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CRGT循环燃气轮机性能仿真

郑洪涛 张玉龙 杨仁

郑洪涛, 张玉龙, 杨仁. CRGT循环燃气轮机性能仿真[J]. 航空动力学报, 2012, 27(1): 118-123.
引用本文: 郑洪涛, 张玉龙, 杨仁. CRGT循环燃气轮机性能仿真[J]. 航空动力学报, 2012, 27(1): 118-123.
ZHENG Hong-tao, ZHANG Yu-long, YANG Ren. Simulation research of the CRGT cycle gas turbine performance[J]. Journal of Aerospace Power, 2012, 27(1): 118-123.
Citation: ZHENG Hong-tao, ZHANG Yu-long, YANG Ren. Simulation research of the CRGT cycle gas turbine performance[J]. Journal of Aerospace Power, 2012, 27(1): 118-123.

CRGT循环燃气轮机性能仿真

Simulation research of the CRGT cycle gas turbine performance

  • 摘要: 采用VC和MATLAB混合编程方法,进行了不同循环燃气轮机的变工况性能分析.其中,采用修正工程算法编制了工质热力性质计算程序,采用反向传播(BP)神经网络法建立了压气机和涡轮部件特性计算模型,采用模块化建模方法建立了简单循环、蒸汽回注(STIG)循环和化学回热(CRGT)循环性能仿真模型.仿真结果表明:在保持燃机几何结构和设计功率不变的条件下,STIG循环和CRGT循环均能降低燃气初温和提高循环热效率.其中,简单循环的热效率为35.16%,STIG循环的热效率可达到45%,CRGT循环的热效率可达到52.8%;为了进一步提高该型燃机的应用潜力和使用范围,可以将该型CRGT循环燃气轮机用于海水淡化应用中.

     

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出版历程
  • 收稿日期:  2011-01-18
  • 修回日期:  2011-06-03
  • 刊出日期:  2012-01-28

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