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回热循环微型燃气轮机非线性数学模型

段建东 赵克 吴凤江 孙力 王要强

段建东, 赵克, 吴凤江, 孙力, 王要强. 回热循环微型燃气轮机非线性数学模型[J]. 航空动力学报, 2014, 29(1): 199-206. doi: 10.13224/j.cnki.jasp.2014.01.026
引用本文: 段建东, 赵克, 吴凤江, 孙力, 王要强. 回热循环微型燃气轮机非线性数学模型[J]. 航空动力学报, 2014, 29(1): 199-206. doi: 10.13224/j.cnki.jasp.2014.01.026
DUAN Jian-dong, ZHAO Ke, WU Feng-jiang, SUN Li, WANG Yao-qiang. Nonlinear mathematical model of regenerative cycle microturbine[J]. Journal of Aerospace Power, 2014, 29(1): 199-206. doi: 10.13224/j.cnki.jasp.2014.01.026
Citation: DUAN Jian-dong, ZHAO Ke, WU Feng-jiang, SUN Li, WANG Yao-qiang. Nonlinear mathematical model of regenerative cycle microturbine[J]. Journal of Aerospace Power, 2014, 29(1): 199-206. doi: 10.13224/j.cnki.jasp.2014.01.026

回热循环微型燃气轮机非线性数学模型

doi: 10.13224/j.cnki.jasp.2014.01.026
基金项目: 国家自然科学基金(51107018);高等学校博士学科点专项科研基金(20102302120013);中央高校基本科研业务费专项资金(HIT. NSRIF. 2010103)

Nonlinear mathematical model of regenerative cycle microturbine

  • 摘要: 建立了回热循环微型燃气轮机非线性动态模型,并考虑模型通用性采用压气机、回热器、透平的变工况解析通用特性建立了静态模型.根据设计参数进行数学模型的实例化,提出解析特性系数确定方法和计算机仿真实现的迭代次序.结果表明:静态特性仿真结果与Capstone C30实际数据之间存在微小偏差,通过更详细的参考数据校正特性解析公式系数可获得与实际数据更好的一致性;采用保持透平进气温度不变的最佳运行方式,空载到满载的动态时间为100s左右,回热器金属壁面平均温度由空载时750K降低到负载时670K.

     

