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Gravity balancing mechanical arm of satellite antenna expanding mechanism of multi-dimensional structure

A technology of satellite antenna and deployment mechanism, which is applied in the direction of measuring force, testing of machine/structural components, measuring devices, etc., can solve the problems of unsatisfactory simulation devices, and achieve the effects of reliable structure, precise posture following, and precise force control

Inactive Publication Date: 2015-12-23
SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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AI Technical Summary

Problems solved by technology

At present, the domestic research on the multi-dimensional frame antenna deployment mechanism is in the stage of mathematical model simulation and three-dimensional analysis. There is no device that can simulate its weightlessness on the ground. There is an urgent need for a gravity balance mechanism corresponding to the multi-dimensional frame antenna deployment mechanism to meet the needs of the deployment mechanism. Real-time gravity balance does not introduce additional moments, thereby providing a weightless environment for ground deployment tests

Method used

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  • Gravity balancing mechanical arm of satellite antenna expanding mechanism of multi-dimensional structure
  • Gravity balancing mechanical arm of satellite antenna expanding mechanism of multi-dimensional structure
  • Gravity balancing mechanical arm of satellite antenna expanding mechanism of multi-dimensional structure

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Embodiment Construction

[0030] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0031] Such as Figure 1~3 and Figure 4A As shown, the present invention includes a deployment drive motor 15, a mounting base 14, an antenna deployment follower arm 16, a pointing follower assembly 12, a three-dimensional adjustment device 19 for a suspension point, a constant force adjustment device 20, an antenna suspension tool 21, and an X-axis suspension tool 23 and the extension arm hanging tool 24, wherein the deployment drive motor 15 is fixedly connected to the mounting base 14, the output end of the deployment drive motor 15 is connected with one end of the antenna deployment follower arm 16, and the other end of the antenna deployment follower arm 16 is connected with Point to follow component 12. The antenna hanging fixture 21 and the X-axis hanging fixture 23 are respectively connected to the respective constant force adjustment devices 20 th...

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Abstract

The invention relates to a weight loss simulation device for ground testing of a satellite antenna expanding mechanism, particularly to a gravity balancing mechanical arm of a satellite antenna expanding mechanism of a multi-dimensional structure. The mechanical arm comprises an installation base, an antenna expanding following arm, a direction following assembly, an encoder, a Hooke's joint, an expansion driving motor, constant force adjustment devices, an X-axis suspension tool, a suspension point three-dimensional adjustment device, and an antenna suspension tool. The Hooke's joint is installed under the antenna expanding following arm and the direction following assembly. The encoder is installed at the hinge of the Hooke's joint. The constant force adjustment devices are installed under the Hooke's joint through suspension shafts and are connected with the X-axis suspension tool and the antenna suspension tool respectively by wire ropes. The X-axis suspension tool and the antenna suspension tool are used for connection with the X axis of the antenna expanding mechanism and an antenna respectively. The mechanical arm has many degrees of freedom and a reliable structure, is precise in pose following and force control, is safe in operation, and satisfies the need of weight loss simulation in ground testing of a satellite antenna expanding mechanism of a multi-dimensional structure.

Description

technical field [0001] The invention relates to a weightless simulation device for ground testing of a satellite antenna deployment mechanism, in particular to a multi-dimensional framed satellite antenna deployment mechanism gravity balance mechanical arm. Background technique [0002] In order to ensure the reliable deployment of the satellite antenna in orbit, the antenna deployment mechanism must be tested on the ground before the satellite is launched, which requires simulating the weightless state of the antenna deployment mechanism in space on the ground. At present, the domestic research on the multi-dimensional frame antenna deployment mechanism is in the stage of mathematical model simulation and three-dimensional analysis. There is no device that can simulate its weightlessness on the ground. There is an urgent need for a gravity balance mechanism corresponding to the multi-dimensional frame antenna deployment mechanism to meet the needs of the deployment mechanism...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M99/00G01L1/00
Inventor 王亚军徐志刚刘勇贺云贺喜斌
Owner SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI
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