Deployable solid reflector antenna
A reflective antenna and antenna technology, applied in the field of aerospace satellite communications, can solve the problems of high cost, high storage rate, heavy weight, etc., and achieve the effects of low cost, low storage rate, and low weight
Active Publication Date: 2019-08-02
HUNAN AEROSPACE HUNAYU COMM TECH CO LTD
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- Description
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- Application Information
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Problems solved by technology
[0005] The present invention provides an expandable solid-surface reflective antenna to solve the technical problems that the solid-surface reflective antenna in the related art cannot be folded and compressed, has large storage rate, heavy weight and high cost
Method used
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[0030] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0031] refer to figure 1 , the preferred embodiment of the present invention provides an expandable solid-surface reflective antenna, including a support mechanism 10 used as a support reference, and a mechanism for controlling the expansion and collapse of the solid-surface reflective antenna along the length direction and / or width direction. Axial expansion assembly 20 and a plurality of strip-shaped solid-surface antennas 30 for combining to form reflector antennas, in this embodiment, strip-shaped solid-surface antennas 30 are a part of reflector antennas, and there are 19 pieces in total. Personnel can understand that the number here is only an example, not a limitation, and 19 pieces of ...
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The invention discloses a foldable fixed surface reflecting antenna. The foldable fixed surface reflecting antenna comprises a supporting mechanism used as a supporting benchmark, an axial unfolding assembly used for controlling the fixed surface reflecting antenna to be switched between unfolding and folding states in the length direction and / or the width direction, and multiple strip-shaped fixed surface antennas used for combining and forming the reflecting surface antenna; the axial unfolding assembly comprises an X-direction unfolding apparatus and a Y-direction unfolding apparatus; the supporting mechanism comprises a bracket assembly used for supporting the strip-shaped fixed surface antennas and a supporting base assembly used for driving the bracket assembly to move; the X-direction unfolding apparatus is connected with the supporting base assembly and used for driving the supporting base assembly to move in the length direction so as to unfold or fold the multiple strip-shaped fixed surface antennas in the length direction; and the Y-direction unfolding apparatus is connected with the bracket assembly and used for driving the bracket assembly to move in the width direction so as to unfold or fold the multiple strip-shaped fixed surface antennas in the width direction. The foldable fixed surface reflecting antenna disclosed in the invention can be folded ad compressed in the length and width directions and is low in accommodating rate, weight and cost.
Description
technical field [0001] The invention relates to the field of aerospace satellite communication, in particular, to a deployable solid-surface reflective antenna. Background technique [0002] With the wide application of satellite technology in mobile communication, radio astronomy, deep space exploration and space science, antennas are playing an increasingly important role. With the increase in the amount of transmitted information, large-aperture, high-precision antennas have become the development trend of antennas. In satellite communication, due to the limitation of the size of the fairing of the space vehicle and the consideration of reducing the cost as much as possible, the satellite antenna must be designed to have an expandable / foldable structure—that is, when the satellite is in the launch phase, the antenna needs to It is folded and folded to reduce its size so that it can be placed in the fairing, and when the satellite enters the predetermined space orbit, the...
Claims
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IPC IPC(8): H01Q1/12H01Q1/08H01Q15/16
CPCH01Q1/08H01Q1/1235H01Q15/161
Inventor 曾品松李完小包鹏李克郎彭兵
Owner HUNAN AEROSPACE HUNAYU COMM TECH CO LTD