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刷式密封吹下效应诱发机理流固耦合数值研究
引用本文:杜宸宇,孙丹,刘永泉,战鹏,信琦. 刷式密封吹下效应诱发机理流固耦合数值研究[J]. 航空动力学报, 2021, 36(2): 310-319. DOI: 10.13224/j.cnki.jasp.2021.02.009
作者姓名:杜宸宇  孙丹  刘永泉  战鹏  信琦
作者单位:沈阳航空航天大学航空发动机学院辽宁省航空推进系统先进测试技术重点实验室,沈阳110136;中国航空发动机集团有限公司沈阳发动机研究所,沈阳110015;中国航空发动机集团有限公司航空发动机动力传输航空科技重点实验室,沈阳110015
基金项目:国家自然科学基金(52075346,51675351); 中国博士后科学基金(2018M633572); 辽宁省自然科学基金(2019-ZD-023)
摘    要:
分析了刷式密封吹下效应理论模型,建立基于arbitrary Lagrange-Euler(ALE)流固耦合方法的刷式密封吹下效应三维瞬态数值模型,在验证数值模型准确性的基础上,分别研究了刷丝轴向、径向和截面变形特性,量化分析了刷丝径向吹下量,揭示了刷式密封吹下效应诱发机理.研究表明:刷式密封吹下效应会减小刷丝径向间隙,...

关 键 词:刷式密封  吹下效应  诱发机理  arbitrary Lagrange-Euler(ALE)方法  流固耦合
收稿时间:2020-05-27

Numerical investigation on induced mechanism of blow-down effect of brush seals with fluid-structure interaction
DU Chenyu,SUN Dan,LIU Yongquan,ZHAN Peng,XIN Qi,SUN Dan,LIU Yongquan,ZHAN Peng,XIN Qi. Numerical investigation on induced mechanism of blow-down effect of brush seals with fluid-structure interaction[J]. Journal of Aerospace Power, 2021, 36(2): 310-319. DOI: 10.13224/j.cnki.jasp.2021.02.009
Authors:DU Chenyu  SUN Dan  LIU Yongquan  ZHAN Peng  XIN Qi  SUN Dan  LIU Yongquan  ZHAN Peng  XIN Qi
Affiliation:1.Liaoning Key Laboratory of Advanced Test Technology for Aerospace Propulsion System,School of Aero-engine,Shenyang Aerospace University,Shenyang 1101362.Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110115,China3.Key Laboratory for Power Transmission of Aero Engine,Aero Engine Corporation of China,Shenyang 110115,China
Abstract:
The theoretical model of blow-down effect of brush seals was analyzed. The three-dimensional transient numerical model of blow-down effect of brush seals based on arbitrary Lagrange-Euler(ALE) fluid-structure interaction method was established. The axial, radial and sectional deflection characteristics of bristles were studied respectively. The radial blow-down displacements of bristles were analyzed quantitatively, and the induced mechanism of blow-down effect of brush seals was revealed. The results showed that the leakage can be calculated more accurately with consideration of blow-down effect, because the bristle radial clearance was reduced by blow-down effect. Blow-down effect of brush seals presented an unsteady deflection with bristle oscillation. Compared with bristle cross section in the radial middle and end position of backing plate, blow-down effect and bristle oscillation of bristle tip were stronger. Bristles had more radial blow-down displacements and stronger bristle oscillation with the increase of inlet-outlet pressure ratio. When the inlet-outlet pressure ratio was 2, 3 and 4, the maximum radial blow-down displacement of bristles in the middle of bristle pack was 0.004, 0.010 mm and 0.019 mm, respectively, under the studied condition. The initial condition for the bristles with a certain circumferential lay angle and the radial pressure gradient in bristle pack contributed to the induced blow-down effect, and blow-down effect was further influenced by the normal pressure and the tangential friction between bristles. Blow-down effect of brush seals can be weakened by increasing the circumferential lay angle. 
Keywords:brush seals  blow-down effect  induced mechanism  arbitrary Lagrange-Euler (ALE) method  fluid-structure interaction
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