欢迎访问机床与液压官方网站!

咨询热线:020-32385312 32385313 RSS EMAIL-ALERT
多微通道式气体静压节流器温度效应的数值仿真
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:

国家自然科学基金资助项目(51075378)


Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    气体静压节流器的变形量一般在微纳米级,难以采用实验的方法测得。对自主设计的多微通道式气体静压节流器,利用ANSYS软件对其受温度效应的影响进行研究。采用流固耦合分析方法,对供气温度和环境温度均为20 ℃,供气压强为(0.2~0.6) MPa,气膜厚度为10 μm、20 μm、30 μm、40 μm时节流器的温度分布及变形量进行仿真分析。研究结果表明:供气压强越大,气膜厚度越小,温度效应越明显,节流器内部温度和压强的降低引起的节流器变形越大。而温度变化对节流器的影响要明显强于压强变化对节流器的影响。其中,温降引起的最大变形量为1.011 6 μm,而压降引起的最大变形量为0.128 9 μm。

    Abstract:

    As the deformation of aerostatic restrictor is generally in the micro-nano level, it cannot be measured by experiment. On self-designed multi-channel restrictor, temperature effects are studied using ANSYS software. By using fluid solid coupling analysis method, the temperature distribution and deformation of the restrictor were analyzed with simulation when the supply air temperature and ambient temperature were all at 20 ℃, gas supply pressure was (0.2 ~ 0.6) MPa and gas film thickness was 10 μm,20 μm,30 μm and 40 μm. Study results show that by increasing the supply pressure and decreasing the film thickness, the temperature effect is more obvious, and deformation of restrictor is larger caused by decreasing of internal temperature and pressure of the restrictor. Moreover the thermal deformation is bigger than deformation caused by pressure drop. Among which, the maximum deformation is 1.011 6 μm caused by temperature decreasing, and the maximum deformation caused by pressure drop is 0.128 9 μm.

    参考文献
    相似文献
    引证文献
引用本文

李东升,李加福,胡佳成,程阳.多微通道式气体静压节流器温度效应的数值仿真[J].机床与液压,2014,42(19):116-119.
.[J]. Machine Tool & Hydraulics,2014,42(19):116-119

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2015-01-28
  • 出版日期: