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A space-deployable inflatable antenna

An inflatable antenna and antenna technology, which is applied to inflatable antennas, antennas suitable for movable objects, antennas and other directions, can solve the problems of uncontrollable filling amount and filling rate, poor stability and controllability of the deployment process, and low deployment reliability. , to reduce the impact overload of deployment, increase the effective area in an orderly manner, and improve safety and reliability.

Active Publication Date: 2020-07-17
SPACETY CO LTD (CHANGSHA)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] In the inflatable flexible antenna and its deployment method provided by this patent, because the deployment process depends on the deployment of the mechanical structure and its driving mechanism is complicated, the reliability of the deployment is low. Both the amount and the filling rate are uncontrollable, so there are many uncontrollable factors in the deployment process. At the same time, the uncontrollable deployment process and the impact of the launch impact force during the satellite launch will cause obvious shock and vibration in the overall structure, and the anti-interference The ability is poor, although the storage ratio is improved, the stability and controllability of the unfolding process is poor

Method used

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  • A space-deployable inflatable antenna
  • A space-deployable inflatable antenna
  • A space-deployable inflatable antenna

Examples

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Embodiment Construction

[0041] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0042] The first-stage deployment assembly 11 at least includes a first inflatable support ring 1 and a second inflatable support ring 2 whose shapes are defined by arcs and have hollow inner chambers. The first inflatable support ring 1 and the second inflatable support ring 2 can be nested and connected to each other, so that the first antenna folded surface 5 can be compressed and folded in height and radial direction, so as to reduce the occupied volume of the first antenna folded surface 5 .

[0043] Preferably, the first inflatable support ring 1 and the second inflatable support ring 2 are arranged adjacent to and spaced apart from each other along the circumferential direction in such a manner that the centers of the two are located at the same point. Preferably, there are two first inflatable support rings 1 and two second inflatable support rings 2, both si...

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PUM

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Abstract

The invention relates to a space-expandable inflatable antenna. The inflatable antenna at least includes a flexible antenna folding surface and an unfolding assembly. The unfolding assembly is sequentially driven by the inflation pressure as a driving force and is respectively connected to at least one flexible antenna folding surface at different heights. The two-stage deployment assembly is composed of a first-stage deployment assembly that can expand outwards under the driving force of the inflation pressure applied to it to drive at least part of the folding surface of the flexible antenna. After the first-stage deployment assembly expands to When the first stage is fully unfolded, the second stage unfolding assembly expands stepwise by releasing the shape memory effect of the shape memory material plate on the folding surface of the flexible antenna due to the driving force applied to it, so that the flexible antenna is folded Incomplete or complete spatial deployment is carried out step by step from bottom to top in a controllable way to increase the effective deployment area and reduce the deployment impact overload.

Description

technical field [0001] The invention relates to the fields of aerospace technology and antenna technology, in particular to a space expandable inflatable antenna. Background technique [0002] The issue of antenna deployability is especially important as the size of satellites becomes smaller. While the sensors and operating electronics of miniaturized satellites can be scaled to extremely small volumes, the wavelengths of the signals used by such miniaturized satellites for communication do not scale accordingly. Given that the wavelength of a signal determines the size of the antenna used to transmit that signal, antennas for miniaturized satellites are still of similar size to larger satellites. Geostationary orbit satellites and deep space exploration activities require long-distance communication measurement and control, so it is very important to ensure that the receiving end has a large signal power, and the only way to ensure that the receiving end has a large signa...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H01Q1/08H01Q1/28
CPCH01Q1/08H01Q1/081H01Q1/288
Inventor 杜志贵杨峰任维佳向晓霞
Owner SPACETY CO LTD (CHANGSHA)
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