Unfoldingantenna basic unit, unfoldingantenna and folding method based on origami

A technology of basic unit and folding method, applied in the field of aviation antenna, can solve the problems of small unfolding area, high cost, complicated unfolding mechanical structure, etc., and achieve the effects of reducing cost, saving space and flexible application.

Active Publication Date: 2018-12-11
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problems of complex unfolding mechanical structure, small unfolded area ratio and high cost in the traditional spac

Method used

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  • Unfoldingantenna basic unit, unfoldingantenna and folding method based on origami
  • Unfoldingantenna basic unit, unfoldingantenna and folding method based on origami
  • Unfoldingantenna basic unit, unfoldingantenna and folding method based on origami

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Experimental program
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specific Embodiment approach 1

[0025] Specific implementation mode one: combine figure 1 and figure 2 To illustrate this embodiment, this embodiment is based on an origami-based unfolded antenna basic unit, which includes a shape memory material connector 1, a heating device 2, and a plurality of substrates 3;

[0026] Each substrate 3 is connected by a shape-memory material connector 1 so that each substrate 3 can be folded. The shape-memory material connector 1 is used as a crease, and a heating device 2 is provided on the shape-memory material connector 1. The heating device 2 is powered by powered by;

[0027] The unfolded area of ​​the unfolded antenna basic unit is 4 times the folded area n times, n≥1, n is an integer.

specific Embodiment approach 2

[0028] Specific implementation mode two: combination figure 1 and figure 2 To illustrate this embodiment, in this embodiment, when n=1, the unfolded antenna basic unit has twelve folds, and the shape of the unfolded surface of the unfolded antenna basic unit is a square,

[0029] Wherein the first crease 5, the second crease 6, the third crease 7 and the fourth crease 8 have the same length, the fifth crease 9, the sixth crease 10, the seventh crease 11 and the eighth crease 12 have the same length, the ninth crease 13, the tenth crease 14, the eleventh crease 15 and the twelfth crease 16 have the same length, the first crease 5, the second crease 6, and the third crease 7 and the fourth crease 8 are connected end to end to form a square, and the four points of the square are set on the center line of the unfolded surface of the unfolded antenna basic unit, the fifth crease 9, the sixth crease 10, and the seventh crease The crease 11 and the eighth crease 12 are set on the ...

specific Embodiment approach 3

[0031] Specific implementation mode three: combination figure 1 and figure 2 To describe this embodiment, the length of the diagonal of the square formed by the first crease 5, the second crease 6, the third crease 7 and the fourth crease 8 in this embodiment is equal to the ninth crease 13, The lengths of the tenth crease 14, the eleventh crease 15 and the twelfth crease 16, the lengths of the ninth crease 13, the tenth crease 14, the eleventh crease 15 and the twelfth crease 16 are Twice the length of the fifth crease 9 , the sixth crease 10 , the seventh crease 11 and the eighth crease 12 .

[0032] Other compositions and connections are the same as those in the second embodiment.

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PUM

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Abstract

The invention provides an unfolding antenna basic unit, unfolding antenna and folding method based on origami. The invention relates to the field of aeronautical antennas, which solves the problems ofcomplicated deployment mechanical structure, small deployment area ratio and high cost of the traditional space deployable antenna structure. The invention comprises a shape memory material connecting piece, a heating device and a plurality of substrates. A shape memory material connector is used as a fold mark, and a heating device is arranged on the shape memory material connector, and the heating device is powered by a power supply. The expanded area of the basic unit of the expanded antenna is 4n times the folded area, n >= 1, n is an integer. The ratio of the unfolded area to the foldedarea is 4n, which can save the loading space to a great extent, thereby reducing the cost of aerospace emission. The plurality of unfolded antenna basic units of the invention can be combined and connected to realize different unfolded and folded area ratios. The invention is applicable to space launch.

Description

technical field [0001] The invention relates to the field of aerial antennas, in particular to a unfolded antenna basic unit, an unfolded antenna and a folding method. Background technique [0002] The rapid development of the aerospace industry puts forward higher and higher requirements for antennas. Due to the high power of the antenna required at present and the high transmission rate of data, the demand for large-aperture antennas is gradually increasing, and the space size of the vehicle is limited, so the structural form of the deployable antenna can be used to reduce the loading of the antenna Space, reduce the cost of launch. [0003] Most traditional space-deployable antenna structures use mechanical or inflatable deployment methods, which have problems such as complex deployment mechanical structure, small deployment area ratio, and high cost. Contents of the invention [0004] In order to solve the problems of complicated unfolding mechanical structure, small...

Claims

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Application Information

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IPC IPC(8): H01Q1/08
CPCH01Q1/085
Inventor 冷劲松刘彦菊刘立武孙健刘梦
Owner HARBIN INST OF TECH
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