飞机内循环燃油热管理系统响应延迟效应研究

  • 谭浩天 ,
  • 宁雷 ,
  • 许江涛 ,
  • 吕红庆 ,
  • 朱麟海 ,
  • 吴纪涛
展开
  • 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

  网络出版日期: 2026-02-09

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

  • TAN Hao-Tian ,
  • NING Lei ,
  • XU Jiang-Tao ,
  • XU Jiang-Tao Hong-Qing ,
  • ZHU Lin-Hai ,
  • WU Ji-Tao
Expand

Received date: 2025-11-18

  Revised date: 2026-02-06

  Online published: 2026-02-09

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。

本文引用格式

谭浩天 , 宁雷 , 许江涛 , 吕红庆 , 朱麟海 , 吴纪涛 . 飞机内循环燃油热管理系统响应延迟效应研究[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2026.33104

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.

参考文献

[1] 杨琳萱, 马慧才, 庞丽萍. 超声速民机环控系统设计及性能仿真研究[J]. 航空学报, 2025, 46(22):531585. YANG L X, MA H C, PANG L P, et al. Design and performance simulation of environmental control system for civil supersonic aircraft [J]. Acta Aero-nautica et Astronautica Sinica, 2025, 46(22): 531585 (in Chinese). [2] 杨世宇, 于海育, 林远方, 等. 具备消耗性热沉的燃油热管理系统性能分析及优化[J]. 航空学报, 2025, 46(4): 130897. YANG S Y, YU H Y, Lin Y F, et al. Performance analysis and optimization of fuel thermal manage-ment system with expendable heat sink[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(4): 130897(in Chinese). [3] 杨世宇, 林远方, 于海育, 等. 多温度限制点条件下燃油热管理系统热回油特性分析[J]. 清华大学学报(自然科学版), 2024, 64(5): 841-851. YANG S Y, LIN Y F, YU H Y, et al. Analysis of the hot fuel return characteristics for a fuel thermal mamanagement system with multiple temperature limit points[J]. Journal Tsinghua University(Sci & Technol), 2024, 64(5): 841-851. [4] VAN HEERDEN A S J, JUDT D M, JAFARI S, et al. Aircraft thermal management: Practices, technology, system architectures, future challenges, and oppor-tunities[J]. Progress in Aerospace Sciences, 2022, 128: 100767. [5] SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. Aircraft Thermal Endurance Op-timization Part II: Using A Simple Dual Tank To-pology And Robust Temperature Regula-tion[C/OL]//AIAA Scitech 2019 Forum. San Diego, California: American Institute of Aeronautics and Astronautics, 2019[2025-08-05]. [6] SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. Aircraft Thermal Endurance Op-timization Part I: Using A Mixed Dual Tank Topolo-gy And Robust Temperature Regula-tion[C/OL]//AIAA Scitech 2019 Forum. San Diego, California: American Institute of Aeronautics and Astronautics, 2019[2025-08-05]. [7] 屠敏, 袁耿民, 薛飞, 等. 综合热管理在先进战斗机系统研制中的应用[J]. 航空学报, 2020, 41(6): 523629. TU M,YUAN G M, XUE F, et al. Application of in-tegrated thermal management in development of ad-vanced fighter system[J] Acta Aeronautica et Astro-nautica Sinica, 2020, 41(6) :523629 (in Chinese) [8] 成超乾, 于鹏, 谢宗齐, 等. 基于LNG的高速飞机热管理系统设计建模与分析[J]. 航空学报, 2023, 44(10): 127545. CHENG C Q,YU P,XIE Z Q,et al. Design simulation of thermal management system for hy-personic aircraft based on liquid natural gas[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(10): 127545 (in Chinese). [9] SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. Aircraft Thermal Endurance En-hancement Using A Dual Tank Configuration And Temperature Regulation[C/OL]//2018 AIAA Guid-ance, Navigation, and Control Conference. Kis-simmee, Florida: American Institute of Aeronautics and Astronautics, 2018[2025-08-05]. [10] DOTY J, YERKES K, BYRD L, et al. Dynamic Thermal Management for Aerospace Technology: Review and Outlook[J]. Journal of Thermophysics and Heat Transfer, 2017, 31(1): 86-98. [11] 王艾伦. 复杂机电系统(键合图—模态分析)方法研究[D/OL]. 中南大学, 2004. [12] WANG A. Bond Graph Method for the Dynamic Similarity Analysis of Complex Electromechanical System[J]. Journal of Mechanical Engineering, 2010, 46(01): 74. [13] THOMPSON A F, IEZZI A J, PANGBORN H C, et al. Combined Design and Open-loop Control Opti-mization for Propulsion, Power, and Thermal Man-agement of Hybrid-electric Aircraft[C/OL]//2023 IEEE Conference on Control Technology and Appli-cations (CCTA). Bridgetown, Barbados: IEEE, 2023: 955-962[2025-03-30]. [14] AKSLAND C T, TANNOUS P J, WAGENMAKER M J, et al. Hierarchical Predictive Control of an Un-manned Aerial Vehicle Integrated Power, Propulsion, and Thermal Management System[J]. IEEE Transac-tions on Control Systems Technology, 2023, 31(3): 1280-1295. [15] KOELN J P, PANGBORN H C, WILLIAMS M A, et al. Hierarchical Control of Aircraft Electro-Thermal Systems[J]. IEEE Transactions on Control Systems Technology, 2020, 28(4): 1218-1232. [16] PANGBORN H C, KOELN J P, WILLIAMS M A, et al. Experimental Validation of Graph-Based Hierar-chical Control for Thermal Management[J]. Journal of Dynamic Systems, Measurement, and Control, 2018, 140(10): 101016. [17] HU H. A steady-state simulation model of supple-mental cooling system integrated with vapor com-pression refrigeration cycles for commercial air-plane[J]. Applied Thermal Engineering 2020, 166: 114692. [18] DUAN Z, SUN H, WU C, et al. Flow-network based dynamic modelling and simulation of the tempera-ture control system for commercial aircraft with multiple temperature zones[J]. Energy, 2022, 238: 121874. [19] 胡沛, 何世伟, 余长贵, 等. 高空长航时无人机热管理技术发展及挑战[J]. 航空动力学报, 2024: 1-11. HU P, HE S W, YU C G, et al. Development of thermal management technologies for high-altitude long endurance unmanned aerial vehicles: challeng-es and perspectives[J]. Journal of Aerospace Power, 2024: 1-11. [20] 杜晨慧. 高超声速飞行器综合热管理及关键技术研究进展[J]. 装备环境工程, 2023, 20(1): 043-051. DU C H. Research Progress on Integrated Thermal Management and Key Technology of Hypersonic Vehicles[J]. Equipment Environmental Engineering, 2023, 20(1): 043-051. [21] 滕润航, 贺克伦, 赵甜, 等. 飞行器能源与热管理系统中多能流统一建模与分析方法[J]. 航空学报, 2023, 44(19): 128427. TENG R H, HE K L, ZHAO T, et al. Unified model-ing and analysis method of multi-energy flow for aircraft energy and thermal management system[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128427 (in Chinese).
文章导航

/