1.西安交通大学化学工程与技术学院,710049,西安
2.哈尔滨汽轮机厂有限责任公司,150046,哈尔滨
3.北京海鹰科技情报研究所,100074,北京
收稿:2026-07-20,
修回:2026-09-13,
录用:2026-10-13,
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梁钧茗, 王毅飞, 赵云云, 等. 压缩空气储能翅片管换热器翅片参数对传热性能影响的试验与数值研究[J/OL]. 西安交通大学学报,2026-10-13. http://zkxb.xjtu.edu.cn/zh/article/173923776/.
LIANG Junming, WANG Yifei, ZHAO Yunyun, et al. Experimental and Numerical Study on the Effects of Fin Parameters on the Heat Transfer Performance of Finned-Tube Heat Exchangers for CAES[J/OL]. JOURNAL OF XI’AN JIAOTONG UNIVERSITY,2026-10-13. http://zkxb.xjtu.edu.cn/zh/article/173923776/.
梁钧茗, 王毅飞, 赵云云, 等. 压缩空气储能翅片管换热器翅片参数对传热性能影响的试验与数值研究[J/OL]. 西安交通大学学报,2026-10-13. http://zkxb.xjtu.edu.cn/zh/article/173923776/. DOI:
LIANG Junming, WANG Yifei, ZHAO Yunyun, et al. Experimental and Numerical Study on the Effects of Fin Parameters on the Heat Transfer Performance of Finned-Tube Heat Exchangers for CAES[J/OL]. JOURNAL OF XI’AN JIAOTONG UNIVERSITY,2026-10-13. http://zkxb.xjtu.edu.cn/zh/article/173923776/. DOI:
对于压缩空气储能系统中压缩空气-水翅片管换热器的气侧热阻较大、翅片结构参数选取缺乏依据的问题,本文开展了翅片参数对换热器换热性能影响的试验与数值研究。基于工程实际换热器结构,设计并制造了13种不同翅片参数的试验样机,翅片密度覆盖512~1023 翅/m,翅片高度覆盖1.1~1.35 mm,并且搭建了0.6 MPa带压闭式换热试验平台,在雷诺数7000~40000范围内测试了各样机的传热性能。此外,本文建立翅片管束单周期三维数值模型,通过网格独立性验证和湍流模型对比,确定了适用于高压空气横掠翅片管束的数值计算方法。结果表明,翅片管单位面积传热强度与整体传热能力并不完全一致。翅片密度512 翅/m、翅高1.1 mm样机的传热系数最高,说明其单位面积传热强度最高;而翅片密度905 翅/m、翅高1.1 mm样机的
UA
值最大,表明其整体传热能力最佳。本文还基于试验数据建立了考虑雷诺数和翅化比影响的
UA
值预测关联式,关联式的决定系数
R
2
为0.979,可较好估算压缩空气储能工况下换热器的整体传热能力。本文研究结果可为压缩空气储能系统用换热器翅片参数选取及性能预测提供参
考。
Aiming at the high air-side thermal resistance and limited guidance for fin parameter selection in compressed air–water finned-tube heat exchangers for compressed air energy storage (CAES) systems
experimental and numerical investigations were conducted on the effects of fin parameters on heat transfer performance. Thirteen prototypes were designed and fabricated
with fin densities of 512–1023 fins/m and fin heights of 1.1–1.35 mm. Their performance was tested on a 0.6 MPa closed pressurized test platform over a Reynolds number range of 7000–40000. A three-dimensional single-period model of the finned-tube bundle was also developed. Grid independence and turbulence-model comparisons were performed to determine a numerical method suitable for high-pressure air crossflow. The results show that heat transfer intensity per unit area does not fully correspond to overall heat transfer capacity. The prototype with 512 fins/m and a fin height of 1.1 mm achieved the highest heat transfer coefficient
whereas that with 905 fins/m and a fin height of 1.1 mm exhibited the largest UA value. A UA correlation incorporating the Reynolds number and finning ratio was developed with a coefficient of determination of 0.979
enabling reasonable estimation of overall heat transfer capacity under CAES conditions. The results provide a basis for fin parameter selection and performance prediction of CAES heat exchangers.
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