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Static shaping film reflector antenna based on scissor-type truss structure

A truss structure and electrostatic forming technology, applied in the field of satellite antennas, can solve the problems of increasing the difficulty of system design and increasing the overall quality of the structure, and achieve the effects of reducing the design complexity, reducing the folded volume and simplifying the structure

Active Publication Date: 2017-01-04
XIDIAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existence of supporting structures will not only increase the overall quality of the structure, but also increase the difficulty of system design

Method used

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  • Static shaping film reflector antenna based on scissor-type truss structure
  • Static shaping film reflector antenna based on scissor-type truss structure
  • Static shaping film reflector antenna based on scissor-type truss structure

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Embodiment Construction

[0029] Below in conjunction with accompanying drawing, the present invention is described in further detail:

[0030] refer to figure 1 , figure 2 , the present invention includes a scissors-type truss structure 1, a flexible cable 2, a basic cable-net electrode 3, a film reflection surface 4, and an electrostatic power supply 5. The scissors-type truss structure 1 includes m expansion units, and a scissors-type The hinge 13 realizes the folding and unfolding of the entire antenna system, wherein m≥6, and is an integer multiple of 6; the flexible cables 2 are interleavedly arranged on the inside of the scissors truss structure 1, and are deployed together with the scissors truss structure 1 The joints are connected; the basic cable net electrode 3 is laid on the top of the flexible cable 2, and is connected with the scissors truss structure 1 at the joint of the unfolded unit; Connected and fixed above the basic cable net electrode 3; the electrostatic power supply 5 provid...

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Abstract

The present invention discloses a static shaping film reflector antenna based on a scissor-type truss structure. The static shaping film reflector antenna is composed of a scissor-type truss structure, a flexible cable, a basic cable net electrode, a thin film reflector and a static power supply. The scissor-type truss structure is configured to provide support for the whole structure, flexible cables are staggeringly arranged at the inner side of the scissor-type truss structure, the basic cable net electrode is connected with the scissor-type truss structure through the flexible cables, the thin film reflector is fixed on the basic cable net electrode and is connected and fixed with the scissor-type truss structure, and the static power supply is configured to provide high potential for the basic cable net electrode so as to provide grounding low potential for the thin film reflector. At folding, the flexible cables, the basic cable net electrode and the thin film reflector are folded in the free space of the scissor-type truss structure; and at unfolding, the flexible cables are tightened and are configured to support the basic cable net electrode, the thin film reflector forms the paraboloid shape under the action of the electrostatic force outputted by the static power supply. The static shaping film reflector antenna based on the scissor-type truss structure is small in the folding size and simple in structure, and can be used in the high-precision static shaping film reflector antenna.

Description

technical field [0001] The invention belongs to the technical field of satellite antennas, in particular to an electrostatically formed film reflector antenna based on a scissor truss structure in the field of satellite antennas, which can be applied to the design of high-precision electrostatically formed film reflector antennas. Background technique [0002] The rapid development of aerospace technology has put forward higher and higher requirements for spaceborne deployable antennas, mainly in two aspects: large aperture and high precision. Future communications, ground remote sensing and other fields also have potential demands for large-aperture, high-precision spaceborne antennas. At present, more mature space-borne reflector antennas, such as radial ribs, frame-type, peripheral truss and other mesh deployable reflector antennas, are difficult to meet the requirements of large aperture and high precision at the same time. For this reason, a variety of new concept ante...

Claims

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Application Information

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IPC IPC(8): H01Q1/12H01Q15/14
CPCH01Q1/1235H01Q15/14
Inventor 张树新姜文明杜敬利段宝岩张逸群宋立伟杨东武崔传贞
Owner XIDIAN UNIV
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