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离心压缩机密封及空腔流动的一维/三维耦合建模研究

唐永洪 席光 金志宏 王志恒

唐永洪, 席光, 金志宏, 王志恒. 离心压缩机密封及空腔流动的一维/三维耦合建模研究[J]. 航空动力学报, 2019, 34(9): 2038-2047. doi: 10.13224/j.cnki.jasp.2019.09.021
引用本文: 唐永洪, 席光, 金志宏, 王志恒. 离心压缩机密封及空腔流动的一维/三维耦合建模研究[J]. 航空动力学报, 2019, 34(9): 2038-2047. doi: 10.13224/j.cnki.jasp.2019.09.021
Research on one-dimensional/three-dimensional coupled modeling for seal and cavity flow of centrifugal compressor[J]. Journal of Aerospace Power, 2019, 34(9): 2038-2047. doi: 10.13224/j.cnki.jasp.2019.09.021
Citation: Research on one-dimensional/three-dimensional coupled modeling for seal and cavity flow of centrifugal compressor[J]. Journal of Aerospace Power, 2019, 34(9): 2038-2047. doi: 10.13224/j.cnki.jasp.2019.09.021

离心压缩机密封及空腔流动的一维/三维耦合建模研究

doi: 10.13224/j.cnki.jasp.2019.09.021
基金项目: 国家重点研发计划(2018YFB0606102)

Research on one-dimensional/three-dimensional coupled modeling for seal and cavity flow of centrifugal compressor

  • 摘要: 为了在保证数值预测精度的同时降低离心压缩机的建模复杂度,以一维密封泄漏计算替代完整的密封及空腔建模,开展了离心压缩机盖盘密封及空腔流动的源项建模方法研究。结果表明:基于源项方法的密封及空腔简化建模仅需在主流道建模基础上施加泄漏质量流量、总温和摩擦损失源项边界条件,即可较高精度地还原完整的盖盘密封及空腔建模的性能和关键流动细节。与完整建模相比,在全工况下源项建模预测的等熵效率的绝对偏差小于0.65%,总压比和等熵效率的相对性能偏差小于1%。该方法可在满足下游部件匹配设计精度需求的同时,减少50%以上的网格数量,并显著提高计算的经济性和收敛性。泄漏流量的计算精确度是影响源项建模法性能预测准确性的最关键因素,耦合建模可以采用一维计算中推荐的密封泄漏系数值。

     

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出版历程
  • 收稿日期:  2019-03-09
  • 刊出日期:  2019-09-28

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