超高负荷压缩机流动分析OA
Flow Analysis of Ultra-high Load Compressors
压缩机转速越低,运行振动越小,寿命越长.为了实现压缩机低转速,提出一种应用大弯度、低损失的扩压叶型进行载荷系数1.78的超高负荷设计,使转速由常规700 r/min降低至330 r/min.采用数值计算方法对所设计的超高负荷压缩机级进行流场模拟,分析压缩机的性能和流动特点.结果表明:所设计的压缩机级设计点转静子叶片通道内流动损失小,具有较高的设计点效率;转子叶片通道不易产生流动分离,因此具有很高的稳定工作裕度.
The lower the speed,the smaller the operation vibration of the compressor,and the longer the service life.To achieve low compressor speed,a diffuser blade with large camber and low loss with 1.78 load coefficient of ultra-high load is designed,which reduces the speed from the conventional speed of 700 r/min to 330 r/min.By numerical calculation method,the flow field of the ultra-high load compressor stage is simulated,and the performance and flow characteristics of the compressor are analyzed.The results show that the flow loss in the compressor stage from design point to stator blade channel is small with high design point efficiency,and the rotor blade channel is not prone to generating flow separation,and has high stable operating margin.
吴敏怡;周正贵
南京航空航天大学能源与动力学院,江苏南京 210016南京航空航天大学能源与动力学院,江苏南京 210016
机械制造
压缩机超高负荷三维转静子气动特性
compressorultra-high loadthree-dimensional rotor and statoraerodynamic characteristics
《机械制造与自动化》 2026 (2)
86-90,5
国家科技重大专项(2017-Ⅱ-0001-0013)
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