Investigation into Operation of Energy-Intensive Heat Exchangers with Many Plates

IF 0.9 Q4 ENERGY & FUELS
A. E. Baranov, A. E. Belov, D. N. Il’mov, V. A. Mavrov, A. S. Skorokhodov, N. I. Filatov
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Abstract

Heat exchangers in a gas turbine circuit for advanced space power facilities are innovative developments in the field of elaboration of heat exchangers meeting a set of technical and operating requirements. A design of a heat-transfer matrix consisting of a set of biconvex stamped plates with a specific surface relief is proposed. It enables construction of heat exchangers meeting the requirements for strength, stiffness, weight, and size under the specified operating conditions. The results of testing of heat exchangers made of 288 and 450 plates are presented. A nonuniformity of the coolant distribution among heat-transfer panels was found. Under the same operating conditions, it makes the thermal efficiency of a heat exchanger made of 450 plates lower than that of a heat exchanger made of 288 plates. Based on the analysis of test results, a mathematical model has been developed for the thermal and gas-dynamic design calculation of a heat exchanger with an arbitrary number of plates, which takes into account the effect of nonuniformity of the coolant flow through the channels between the plates. The calculation calls for determination of a temperature distribution along the length of each channel considering variable thermophysical properties of the coolant. For the mathematical model, a dimensionless dependence of the resistance coefficient and the Nusselt number on the Reynolds number was found in the Reynolds number range from 500 to 2000. Universal dependences enable simulation in both hot coolant paths consisting of identical interplate channels and cold coolant paths consisting of the same complete and half channels. The correlations for the hydraulic resistance coefficient and the Nusselt number versus the Reynolds number agree well with the known dependences obtained for corrugated heat-transfer surfaces of the same class. The mathematical model has been verified against experimental data. The effect of the scheme of connection of heat exchangers with different number of plates to a gas circuit is examined. The connection schemes are analyzed, and one of them is recommended as the most suitable for practice.

Abstract Image

Abstract Image

多板高能热交换器运行调查
摘要 先进空间电力设施燃气轮机回路中的热交换器是在满足一系列技术和操作要求的热交换器设计领域的创新发展。本文提出了一种由一组具有特定表面浮雕的双凸冲压板组成的换热矩阵设计。这样就能在规定的运行条件下建造出符合强度、刚度、重量和尺寸要求的热交换器。文中介绍了对由 288 块和 450 块板材制成的热交换器的测试结果。结果发现,换热板之间的冷却剂分布不均匀。在相同的工作条件下,这使得 450 板热交换器的热效率低于 288 板热交换器。根据对测试结果的分析,我们建立了一个数学模型,用于计算任意数量板片的热交换器的热能和气体动力设计,其中考虑到了冷却剂流经板片之间通道的不均匀性的影响。考虑到冷却剂的不同热物理性质,计算需要确定每个通道沿长度方向的温度分布。在数学模型中,发现在雷诺数 500 到 2000 的范围内,阻力系数和努塞尔特数与雷诺数之间存在无量纲关系。通用的依赖关系可以模拟由完全相同的板间通道组成的热冷却剂路径和由相同的完整半通道组成的冷冷却剂路径。水阻系数和努塞尔特数与雷诺数的相关性与同类波纹传热表面的已知相关性非常吻合。数学模型已通过实验数据进行了验证。研究了不同板数的热交换器与气路连接方案的影响。对连接方案进行了分析,并推荐了其中一种最适合实际应用的方案。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
1.30
自引率
20.00%
发文量
94
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