燃气轮机压气机气动性能数值模拟及试验研究  

Numerical simulation and experimental research on the aerodynamic performance of a gas turbine compressor

作　　者：何中海 刘臻梁 吴亚东[1,2] HE Zhonghai;LIU Zhenliang;WU Yadong(School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China;Engineering Research Center of Gas Turbine and Civil Aero Engine of the Ministry of Education,Shanghai 200240,China)

机构地区：[1]上海交通大学机械与动力工程学院,上海200240 [2]燃气轮机与民用航空发动机教育部工程中心,上海200240

出　　处：《内燃机与动力装置》2024年第5期17-22,共6页Internal Combustion Engine & Powerplant

基　　金：国家科技重大专项(J2019-II-0004-0024);航空发动机及燃气轮机基础科学中心项目(P2022-B-V-004-001)。

摘　　要：为精确预测燃气轮机用压气机的气动性能,针对压气机实际工作中频繁出现的偏离设计点的起停工况,采用二维流线曲率法仿真分析不同转速下压气机部件的气动性能;并与搭建的亚音双级压气机试验台试验结果进行对比。结果表明:二维流线曲率法能够较好地预测燃气轮机亚音双级压气机气动特性,预测结果与试验结果相对误差在4.5%以内,可以为压气机设计和优化提供参考。To accurately predict the aerodynamic performance of compressors used in gas turbines,particularly under the frequently encountered startup and shutdown conditions that deviate from the design point in actual operations,a two-dimensional streamline curvature method is adopted to simulate and analyze the aerodynamic performance of compressor components at various rotational speeds.The results are then compared with those obtained from experimental tests conducted on a subsonic two-stage compressor test rig that is specifically set up.The results indicate that the two-dimensional streamline curvature method is highly proficient in predicting the aerodynamic attributes of subsonic two-stage compressors in gas turbines.The relative error between the prediction results and experimental data remains within 4.5%,indicating that this method can provide valuable insights for the design and optimization of compressors.

关 键 词：流线曲率法 亚音速压气机 压比 等熵效率 

分 类 号：TK221[动力工程及工程热物理—动力机械及工程]