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空气系统双腔模型的压力动态特性分析

丁水汀 车巍巍 刘传凯

丁水汀, 车巍巍, 刘传凯等 . 空气系统双腔模型的压力动态特性分析[J]. 北京航空航天大学学报, 2016, 42(4): 654-661. doi: 10.13700/j.bh.1001-5965.2015.0256
引用本文: 丁水汀, 车巍巍, 刘传凯等 . 空气系统双腔模型的压力动态特性分析[J]. 北京航空航天大学学报, 2016, 42(4): 654-661. doi: 10.13700/j.bh.1001-5965.2015.0256
DING Shuiting, CHE Weiwei, LIU Chuankaiet al. Dynamic pressure characteristic analysis for double-cavity model of air system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(4): 654-661. doi: 10.13700/j.bh.1001-5965.2015.0256(in Chinese)
Citation: DING Shuiting, CHE Weiwei, LIU Chuankaiet al. Dynamic pressure characteristic analysis for double-cavity model of air system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(4): 654-661. doi: 10.13700/j.bh.1001-5965.2015.0256(in Chinese)

空气系统双腔模型的压力动态特性分析

doi: 10.13700/j.bh.1001-5965.2015.0256
基金项目: 教育部长江学者创新团队“航空发动机复杂系统安全性”(IRT0905)
详细信息
    作者简介:

    车巍巍 男,博士研究生。主要研究方向:发动机瞬态空气系统及总体性能。 Tel.: 13716745697 E-mail: cww861028925@163.com;丁水汀 男,博士,教授,博士生导师。主要研究方向:燃气轮机热端旋转部件流动与换热机理及航空发动机适航性设计与验证技术。 Tel.: 010-82317435 E-mail: dst@buaa.edu.cn

    通讯作者:

    丁水汀, Tel.: 010-82317435 E-mail: dst@buaa.edu.cn

  • 中图分类号: V228.3

Dynamic pressure characteristic analysis for double-cavity model of air system

Funds: Innovation Plan of Aero Engine Complex System Safety by the Ministry of Education Chang Jiang Scholars of China (IRT0905)
  • 摘要: 当发动机突然加速或发生突发失效时,空气系统在短时间内由容腔效应和管道流体惯性所形成的压力波动将对某些空气系统零部件产生负面影响。在经过验证的模块化瞬态空气系统仿真程序的基础上,分析了双腔模型的管道不同部位和容腔的压力变化。重点考虑了关键元件的尺寸对压力变化的影响规律。结果表明,此瞬变过程中出现的压力波动与空气系统的几何结构尺寸密切相关。此模型分析方法可以作为研究整机空气系统瞬变过程的基础。

     

  • [1] 徐晓菊. 动力系统中瞬变流动的特性研究[J].机械管理开发,2010,25(5):50-52. XU X J.On characteristic research of transient flow in dynamic system[J].Mechanical Management and Development,2010,25(5):50-52(in Chinese).
    [2] 郭建明. 管道动力系统中非定常流动特性[J].科技情报开发与经济,2006,16(9):179-181. GU J M.The characters of the unsteady flow in the dynamical system of the pipeline[J].SCI-TECH Information Development & Economy,2006,16(9):179-181(in Chinese).
    [3] DUTTON J C, COVERDILL R E.Experiments to study the gaseous discharge and filling of vessels[J].International Journal of Engineering Education,1997,13(2):123-134.
    [4] THORNCROFT G P, GORDON J S,GORDON R.Modeling compressible air flow in a charging or discharging vessel and assessment of polytropic exponent[C]//Proceedings of ASEE Annual Conference and Exposition,2007.Chantilly,VA:American Society for Engineering Education,2007:AC 2007-2695.
    [5] CALCAGNI C, GALLAR L.Development of a one dimensional dynamic gas turbine secondary air system model-Part I:Tool components development and validation[C]//Proceeding of ASME Turbo Expo 2009:Power for Land Sea and Air.New York:ASME Press,2009,4:457-465.
    [6] CALCAGNI C, GALLAR L.Development of a one dimensional dynamic gas turbine secondary air system model-Part II:Assembly and validation of a complete network[C]//Proceedings of ASME Turbo Expo 2009:Power for Land,Sea and Air.New York:ASME Press,2009,4:435-443.
    [7] GALLAR L, CALCAGNI C.Time accurate modelling of the secondary air system response to rapid transients[J].Journal of Aerospace Engineering,2011,225(8):946-958.
    [8] 吕亚国,刘振侠, 黄生勤.航空发动机内流空气系统通用分析软件开发[C]//全国博士生学术论坛.北京:计算机仿真出版社,2009:99-103. LV Y G,LIU Z X,HUANG S Q.General analysis software design of aero-engine internal air system[C]//National Doctoral Academic Forum.Beijing:Computer Simulation Press,2009:99-103(in Chinese).
    [9] 候升平,陶智. 非稳态流体网络方法在发动机空气冷却系统中的应用[J].航空动力学报,2009,24(3):494-498. HOU S P,TAO Z.Study on application of unsteady fluid network to the air system in engine[J].Journal of Aerospace Power,2009,24(3):494-498(in Chinese).
    [10] 陶智,候升平. 流体网络法在发动机空气冷却系统设计中的应用[J].航空动力学报,2009,24(1):1-6. TAO Z,HOU S P.Study on application of fluid network to the design of air system in engine[J].Journal of Aerospace Power,2009,24(1):1-6(in Chinese).
    [11] 候升平,陶智. 非稳态流体网络模拟新方法及其应用[J].航空动力学报,2009,24(6):1253-1257. HOU S P,TAO Z.New simulation approach to the unsteady fluid network and the application[J].Journal of Aerospace Power,2009,24(6):1253-1257(in Chinese).
    [12] 刘传凯,刘海明, 李艳茹,等.强瞬变空气系统的模块化仿真建模[J].航空动力学报,2015,30(8):1826-1833. LIU C K,LIU H M,LI Y R,et al.Modularized simulation of air.Modularized simulation of air system with fast transient[J].Journal of Aerospace Power,2015,30(8):1826-1833(in Chinese).
    [13] 吴丁毅. 内流系统的网络计算法[J].航空学报,1996,17(6): 653-657. WU D Y.Network technique of internal system[J].Acta Aeronautica et Astronautica Sinica,1996,17(6):653-657(in Chinese).
    [14] 倪维斗,苟建兵,孙怠. 热动力系统流体网络及算法处理[J].系统仿真学报,1997,9(3):78-83. NI W D,GOU J B,SUN X.Research on fluid network in thermal power system[J].Journal System Simulation,1997,9(3):78-83(in Chinese).
    [15] 陈卓,周萍. 传递过程原理[M].长沙:中南大学出版社,2011:75-78. CHEN Z,ZHOU P.Principle of transport processes[M].Changsha:Central South University Press,2011:75-78(in Chinese).
    [16] 王华阁. 航空发动机设计手册-空气系统及传热[M].北京:航空工业出版社,2001:76-77. WANG H G.Aero engine design manual-air system and heat transfer[M].Beijing:Aviation Industry Press,2001:76-77(in Chinese).
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出版历程
  • 收稿日期:  2015-04-24
  • 修回日期:  2015-09-06
  • 网络出版日期:  2016-04-20

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