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飞机内循环燃油热管理系统响应延迟效应研究

谭浩天1,宁雷2,许江涛3,吕红庆4,朱麟海5,吴纪涛1   

  1. 1. 哈尔滨工程大学
    2. 上海航天控制技术研究所
    3. 哈尔滨工程大学航天工程系
    4. 哈尔滨工程大学航天与建筑工程学院
    5. 沈阳飞机设计研究所
  • 收稿日期:2025-11-18 修回日期:2026-02-06 出版日期:2026-02-09 发布日期:2026-02-09
  • 通讯作者: 许江涛

Analysis on Delay Characteristics of Response Modes of Aircraft Internal Circulation Fuel Thermal Management System

  • Received:2025-11-18 Revised:2026-02-06 Online:2026-02-09 Published:2026-02-09
  • Contact: XU Jiang-Tao

摘要: 引入内循环结构是提升飞机燃油热管理系统热沉利用效率的关键途径,但内循环会带来复杂的动力学特性,系统响应时间会随着流量分布出现不同程度的延迟。而热管理系统耦合了热力学过程与流体力学过程,系统内节点众多、相互耦合,表现高度的异质性与复杂性,常规的动力学建模方法难以表征其动态特性,无法分析延迟效应产生原因,难以针对性设计控制系统。本文提出基于图论的分层(流体-热力学)内循环燃油热管理系统动力学建模方法,利用所建模型揭示响应延迟问题产生的内在机理,并量化响应模态随流动状态分布的区域特征。结果表明延迟效应产生的本质原因是内循环改变了系统动力学的拓扑结构,增加了正反馈项,内循环的流量越大系统响应速度越慢。

关键词: 热管理, 内循环, 图论, 网络动力学, 模态分析

Abstract: Introducing an internal circulation loop boosts aircraft thermal management system (TMS) heat sink efficiency. However, it cre-ates complex dynamics with flow-dependent response delays. TMS couples thermodynamic and fluid dynamic processes, featur-ing numerous interconnected nodes that exhibit high heterogeneity and complexity. Conventional modeling fails to capture these dynamics or analyze delay causes, hindering control design. This paper proposes a hierarchical (hydraulic-thermal) graph-based modeling method for internal loop TMS dynamics. It reveals delay mechanisms and quantifies delay zones across flow states. The results show that the fundamental cause of the delay effect is that the internal circulation alters the topological structure of system dynamics and adds positive feedback terms, and the larger the flow rate of the internal circulation, the slower the system response speed.

Key words: Thermal Management System, Internal Circulation, Graph Theory, Network Dynamic, Modal Analysis

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