ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Performance analysis and optimization of fuel thermal management system with expendable heat sink
Received date: 2024-07-02
Revised date: 2024-07-25
Accepted date: 2024-09-23
Online published: 2024-09-29
Supported by
National Science and Technology Major Project of China (2019-Ⅲ-0001-0044)
To investigate the performance of a Fuel Thermal Management System (FTMS) with expendable heat sink under multiple temperature limit points, and to extend the system’s longest normally working time (thermal endurance) by optimizing the utilization of expendable heat sink, a simulation flow path using Liquid Methane (LM) as the expendable heat sink was constructed. Initially, the characteristics of hot fuel return were analyzed. The results indicate that the fuel heat sink consumption rate increases with increasing supply pump flow rate during normal operations. When the ram air is insufficient, the fuel return temperature to the fuel tank becomes the main limit temperature of the FTMS, and to meet the temperature requirement of hot fuel return, the system optimal supply pump flow rate is too high, resulting in a poor heat dissipation performance. In this case, the use of LM can not only cool the hot fuel return, but also further reduce the fuel heat sink consumption by reducing the optimal supply pump flow rate. Subsequently, the effect of the Middle Fuel Return Branch (MFRB) on system heat dissipation performance was explored. The results show that once the ram air is insufficient, the MFRB can not only increase the heat dissipation through combustion fuel, but also further enhance the system heat dissipation capability by decreasing the optimal supply pump flow rate as well. The fuel heat sink consumption rate under the standard condition without LM can be reduced by 17.62% in the new flow path. Next, the characteristics of LM supply flow were analyzed. The results demonstrate that the LM supply flow rate can be divided into the high efficiency, general, and low efficiency zones for LM according to the effect of using LM. Finally, a new dynamic supply strategy of LM was proposed. Under the standard condition, the thermal endurance can be improved by 9.21% and 27.44% compared to the constant low flow and high flow LM supply strategies, respectively.
Key words: thermal management system; heat sink; dynamic optimization; thermal endurance; fuel
Shiyu YANG , Haiyu YU , Yuanfang LIN , Xingang LIANG . Performance analysis and optimization of fuel thermal management system with expendable heat sink[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2025 , 46(4) : 130897 -130897 . DOI: 10.7527/S1000-6893.2024.30897
1 | VAN HEERDEN A S J, JUDT D M, JAFARI S, et al. Aircraft thermal management: Practices, technology, system architectures, future challenges, and opportunities[J]. Progress in Aerospace Sciences, 2022, 128: 100767. |
2 | MAHEFKEY T, YERKES K L, DONOVAN B D, et al. Thermal management challenges for future military aircraft power systems[J]. SAE Transactions, 2004, 113: 1965-1973. |
3 | HUANG H, SPADACCINI L J, SOBEL D R. Fuel-cooled thermal management for advanced aeroengines[J]. Journal of Engineering for Gas Turbines and Power, 2004, 126(2): 284-293. |
4 | A R, PANG L P, JIANG X Y, et al. Analysis and comparison of potential power and thermal management systems for high-speed aircraft with an optimization method[J]. Energy and Built Environment, 2021, 2(1): 13-20. |
5 | ZHOU Z Y, HUANG J. Mixed design of radar/infrared stealth for advanced fighter intake and exhaust system[J]. Aerospace Science and Technology, 2021, 110: 106490. |
6 | GERMAN B J. Tank heating model for aircraft fuel thermal systems with recirculation[J]. Journal of Propulsion and Power, 2012, 28(1): 204-210. |
7 | SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. Flight endurance enhancement via thermal management system control subject to multiple limitations[C]?∥AIAA Scitech 2020 Forum. Reston: AIAA, 2020. |
