FUZHOU UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

They have five revolving pairs and seven revolving pairs for expandable units. There are a large number of revolving pairs, complex structures, poor stability, which is not conducive to manipulation, high manufacturing process difficulty, strict requirements on geometric parameters, poor deployment performance, and difficult to expand. Suitable for large-scale spatial deployable structures

Method used

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  • Single-degree-of-freedom infinitely expandable and deployable structure with quadrilateral components and application thereof
  • Single-degree-of-freedom infinitely expandable and deployable structure with quadrilateral components and application thereof
  • Single-degree-of-freedom infinitely expandable and deployable structure with quadrilateral components and application thereof

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Experimental program
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Embodiment 1

[0037] A single-degree-of-freedom infinitely expandable structure with quadrilateral components, including 9 identical quadrilaterals with 4 connecting vertices, all quadrilaterals with 4 connecting vertices are connected to other 4 adjacent ones with 4 The quadrilaterals connecting the vertices are connected in sequence.

[0038] In this embodiment, the number of quadrilaterals ranges from 4 to infinitely many, which can be determined according to any requirement of the user.

[0039] In this embodiment, the quadrilateral with 4 connected vertices is connected to its adjacent quadrangle with 4 connected vertices that is exactly the same through only one rotation joint.

[0040] In this embodiment, the quadrangle with 4 connected vertices has four revolving pairs, which are respectively numbered as the first revolving pair, the second revolving pair, the third revolving pair and the fourth revolving pair in sequence.

[0041] In this embodiment, the four revolving pairs of th...

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PUM

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Abstract

The invention relates to a single-degree-of-freedom infinitely expandable and deployable structure with quadrilateral components, which comprises a plurality of identical quadrangles with four connecting vertexes, wherein the quadrangles with the four connecting vertexes are sequentially and movably connected with other four adjacent quadrangles with the four connecting vertexes through revolute pairs. The quadrilateral unfolding device is simple in structure, the vertex of each quadrilateral is provided with one revolute pair, a plurality of quadrilateral units can be connected according to actual requirements of users, and the quadrilateral unfolding device has infinite unfolding performance and is suitable for unfolding large-scale space. The whole mechanism is in single-degree-of-freedom motion, and one axial cylindrical surface can be converted into the other axial cylindrical surface perpendicular to the axial cylindrical surface; the mechanism has the advantages of being good incontrollability, large in folding ratio and good in repeatable folding and unfolding performance.

Description

technical field [0001] The invention relates to an infinitely expandable and deployable structure, especially a single-degree-of-freedom infinitely expandable and deployable structure with a quadrilateral member and its application. Background technique [0002] The deployable structure is a new type of structure that has been rapidly developed over the past half century with the increasing area of ​​solar arrays required on spacecraft and the support requirements of satellite antennas. The deployable structure is folded into a specific shape during transportation and storage, and when it needs to work, under the action of external force, the structure gradually unfolds to reach the working state. Deployable mechanisms are widely used in solar cell arrays, satellite antenna support frames and other fields. [0003] Common deployable structures are mainly divided into non-rigid deployable structures and rigid deployable structures. Inflatable non-rigid deployable structures...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02S30/20H01Q1/12H01Q1/08
CPCH02S30/20H01Q1/1235H01Q1/084Y02E10/50
Inventor 杨富富卢帅龙陈昆精宋亚庆张俊
Owner FUZHOU UNIV