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刷式封严结构泄漏特性的数值研究
引用本文:白花蕾,王 伟,信 琦.刷式封严结构泄漏特性的数值研究[J].航空发动机,2013,39(5):34-36.
作者姓名:白花蕾  王 伟  信 琦
作者单位:中航工业沈阳发动机设计研究所,沈阳 110015
摘    要:为了简化工程设计,将刷束区域处理为多孔介质模型并建立控制方程,其区域内压力对空间坐标的导数作为动量方程中的源项,推导出动量源项中的黏性损失系数和内部损失系数,从而建立了模拟刷式封严结构泄漏流动的多孔介质模型。采用FLUENT软件对刷式封严结构的泄漏特性进行数值模拟,并根据试验结果对计算模型进行修正,使计算结果与试验结果比较吻合。用修正的多孔介质模型对刷式封严结构的泄漏流场进行了分析,分析结果具有一定的工程意义

关 键 词:刷式封严结构  泄漏流动  数值模拟  多孔介质  航空发动机

Numerical Study on Leakage Characteristics of Brush Sea
Authors:BAI Hua-lei  WANG Wei  XIN Qi
Abstract:In order to simplify engineering design, the bristle pack was treated as porous medium and the control equation was built up. The space rate of pressure change was regarded as the source term of momentum equation, deriving internal losing coefficient and viscous losing coefficient in the momentum source term to set up the porous medium model which can simulate the leakage through brush seal structure. The leakage of brush seal was numerical simulated based on the FLUENT software, modifying the computational model based on the test results, and the computational results were coincided with the test results. The flow field of leakage for the brush seal was analyzed by modifying porous medium model, which brings some sense in the engineering extent.
Keywords:brush seal  leakage flow  numerical simulation  porous medium  aeroengine
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