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A triangular prism unit modular planar antenna deployable mechanism

A technology of unit modules and unfolding mechanisms, applied in the aerospace field, can solve problems such as complex assembly and difficult fitting, and achieve the effects of low assembly difficulty, accurate fitting, and large folding ratio

Active Publication Date: 2022-07-12
ZHEJIANG SCI-TECH UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, tetrahedral or hexagonal prisms are mostly used as expandable structural units, but they have the disadvantages of complex assembly and difficult fitting of the working plane respectively.

Method used

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  • A triangular prism unit modular planar antenna deployable mechanism
  • A triangular prism unit modular planar antenna deployable mechanism
  • A triangular prism unit modular planar antenna deployable mechanism

Examples

Experimental program
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Embodiment Construction

[0019] The present invention will be further described below with reference to the accompanying drawings.

[0020] like figure 1 and figure 2 As shown, a triangular prism unit modular planar antenna deployable mechanism includes a driving module 2, a deployment chord 3 and a tensioning rope 4; the driving module 2 at the center position is arranged with N driving modules 2 evenly distributed along the circumferential direction, N≥6, the value of N in this embodiment is 6.

[0021] like image 3 , Figure 4 and Figure 5 As shown, the driving module 2 includes a central connecting block 2-5, a spring 2-1, a driving slider 2-2, a supporting circular tube 2-6, a driving link 2-3, a joint link 2-4 and a cylindrical pin 2 -7; both ends of the supporting circular tube 2-6 are fixed with a central connecting block 2-5 through cylindrical pins 2-7; The driving slider 2-2 is connected with the central connecting block 2-5 at the corresponding end position of the supporting circu...

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PUM

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Abstract

The invention discloses a deployable mechanism for a triangular prism unit modular plane antenna. The existing deployable mechanism units are complicated to assemble or difficult to fit on the work plane. The driving module at the central position of the present invention is arranged with N driving modules evenly distributed along the circumferential direction; the driving module includes a central connecting block, a spring, a driving slider, a supporting circular tube, a driving link, a joint link and a cylindrical pin; each phase Two adjacent peripheral drive modules are connected by two spaced chords, and each peripheral drive module is fixedly connected to the central drive module by two spaced unwinding chords. The invention can realize the two-dimensional plane folding of the large-scale antenna, the folding ratio is large, and the rigidity is high in the unfolded state; the triangular prism can be used to unfold the mechanism unit, and the fitting of the working plane is accurate.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and relates to a frame-type plane antenna deployable mechanism, in particular to a triangular prism unit modular plane antenna deployment mechanism. Background technique [0002] Compared with the rigid reflector antenna or the gas-filled reflector antenna, the frame antenna is a new type of deployable antenna. In the folded state, the volume of the antenna can be effectively reduced, and the carrying capacity of the rocket can be improved; when it reaches a predetermined orbit and is unfolded, it can provide better structural rigidity for the antenna. The frame-type antenna utilizes the idea of ​​modular expansion, and uses the modular unit mechanism to form the antenna support structure. By changing the number and size of the modular units, the expandable antenna support structure of different diameters can be obtained, so it is also called the modular antenna. . At present, tetrahedron or...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/10
CPCH01Q1/10Y02E10/50
Inventor 李健高兴文胡明孟少华赵德明高云杨景王丙旭吴梅
Owner ZHEJIANG SCI-TECH UNIV
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