Liu Shuyang, Cao Sukai, Han Zhihong, Li Shenshen, Li Qiang, Zhang Jian, Xu Huilong
New Engineering Industry College,Putian University, Putian, Fujian, 351100, China.
Hangzhou Ruhr New Material Technology Co., Ltd, China.
Heliyon. 2024 May 7;10(10):e30710. doi: 10.1016/j.heliyon.2024.e30710. eCollection 2024 May 30.
In this paper, in order to establish the energy separation mechanism of the vortex tube, the hydrodynamic behavior of the compressible fluid in the asymmetric cavity space is investigated, and a numerical model of the trajectory deflection behavior is deduced and established; in order to form the optimal design method of the structural parameters of the vortex tube, the force situation of the fluid microelements entering different regions of the vortex chamber of the vortex tube is analyzed, and the trajectory deflection equations are corrected by combining with the expansion behavior of the fluid and the characterizing equations of vortex strength, transportability, and vortex initiation characteristics are given. The characterization equations of vortex strength, transportability and vortex initiation characteristics are given, and the numerical simulation of their influence parameters is carried out; in order to realize the prediction of the vortex tube performance of a given structure, the multifactor Pearson thermodynamic map is used to correlate and analyze the experimental data of vortex tubes reported publicly in the past years, and the polynomial regression equations are designed and established for the prediction of the vortex tube's energy separation effect and the confidence level and the degree of coincidence of the prediction results are examined. The confidence level and degree of agreement of the prediction results were examined. It is found that: the trajectory deflection motion of the compressible fluid in the asymmetric cavity space is the result of the combined effect of structural air pressure bias and the expansion behavior of the incident fluid; in order to improve the vortex strength in the vortex tube, the vortex initiation chamber space should be as small as possible; the increase of the diameters of the hot-end pipe and the cold-end pipe is conducive to the enhancement of vortex strength, but at the same time, it weakens the vortex transport in the heat pipe; the vortex initiation chamber size has a negative correlation with the hot-end temperature rise, and the inlet fluid pressure has a The negative correlation between the size of the vortex chamber and the temperature rise at the hot end, the positive correlation between the increase of inlet fluid pressure and the resulting temperature rise, and the strong correlation between the inlet fluid pressure and the friction coefficient on the effect of energy separation; the predictive equations for the effect of energy separation obtained by the fitting are in good agreement with the real situation.
在本文中,为了建立涡旋管的能量分离机制,研究了非对称腔体内可压缩流体的流体动力学行为,推导并建立了轨迹偏转行为的数值模型;为了形成涡旋管结构参数的优化设计方法,分析了进入涡旋管涡旋腔不同区域的流体微元的受力情况,并结合流体的膨胀行为对轨迹偏转方程进行了修正,给出了涡旋强度、可传输性和涡旋起始特性的表征方程,并对其影响参数进行了数值模拟;为了实现对给定结构涡旋管性能的预测,利用多因素皮尔逊热力图对过去几年公开报道的涡旋管实验数据进行关联分析,设计并建立了多项式回归方程用于预测涡旋管的能量分离效果,并检验了预测结果的置信水平和吻合度。检验了预测结果的置信水平和吻合度。研究发现:非对称腔体内可压缩流体的轨迹偏转运动是结构气压偏差和入射流体膨胀行为共同作用的结果;为了提高涡旋管内的涡旋强度,涡旋起始腔空间应尽可能小;热端管和冷端管直径的增加有利于涡旋强度的增强,但同时会削弱热管内的涡旋传输;涡旋起始腔尺寸与热端温度升高呈负相关,入口流体压力与涡旋腔尺寸呈负相关,入口流体压力的增加与热端温度升高呈正相关,入口流体压力与能量分离效果上的摩擦系数呈强相关;拟合得到的能量分离效果预测方程与实际情况吻合良好。