首页|期刊导航|哈尔滨工程大学学报|湿空气对压气机裕度边界性能的敏感性分析

湿空气对压气机裕度边界性能的敏感性分析OA

Sensitivity analysis of wet air on compressor performance at margin boundary

中文摘要英文摘要

针对湿空气条件对压气机失稳过程影响的问题,本文基于欧拉-拉格朗日多相流控制方程解析了压气机湿压缩的相变冷却过程,获得了压气机不同湿空气流态耦合过程的气热特性,评估了湿压缩过程流动传热对压气机裕度边界的敏感性.结果表明:在喷雾量为0.5%~8%、平均喷雾粒径为3~200 μm范围内,靠近压气机近失速边界时,湿压缩能降低流场温度25~49 K,并提升压气机效率0.25%~4%;而靠近压气机近喘振边界时,由于液滴蒸发作用降低,湿压缩所造成的流场温度变化小于10 K,且液滴的惰性阻力使转子叶片周边25~97 m/s范围的低速气流范围扩大,导致压气机喘振边界左移,稳定工作范围缩小.

Addressing the impact of wet air conditions on compressor instability processes,this paper analyzes the phase-change cooling process of wet compression in a compressor based on the Euler-Lagrange multiphase flow gov-erning equations.The aerothermal characteristics of different wet air flow regime coupling processes within the com-pressor were obtained,and the sensitivity of flow and heat transfer during wet compression to the compressor stabil-ity margin boundary was evaluated.The results indicate that,with spray flow rate ranging from 0.5%to 8%and av-erage droplet sizes from 3 μm to 200 μm,near the compressor's near-stall boundary,wet compression can reduce the flow field temperature by 25 K to 49 K,while improving compressor efficiency by 0.25%to 4%.However,near the compressor's near-surging boundary,due to reduced droplet evaporation,the temperature change in the flow field is less than 10 K.Additionally,the inertia resistance of the droplets expands the range of low-speed air-flow around the rotor blades(from 25 m/s to 97 m/s),causing the compressor surge boundary to shift left,thus re-ducing the stable operating range.

段昱;张鑫烨;胡永慧;陈燕;林阿强

潍柴动力股份有限公司,山东 潍坊 261061西北工业大学 动力与能源学院,陕西 西安 710129潍柴动力股份有限公司,山东 潍坊 261061西北工业大学 动力与能源学院,陕西 西安 710129西北工业大学 动力与能源学院,陕西 西安 710129

航空航天

压气机湿压缩裕度边界喷雾量喷雾粒径总温比总压比效率

compressorwet compressionmargin boundaryspray flow ratespray particle sizetotal tempera-ture ratiototal pressure ratioefficiency

《哈尔滨工程大学学报》 2026 (2)

290-298,9

中国博士后科学基金项目(2025T181167,2023M742834).

10.11990/jheu.202406028

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