节点文献

考虑冷却模型的燃气轮机热力循环计算模型的研究

Performance Prediction of a Three-Shaft MW-Level Gas Turbine Supported by Turbine Cooling Model

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 纪星星顾春伟刘红李朝坤

【Author】 JI Xing-Xing;GU Chun-Wei;LIU Hong;LI Chao-Kun;Key Laboratory for Thermal Science and Power Engineering of Ministry of Education,Department of Thermal Engineering,School of Mechanical Engineering,Tsinghua University;Southern China Aviation Industry Aviation Industry Co.,Ltd.;

【机构】 清华大学热能工程系热科学与动力工程教育部重点实验室中航工业南方航空工业集团有限公司

【摘要】 热力循环计算是燃气轮机性能分析和设计的重要手段。随着燃气轮机热力循环参数不断提高,热力循环计算必须要能对变工况下透平冷气需求量作出准确的估计,并考虑冷气在燃气轮机循环各环节的影响。本文基于适用于多轴燃气轮机热力循环计算模型,引入混合模型,结合气体掺混的Hartsel模型,建立了带冷却模型的热力循环计算模型。对某三轴MW级燃气轮机的变工况性能进行计算,通过与简化冷却模型的计算结果及实验数据的比较、分析,表明考虑混合模型的热力循环计算结果与实验数据具有更好的一致性。

【Abstract】 Thermodynamic cycle calculation is an important means for gas turbine performance analysis and design.With the improvement of gas turbine thermodynamic cycle parameters,it must be able to make accurate estimates of the coolant requirement for the turbine cooling at the off-design performance,and consider the coolant’s influence on the engine performance.The paper,based on the model for multi-shaft gas turbine performance calculation,establishes a prediction model for the engine performance with the introduction of hybrid cooling model and the gas mix Hartsel model.The concerned engine steady-state performance are calculated,and the better consistency of the prediction method is validated by comparison with the experimental data and the calculation results supported by simplified cooling model.

【关键词】 热力循环冷却模型气体掺混
【Key words】 thermodynamic cyclecooling modelgas mix
【基金】 国家863项目(No.2008AA050502)
  • 【文献出处】 工程热物理学报 ,Journal of Engineering Thermophysics , 编辑部邮箱 ,2015年02期
  • 【分类号】TK471
  • 【下载频次】230
节点文献中: 

本文链接的文献网络图示:

本文的引文网络