基于AMESim和modelfrontier联合仿真优化的液冷循环制冷量分配方法

Li Haodong, Dong Sujun, J. Hongsheng, Li Yunhua
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引用次数: 0

摘要

飞机机载液冷循环各分支的流量分布是保证制冷性能和提高能源利用率的关键问题。由于多种因素的相关性,现有的机载液冷循环流量分配方法无法获得准确的流量分配结果。本文以所有设备的最高温度为优化目标,利用AMESim软件和modelfrontier平台联合仿真优化,解决了配流方案的优化设计问题。结果表明,与传统设计方法相比,采用基于仿真的优化设计方法可以充分发挥AMESim软件在仿真和性能指标计算方面的优势,以及modeFRONTIER软件在寻找最优分配方案方面的优势。可降低各支路装置的最高温度,有效提高冷却效果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A cooling capacity distribution method for liquid cooling cycle based on Co-simulation and optimization of AMESim and modeFRONTIER
The flow distribution of each branch of the aircraft's airborne liquid cooling cycle is a key issue to ensure refrigeration performance and improve energy utilization. Due to the correlation of multiple factors, the existing airborne liquid cooling cycle flow distribution method cannot achieve accurate flow distribution result. This paper takes the maximum maximum temperature of all equipment as the optimization goal, and the joint simulation-optimization of the AMESim software and the modeFRONTIER platform is used to solve the optimization design problem of the flow distribution scheme. The result shows that compared with traditional design methods, the use of simulation-based optimization design methods can give full play to the advantages of AMESim software in simulation and performance index calculation and modeFRONTIER software in searching for optimal allocation schemes. It can reduce the maximum temperature of each branch device and effectively improve the cooling effect.
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