  • [1] 张弛, 王建臣, 覃清钦, 等.微型燃气轮机乙醇燃烧室点火与熄火试验[J].航空动力学报, 2009, 24(9):1930-1936. ZHANG Chi, WANG Jianchen, QIN Qingqin, et al.Experimental research on ignition and lean blowout for micro gas turbine ethanol combustor[J].Journal of Aerospace Power, 2009, 24(9):1930-1936.(in Chinese)
    [2] 沈煜欣, 刘建军.考虑热传导的微型离心压气机设计与数值分析[J].航空动力学报, 2010, 25(4):897-901. SHEN Yuxin, LIU Jianjun.Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance[J].Journal of Aerospace Power, 2010, 25(4):897-901.(in Chinese)
    [3] 李聪, 方蜀州, 张平.微型涡喷发动机燃烧室设计研究[J].航空动力学报, 2008, 23(10):1783-1787. LI Cong, FANG Shuzhou, ZHANG Ping.Design and study of annular combustor for micro-turbine engine[J].Journal of Aerospace Power, 2008, 23(10):1783-1787.(in Chinese)
    [4] 黄国平, 温泉, 李博.微型涡喷发动机顶层设计研究[J].航空动力学报, 2003, 18(6):832-838. HUANG Guoping, WEN Quan, LI Bo.Top level design of micro turbine jet engine[J].Journal of Aerospace Power, 2003, 18(6):832-838.(in Chinese)
    [5] 刘爱虢, 翁一武.熔融碳酸盐燃料电池/燃气轮机混合动力系统启动停机过程特性分析[J].中国电机工程学报, 2012, 32(17):7-12. LIU Aiguo, WENG Yiwu.Analysis on startup and shutdown process of molten carbonate fuel cell/micro-gas turbine hybrid system[J].Proceedings of the Chinese Society for Electrical Engineering, 2012, 32(17):7-12.(in Chinese)
    [6] Rowen W I.Simplified mathematical representations of heavy-duty gas turbines[J]. Journal of Engineering for Power, 1983, 105(4):865-869.
    [7] Working Group on Prime Mover and Energy Supply Models.Dynamic models for combined cycle plants in power system studies[J].Transactions on Power Systems, 1994, 9(3):1698-1708.
    [8] Al-Hamdan Q Z, Ebaid M S Y.Modeling and simulation of a gas turbine engine for power generation[J].Journal of Engineering for Gas Turbines and Power, 2006, 128(2):302-311.
    [9] Nascimento M A R, Lora E S, Correa P S P.Biodiesel fuel in diesel micro-turbine engines:modelling and experimental evaluation[J].Energy, 2008, 33(2):233-240.
    [10] 闻洁, 李禄明, 徐国强, 等.全热换热器计算方法研究[J].暖通空调, 2009, 39(2):36-40. WEN Jie, LI Luming, XU Guoqiang, et al.Calculation method of total heat exchangers[J].Heating, Ventilating and Air Conditioning, 2009, 39(2):36-40.(in Chinese)
    [11] 张化光, 邓玮, 耿加民.发电用燃气轮机的非线性数学建模及稳定性分析[J].中国电机工程学报, 2007, 27(26):108-114. ZHANG Huaguang, DENG Wei, GENG Jiamin.Nonlinear modeling and stability analysis of gas turbine used for electricity generating[J].Proceedings of the Chinese Society for Electrical Engineering, 2007, 27(26):108-114.(in Chinese)
    [12] 董钺, 孔力.微型燃气轮机发电系统直流侧建模方法[J].电网技术, 2008, 32(3):13-17. DONG Yue, KONG Li.A modeling approach of DC link of micro-gas turbine generation system[J].Power System Technology, 2008, 32(3):13-17.(in Chinese)
    [13] WANG Wei, CAI Ruixian, ZHANG Na.General characteristics of single shaft microturbine set at variable speed operation and its optimization[J].Applied Thermal Engineering, 2004, 24(13):1851-1863.
    [14] Kim T S, Hwang S H.Part load performance analysis of recuperated gas turbines considering engine configuration and operation strategy[J].Energy, 2006, 31(2/3):260-277.
    [15] 梁红侠, 王秋旺, 王军伟.微型燃气轮机CW原表面回热器流动与换热的试验研究[J].工程热物理学报, 2006, 27(5):865-867. LIANG Hongxia, WANG Qiuwang, WANG Junwei.Experimental study on flow and heat transfer of CW primary surface recuperator for microturbine[J].Journal of Engineering Thermophysics, 2006, 27(5):865-867.(in Chinese)
    [16] ZHANG Na, CAI Ruixian.Analytical solutions and typical characteristics of part-load performances of single shaft gas turbine and its cogeneration[J].Energy Conversion and Management, 2002, 43(9):1323-1337.
    [17] Capstone Turbine Corporation. Technical reference capstone model C30 performance[EB/OL].[2013-08-22].http://www. capstoneturbine. com/ prodsol/ products/.
    [18] 李政, 王德慧, 徐大懋.微型燃气轮机变工况运行方式研究[J].汽轮机技术, 2005, 47(2):114-117. LI Zheng, WANG Dehu, XU Damao.Study on microturbine operation mode at off-design condition[J].Turbine Technology, 2005, 47(2):114-117.(in Chinese)
    [19] DUAN Jiandong, ZHAO Ke, XIAO Fang.Study on high-speed permanent magnet synchronous generators with PWM rectifier for microturbines[R]//www.Beijing:International Conference on Electrical Machines and Systems, 2011.
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出版历程
  • 收稿日期:  2012-11-21
  • 刊出日期:  2014-01-28

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