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发动机动力模拟风洞试验中的空气桥技术

章荣平 王勋年 黄勇

章荣平, 王勋年, 黄勇. 发动机动力模拟风洞试验中的空气桥技术[J]. 航空动力学报, 2015, 30(4): 910-915. doi: 10.13224/j.cnki.jasp.2015.04.018
引用本文: 章荣平, 王勋年, 黄勇. 发动机动力模拟风洞试验中的空气桥技术[J]. 航空动力学报, 2015, 30(4): 910-915. doi: 10.13224/j.cnki.jasp.2015.04.018
ZHANG Rong-ping, WANG Xun-nian, HUANG Yong. Air bridge technology for engine power simulation test in wind tunnel[J]. Journal of Aerospace Power, 2015, 30(4): 910-915. doi: 10.13224/j.cnki.jasp.2015.04.018
Citation: ZHANG Rong-ping, WANG Xun-nian, HUANG Yong. Air bridge technology for engine power simulation test in wind tunnel[J]. Journal of Aerospace Power, 2015, 30(4): 910-915. doi: 10.13224/j.cnki.jasp.2015.04.018

发动机动力模拟风洞试验中的空气桥技术

doi: 10.13224/j.cnki.jasp.2015.04.018
基金项目: 

空气动力学国家重点实验室基金(SKLA2009A0103)

详细信息
    作者简介:

    章荣平(1981-),男,安徽庐江人,助理研究员,硕士,主要从事低速风洞试验技术研究.

  • 中图分类号: V211.7

Air bridge technology for engine power simulation test in wind tunnel

  • 摘要: 介绍了发动机动力模拟风洞试验中的空气桥设计技术和影响修正方法.通过自由度分析,选择了合理空气桥布局,采用有限元方法对空气桥关键受力梁进行了优化,建立了空气桥天平一体化数值模拟技术,使得空气桥和天平刚度更加匹配.通过这些设计及优化使得空气桥的作用力最小,并具有较强的克服压力影响、温度影响的能力.通过试验建立了空气桥附加刚度影响、内部压力影响、温度影响和内部流量影响的修正方法,进一步减小了空气桥对天平的影响.在8m×6m低速风洞进行了某大展弦比飞机全模涡扇动力模拟器(TPS)短舱动力模拟试验.试验结果重复性好,阻力系数精度达到0.0003,和相关文献吻合.这表明空气桥技术是成功的,满足了TPS短舱动力模拟试验要求.

     

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出版历程
  • 收稿日期:  2014-03-25
  • 刊出日期:  2015-04-28

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