Large working space variable driving parallel antenna seat mechanism

A working space and parallel technology, which is applied in the direction of antenna, antenna support/mounting device, electrical components, etc., can solve problems such as over-the-top problem and negative angle problem that are difficult to solve at the same time, to solve the problem of over-the-top tracking and ensure the service life , Guarantee the effect of signal strength

Pending Publication Date: 2017-05-10
NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to solve the problem of over-the-top and negative angle problems that are difficult to solve in the prior art at the same time, and to provide a variable-drive parallel antenna seat mechanism with large work

Method used

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  • Large working space variable driving parallel antenna seat mechanism
  • Large working space variable driving parallel antenna seat mechanism
  • Large working space variable driving parallel antenna seat mechanism

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Embodiment Construction

[0027] Such as figure 1 and figure 2 As shown, a large working space variable drive parallel antenna seat mechanism is provided, including a fixed platform 1 and a moving platform 2 arranged in parallel. The fixed platform 1 and the moving platform 2 have the same structure, and the fixed platform is a triangular plate or The fixed platform is a hexagonal plate, the moving platform is located above the fixed platform, and the fixed platform and the moving platform are connected by three moving branch chains evenly distributed along the circumferential direction, and the distance between the moving branch chains is 120 ° Evenly distributed.

[0028] Such as figure 1 As shown, each motion branch chain includes a swing rod 3 and a linear drive unit 4, one end of the swing rod and one end of the linear drive unit are hinged through a spherical pair 5, and the other end of the linear drive unit is the driving end. The driving end of the linear drive unit is hinged to the side w...

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Abstract

The invention discloses a large working space variable driving parallel antenna seat mechanism and belongs to the field of an antenna device. The antenna seat mechanism comprises a fixed platform, a moving platform and three motion branch chains having identical structures, wherein the motion branch chains comprise swing rods and linear driving units, the motion branch chains are respectively connected with the fixed platform and the moving platform through revolute pairs, and the revolute pairs connected with the fixed platform and the moving platform are respectively uniformly distributed along respective circumferences with an angle interval of 120 DEG. The antenna seat mechanism is a parallel mechanism, continuous tracking of the antenna for an any-attitude non-blind target area in a work scope can be realized, slip ring and joint equipment can be saved, a driving mode is variable and can adapt to large work space scope antenna demands, and the antenna seat mechanism further has properties of symmetric structure, compact structure, large rigidity, high directional precision, strong bearing capability and good dynamic characteristic.

Description

technical field [0001] The invention belongs to the field of antenna devices, and relates to a large working space variable drive parallel antenna seat mechanism, which is applied to fixed, vehicle-mounted, airborne and ship-borne satellite receiving antennas in aerospace remote sensing and satellite communications. Background technique [0002] The satellite antenna is generally composed of an antenna reflector connected with an antenna base. The antenna base is the support and orientation device of the antenna, which is used to enable the antenna to move according to the predetermined trajectory or follow the target. Its structure greatly affects the overall performance of the antenna. Performance. [0003] At present, there is a "blind cone" area in the zenith position of the classic pitch-azimuth antenna used in the world's known aerospace remote sensing, which cannot be continuously tracked "over the top". The size of the blind cone area (ie, the cone of the blind cone ...

Claims

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Application Information

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IPC IPC(8): H01Q1/12H01Q3/08
CPCH01Q1/12H01Q3/08
Inventor 李建军侯雨雷段艳宾窦玉超井国宁曾达幸
Owner NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP
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