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本文确定了微型压缩机碟阀的主要气动性能,并由试验研究结果得到了流量系数和气流压力的关系式,借此可以使级工作过程数学模型更准确,并将应用于微型无油润滑活塞式压缩机结构最佳化。
In this paper, the main aerodynamic performance of the miniature compressor disc valve is determined and the relationship between the flow coefficient and the airflow pressure is obtained from the experimental results, so as to make the mathematical model of the working process more accurate and apply to the micro-oil-free piston Compressor structure optimization.