ISSN   1004-0595

CN  62-1224/O4

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用于微重力试验的气磁混合悬吊单元研制

Development of An Air-Magnetic Hybrid Suspension Unit for Microgravity Testing

  • 摘要: 传统被动式跟随悬吊法应用中摩擦干扰力大的问题影响了微低重力试验的精度,本文中结合悬吊法和气浮法的优点,利用气体轴承极低摩擦力的特点,设计了一款气磁混合悬吊单元原理样机,以提高被动式跟随悬吊法微低重力试验的精度. 首先介绍了气磁混合悬吊单元的工作原理,对气磁模块的布局方案进行了初选,选择了环形气体止推轴承与中央磁吸力单元组合的结构形式. 设计了独特的永磁-电磁模块,并对其电磁吸力特性进行了分析,分析结果显示在气隙厚度为0.65 mm左右时,磁力能够保持在2 kN左右,得到了0.3~1.0 mm气隙长度下混合磁单元的磁力及刚度变化曲线. 气体止推轴承采用大块多孔石墨作为节流器,能够在较小的空间尺寸中实现最大的承载能力,应用有限元方法对多孔质气体轴承的承载能力进行了分析,并进行了网格无关性分析,确定了计算模型的规模. 对供气压力和渗透率等主要参数的影响规律进行了分析,分析结果显示选定的工作参数可在20 μm气膜厚度下实现2 kN的承载. 完成了气磁混合悬吊单元的结构设计,并试制了3台样机. 针对气浮轴承进行了多孔材料渗透率测试. 针对气磁混合悬吊单元,考虑到测试的安全性,设计了倒扣拉力法试验装置进行了气磁混合悬吊单元承载能力测试. 针对气磁混合单元的极限承载能力和承载-位移特性进行了测试. 基于恒定磁吸力及非线性磁吸力假设,将气磁混合单元的承载-位移特性转化为气体轴承的承载-位移特性,并与气体轴承承载能力的理论分析结果进行了比较. 试验结果显示:试制的3台样机其最大极限承载能力均在2.4 kN以上,在安全系数3的条件下,可以承载80 kg的重物悬挂;磁吸力设计过程中应当使用非线性假设进行计算校核,得出的气膜承载能力与理论分析能够较好地吻合.

     

    Abstract:
    The high frictional interference in traditional passive follow suspension methods has affected the accuracy of micro gravity tests. A prototype of air magnetic hybrid suspension unit was designed by utilizing the extremely low friction characteristics of air bearings to improve the accuracy of micro gravity tests with passive follow suspension methods in this article, which combined the advantages of suspension methods and air flotation methods. The operating principle of the air-magnetic hybrid suspension unit was introduced firstly, and the layout scheme of the air bearing and magnetic module was preliminarily selected. The structural form of the combination of annular air thrust bearing and central magnetic force unit was selected finally. The unique permanent magnet-electromagnetic module was designed to maintain the magnetic force at about 2 kN when the air gap thickness was about 0.65 mm. The electromagnetic force characteristics was analyzed for getting the change curve of the load capacity and stiffness under the range of 0.3~1.0 mm. The large porous graphite restrictor was used in air thrust bearings to achieve maximum load capacity in a smaller space dimension. The load capacity of air thrust
    bearing was analyzed by finite element method and the grid independence analysis was also executed for determining the scale of the computational model. The influence laws of main parameters, such as supply pressure and permeability were analyzed, and the load capacity of 2 kN could be achieved under the selected working parameters when the air film thickness was at 20 μm. The structural design of the air-magnetic hybrid suspension unit was completed and three prototypes were developed. The permeability of porous materials was tested for air bearing part. The load capacity of the air magnetic hybrid suspension unit was tested by reverse tension test method in order to avoid security risks, and the test device was also designed. The maximum bearing capacity and load-displacement characteristics of the air-magnetic hybrid unit were tested. Based on the assumption of constant magnetic force and nonlinear magnetic force, the load-displacement characteristics of the air-magnetic hybrid unit were transformed into the load-displacement characteristics of the air bearing, and was compared with the theoretical analysis results of the air bearing load capacity. The experimental results showed that the maximum bearing capacity of the prototypes was above 2.4 kN, under the safety factor of 3, it could carry the heavy suspension load of 80 kg, the magnetic force should be calculated and calibrated by using non-linear assumptions in design process, and the experimental results of air bearing load capacity could be in well agreement with the theoretical analysis.

     

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