Zero-gravity suspension type deployment test device

A test device and suspension technology, which is applied in the field of zero-gravity suspension test device, can solve the problems of difficult adjustment of precision, numerous configuration resources, inconvenient movement, etc., and achieve the effect of broad application prospects, flexible movement and large span

Active Publication Date: 2011-08-10
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to overcome the deficiencies in the existing technology, such as inconvenient overall movement of the air-floating deployment test device, difficulty in precision adjustment, numerous configuration resources, limited use, and potential safety hazards in the deployment process, the satellite solar cell array and antenna are solved under the ground gravity environment. To simulate problems such as the zero-gravity state of the environmental track, the purpose of the present invention is to provide a zero-gravity suspension type deployment test device

Method used

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  • Zero-gravity suspension type deployment test device
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  • Zero-gravity suspension type deployment test device

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Embodiment Construction

[0015] Preferred embodiments of the present invention will be described below in conjunction with the accompanying drawings.

[0016] The zero-gravity suspension type unfolding test device of the present invention is composed of a support system, a guide rail system, a suspension system, etc., and adopts a grid structure formed by stainless steel round pipes and spherical joints as the support system, and adopts stainless steel round pipes to be cold-rolled and polished to make guide rails The system uses a tubular dynamometer as a suspension system to balance the weight of the suspended object, thereby forming a zero-gravity simulation environment on the ground for the deployment test of the spacecraft solar array and antenna.

[0017] The accompanying drawing is a schematic structural view of a preferred embodiment of the zero-gravity suspension type deployment test device of the present invention. Such as figure 1 , 2 As shown, the device includes:

[0018] The support s...

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Abstract

The invention relates to a solar cell array and antenna deployment test device for spacecraft such as a satellite and the like, and provides a zero-gravity suspension type deployment test device which overcomes the shortcomings of the air-floating deployment test device in the prior art and solves the problem existing in simulation of the zero-gravity state of the environment orbit of the solar cell array and antenna of the satellite in the ground gravity environment. The zero-gravity suspension type deployment test device is characterized by comprising a support system [1], a guide rail system [2] and a hanging system [3]. The support system [1] comprises four upright frames and a horizontal frame. The guide rail system [2] comprises two longitudinal guide rails, multiple transverse guide rails and a guide rail hanger. The guide rail system [2] is mounted below the horizontal frame. The hanging system [3] comprises a rolling bearing frame, a tubular dynamometer and a connecting piece. Through the invention, the problems existing in simulation of the zero-gravity state of the environment orbit of the solar cell array and antenna of the satellite in the ground gravity environment and the like are solved, and beneficial effects of simple structure, convenience in use, strong adaptability and the like are obtained.

Description

technical field [0001] The invention relates to ground support equipment for spacecraft such as satellites, in particular to a zero-gravity suspension type deployment test device for solar cell arrays and antenna deployment tests of spacecraft such as satellites. Background technique [0002] In the development process of spacecraft such as satellites, the test of solar cell array and antenna is a basic and indispensable test content. Since the spacecraft is in a state of weightlessness when orbiting, the zero-gravity state that simulates the orbital environment when the solar array and antenna are deployed on the ground is called a key factor for the success of the experiment. At the same time, the deployment trajectory of the solar cell array and antenna is also an important factor to be considered for the test ground support equipment. [0003] At present, most of the deployment tests of solar cell arrays and antennas use air-floating deployment test devices. The overal...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G7/00
Inventor 姚骏吴远波顾志悦朱俭
Owner SHANGHAI SATELLITE ENG INST
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