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涡旋压缩机排气孔流动特性研究OA北大核心CSTPCD

Study on the flow characteristics of discharge port of a scroll compressor

中文摘要英文摘要

为了研究排气孔结构对短型线涡旋压缩机性能的影响,以一款排量为38 cm3的涡旋压缩机为例,建立了三维非稳态数值计算模型,并通过试验对模型进行了验证,误差在9.5%以内.利用此模型,分别研究了排气孔大小和形状对压缩机性能的影响.结果表明,当采用圆形排气孔时,随着孔径由5.2 mm增大到9.0 mm时,压缩机功耗降低了5.82%,总质量流量增加了1.09%,排气过程中压力波动以及上、下腔之间压力不平衡性逐渐增强;当采用腰形、圆弧形以及复合形的排气孔时,相比5.2 mm圆形孔,压缩机功耗有一定程度降低,总质量流量少量增加,排气过程中压力波动和上、下腔内压力不稳定性变化不明显,其中排气孔形状为复合形时,性能提升最明显,压缩机功耗降低了5.81%,总质量流量提升了1.26%;相比总质量流量,压缩机排气孔的改变对功耗影响更大.研究结果可为涡旋压缩机排气孔的结构优化提供参考.

In order to investigate the influence of the discharge port structure on the performance of the scroll compressor with short profile,a three-dimensional transient numerical model of scroll compressor with the displacement of 38 cm3 was established and verified with a deviation within 9.5%.The effects of the size and shape of the discharge port of the compressor were investigated separately.The results show that when the shape of discharge port is circular,with the increase of the port diameter from 5.2 mm to 9.0 mm,the compressor power consumption decreases by 5.82%.The total mass flow rate grows by 1.09%.The pressure fluctuation and the pressure unbalance between the upper chamber and lower chamber are enhanced obviously during the discharge process;When kidney,arc and composite shapes of discharge port are applied,compared with the 5.2 mm circular port,the compressor power consumption decreases to a certain extent,the total mass flow rate grows somewhat,and the pressure fluctuation and the pressure unbalance between the upper chamber and lower chamber do not change significantly.When the shape of discharge port is composite,the compressor power is reduced by 5.81%,and the mass flow rate is raised by 1.26%;Compared with the mass flow rate,the change of the discharge port has more significant impact on the power consumption.The study results can provide reference for optimizing the discharge port structure of scroll compressors.

夏阳;金公羽;史宇超;姜子琪;田雅芬;李康;张华

上海理工大学 能源与动力工程学院,上海 200093国网浙江省电力有限公司杭州供电公司,杭州 311500

机械工程

短型线涡旋压缩机排气孔结构流动特性能耗数值仿真

short profile scroll compressordischarge portflow characteristicenergy consumptionnumerical simulation

《流体机械》 2024 (007)

15-23 / 9

国家自然科学基金项目(52206016,51206022);浙江省电力有限公司科技项目(5211HZ230009)

10.3969/j.issn.1005-0329.2024.07.003

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