A Porous Air Suspension Support System Applied to Full Physical Simulation

A support system, air suspension technology, applied in the direction of bearings, shafts and bearings, mechanical equipment, etc., can solve the problem of composite application of vacuum preload on the air-floating plane, and elaboration of relevant contents of the porous material restrictor, etc. problems, to achieve the effect of improving key indicators, preventing twisting and deflection, and reducing sudden tremors

Active Publication Date: 2018-08-21
北京太和科技有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For example, Shanghai Microelectronics Equipment Co., Ltd.'s invention patent publications "Air Float Support System" (Application No.: 201110130112.5) and "A Rotary Table Supported by Air Float" (Application No.: 201010022989.8), Chinese Academy of Sciences Changchun Optics, Fine Mechanics and Physics The invention patent publication of the research institute "Heavy-load air flotation support device for multi-legged optical installation and calibration" (application number: 201410187153.1) and the utility model patent of the 518th Research Institute of the Fifth Research Institute of China Aerospace Science and Technology Corporation "Large Bearing Air Float Support Device" (Application No.: 201120297229.8), there is no description of the use of porous materials as restrictors, nor the composite application of vacuum preload in the same air flotation plane

Method used

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  • A Porous Air Suspension Support System Applied to Full Physical Simulation
  • A Porous Air Suspension Support System Applied to Full Physical Simulation
  • A Porous Air Suspension Support System Applied to Full Physical Simulation

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Embodiment Construction

[0028] The air flotation support system using the porous restrictor proposed by the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. The drawings are in simplified form and use imprecise ratios, which are only used to facilitate and clearly assist the purpose of illustrating the embodiments of the present invention.

[0029] Such as figure 1 As shown, the air bearing support system using a porous medium restrictor includes a spring 1, a guide rod 12, a linear guide rail bushing 18, an anti-twist connecting rod 6, an air suspension support mechanism 3, a ball screw 2, and a two-way height adjustment screw 10 , lock nuts 8,9, air suspension support mechanism lock nut 4, upper beam 13, middle beam 14, lower beam 15, limit nut 16, load cell 17, volume reduction mound 22.

[0030] Described working platform is installed on the upper beam 13 by guide bar 12 and spring 1. The beams 13 , 14 , 15 are con...

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Abstract

The invention relates to a porous air-suspending supporting system applied to full physical simulation. According to the air-suspending supporting system, a vacuum pre-load with volume reduction hills is adopted for being combined with a porous flow controller; and the porous air-suspending supporting system mainly comprises a vertical guide mechanism, an adjustable supporting transverse beam, a bearing sensor (17) and an air-suspending supporting mechanism (3), wherein the air-suspending supporting mechanism (3) is formed by an air-suspending supporting shell (23), air nozzles (19 and 20) and the porous flow controller (7). The air-suspending supporting shell (23) is formed by air-suspending pressure-sharing structures (7, 22, 24, 25 and 26), a negative pressure vacuum cavity (26) and the volume reduction hills (22). According to the porous air-suspending supporting system applied to full physical simulation, the anti-dumping force is increased so that the system can be more stable; and the system stability is further improved.

Description

technical field [0001] The invention relates to a porous air-suspension support system applied to full physical simulation, in particular to a porous air-suspension support system with vacuum preload. Background technique [0002] The attitude control of the spacecraft is the key to ensure the reliable operation of the spacecraft. In order to ensure the high precision and reliability of spacecraft operation, before the spacecraft deorbits, it is necessary to conduct dynamic testing experiments on the sub-systems of the spacecraft (such as antennas, solar arrays, radiators, and shields, etc.) on the ground. One of the most important features of the space environment is zero gravity. How to realize the working state of the test mechanism under the condition of weightlessness in the gravity environment of the ground environment has always been a difficult problem in the ground test of the space structure, which needs to be carried out on the ground. The full-physics simulation...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16C32/06
Inventor 张修竹
Owner 北京太和科技有限公司
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