Numerical calculation of scroll compressor geometry and assessment of its delivery

IF 2 Q2 ENGINEERING, MECHANICAL Frontiers in Mechanical Engineering Pub Date : 2023-09-01 DOI:10.3389/fmech.2023.1226857
Jurij Prezelj, N. Cerkovnik
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Abstract

This paper proposes innovative numerical methods for calculating the chamber volumes and tangential leakage gaps in a scroll compressor, a critical aspect of enhancing its performance and efficiency. It proposes two methods, namely, moving away from traditional analytical approaches and presenting a 0D model for mass flow delivery at varying rotational frequencies and discharge pressures. The first method utilizes the numerical identification of conjugate points with a minimum distance within the fixed and orbiting involute pair to calculate chamber volumes. This approach compensates for integration errors by considering the subareas defined by the normal distance of each involute to the other. The second method simplifies the process by assuming that the line defining the orbital angle intersects the involutes at the conjugate points, with volumes calculated using area discretization on triangles. Both methods underwent validation against three analytical calculations, showing an agreement within an overall uncertainty error of 3% for the maximum suction volume. The 0D model’s results were compared with Ma et al.'s hybrid method and actual measurements. Upon improving Ma’s model by accounting for intake air heating and negative pressure in the intake volume, a significant agreement between modeling and measurements was observed. This study concludes that the proposed numerical methods can enhance the accuracy of scroll compressor geometry calculation and mass flow delivery, considering the tangential gap.
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涡旋压缩机几何形状的数值计算及其输送性能评估
本文提出了计算涡旋压缩机腔体体积和切向泄漏间隙的创新数值方法,这是提高涡旋压缩机性能和效率的一个关键方面。它提出了两种方法,即摆脱传统的分析方法,并提出了在不同旋转频率和排放压力下质量流量输送的0D模型。第一种方法利用在固定和轨道渐开线副内具有最小距离的共轭点的数值识别来计算腔体体积。该方法通过考虑由每个渐开线到另一个渐开线的法向距离定义的子区域来补偿积分误差。第二种方法通过假设定义轨道角的线与渐开线在共轭点相交来简化过程,并使用三角形上的面积离散计算体积。两种方法都经过了三次分析计算的验证,在最大吸入体积的总体不确定度误差为3%的范围内显示出一致性。将0D模型的结果与Ma等人的混合方法和实际测量结果进行了比较。在通过考虑进气加热和进气容积负压来改进Ma的模型后,观察到模型和测量结果之间的显著一致性。研究表明,在考虑切向间隙的情况下,所提出的数值方法可以提高涡旋压缩机几何计算和质量流量输出的精度。
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来源期刊
Frontiers in Mechanical Engineering
Frontiers in Mechanical Engineering Engineering-Industrial and Manufacturing Engineering
CiteScore
4.40
自引率
0.00%
发文量
115
审稿时长
14 weeks
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