首页 | 本学科首页   官方微博 | 高级检索  
     

动压式指尖密封工作状态及其影响的流固耦合分析
引用本文:宗兆科,苏华. 动压式指尖密封工作状态及其影响的流固耦合分析[J]. 航空动力学报, 2010, 25(9): 2155-2162
作者姓名:宗兆科  苏华
作者单位:西北工业大学,机电学院,西安,710072;西北工业大学,机电学院,西安,710072
基金项目:国家自然科学基金(50575182);高等学校博士点基金(20060699021);陕西省自然基金(2009JM7002)
摘    要:建立了动压式指尖密封流固耦合的模型和计算方法,对转子起动时该密封的工作状态进行了流固耦合仿真;研究了泄漏率、耦合面径向力随时间的变化情况;提出了稳态下评价该密封性能的参数——泄漏率和耦合面径向力;分析了工况条件及流层参数对性能参数的影响.研究发现:转子起动至稳定阶段时,泄漏率迅速减少达到稳定状态,耦合面径向力达到最大值后有所降低并最终趋于稳定,满足密封低泄漏、非接触的工作要求.该工作为开展动压式指尖密封性能优化奠定了基础. 

关 键 词:周向收敛  动压式指尖密封  流固耦合  数值仿真  泄漏率  耦合面径向力
收稿时间:2009-08-08
修稿时间:2009-10-22

Analysis of fluid solid interaction of hydrodynamic finger seal's working state and its influence
ZONG Zhao-ke and SU Hua. Analysis of fluid solid interaction of hydrodynamic finger seal's working state and its influence[J]. Journal of Aerospace Power, 2010, 25(9): 2155-2162
Authors:ZONG Zhao-ke and SU Hua
Affiliation:School of Mechanical Engineering,Northwestern Polytechnical University,Xi'an 710072,China
Abstract:The fluid-solid coupling model and calculation method of circumferential convergent hydrodynamic finger seal were established.Numerical simulation of fluid solid interaction was conducted in the process of rotor startup.The time-dependent change of leakage rate and radial force of interface was analyzed.Two parameters,i.e.:leakage rate and radial force of interface,were used to evaluate the performance of finger seal at stable state.These two parameters were calculated and their changes were analyzed in different working conditions and structure parameters of fluid interface.Research shows that leakage rate decreases rapidly and tends to be stable,radial force of interface reaches the maximum and then decreases to be stable at last in the process of rotor startup,meeting the requirements of low leakage and non-contacting finger seal.The work provides a basis for optimizing hydrodynamic finger seal with good performance.
Keywords:circumferential convergent   hydrodynamic finger seal   fluid-solid coupling   numerical simulation   leakage rate   radial force of interface
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号