8 | HENEGHAN S, ZABARNICK S, BALLAL D, et al. JP-8+100-The development of high thermal stability jet fuel[C]?∥34th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1996. |
9 | DOMAN D B. Fuel flow control for extending aircraft thermal endurance part I: Underlying principles[C]?∥AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2016. |
10 | DOMAN D B. Fuel flow control for extending aircraft thermal endurance part Ⅱ: Closed loop control[C]?∥AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2016. |
11 | DOMAN D B. Fuel flow topology and control for extending aircraft thermal endurance[J]. Journal of Thermophysics and Heat Transfer, 2018, 32(1): 35-50. |
12 | SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. Aircraft thermal endurance enhancement using a dual tank configuration and temperature regulation[C]?∥2018 AIAA Guidance, Navigation, and Control Conference. Reston: AIAA, 2018. |
13 | HUANG G P, DOMAN D B, OPPENHEIMER M W, et al. Control of a switched mode fuel thermal management system[J]. Journal of Thermophysics and Heat Transfer, 2022, 36(1): 13-27. |
14 | HUANG G P, DOMAN D, OPPENHEIMER M, et al. Topology optimization of a fuel thermal management system[C]?∥AIAA Aviation 2019 Forum. Reston: AIAA, 2019. |
15 | SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. FLEX versus dual tank thermal management systems[C]?∥AIAA Scitech 2023 Forum. Reston: AIAA, 2023. |
16 | YANG S Y, LIN Y F, YU H Y, et al. Thermal management of fuel heat sink in aircraft via flow path optimization[J]. Applied Thermal Engineering, 2024, 246: 122880. |
17 | SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. N-tank continuous framework for thermal management to enhance thermal endurance[C]?∥AIAA Scitech 2024 Forum. Reston: AIAA, 2024. |
18 | SIGTHORSSON D, OPPENHEIMER M W, DOMAN D B. N-tank thermal management system framework for thermal endurance enhancement[C]?∥AIAA Scitech 2022 Forum. Reston: AIAA, 2022. |
19 | LENTS C E. Impact of weight, drag and power demand on aircraft energy consumption[C]?∥AIAA Propulsion and Energy 2021 Forum. Reston: AIAA, 2021. |
20 | 杨晓东, 庞丽萍, 阿嵘, 等. 高速飞行器燃油热管理系统飞行热航时[J]. 化工学报, 2020, 71(S1): 425-429. |
YANG X D, PANG L P, A R, et al. Thermal flight time of fuel heat management system for high speed vehicle[J]. CIESC Journal, 2020, 71(S1): 425-429 (in Chinese). | |
21 | 庞丽萍, 邹凌宇, 阿嵘, 等. 高速运载器燃油热管理系统优化[J]. 北京航空航天大学学报, 2019, 45(2): 252-258. |
PANG L P, ZOU L Y, A R, et al. Optimization of fuel heat management system for high-speed aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(2): 252-258 (in Chinese). | |
22 | 唐玫, 吉洪湖, 胡娅萍. 超声速飞行器综合热管理系统优化设计[J]. 推进技术, 2022, 43(1): 50-60. |
TANG M, JI H H, HU Y P. Optimal design of comprehensive thermal management system for supersonic vehicle[J]. Journal of Propulsion Technology, 2022, 43(1): 50-60 (in Chinese). | |
23 | 唐玫, 胡娅萍, 王强, 等. 飞行器简化模型热管理系统的非稳态仿真[J]. 重庆理工大学学报(自然科学), 2017, 31(3): 58-65. |
TANG M, HU Y P, WANG Q, et al. Unsteady simulation of thermal management system of a simplified aircraft model[J]. Journal of Chongqing University of Technology (Natural Science), 2017, 31(3): 58-65 (in Chinese). | |
24 | 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): 107-121. |
CHENG C Q, YU P, XIE Z Q, et al. Design simulation of thermal management system for hypersonic aircraft based on liquid natural gas[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(10): 107-121 (in Chinese). | |
25 | AFRIANTO H, TANSHEN M R, MUNKHBAYAR B, et al. A numerical investigation on LNG flow and heat transfer characteristic in heat exchanger[J]. International Journal of Heat and Mass Transfer, 2014, 68: 110-118. |
26 | 宋伟明, 孟继安, 梁新刚, 等. 一维换热器中温差场均匀性原则的证明[J]. 化工学报, 2008, 59(10): 2460-2464. |
SONG W M, MENG J A, LIANG X G, et al. Demonstration of uniformity principle of temperature difference field for one-dimensional heat exchangers[J]. CIESC Journal, 2008, 59(10): 2460-2464 (in Chinese). | |
27 | 王海鹰, 杨永敏, 单亚杰. 航空发动机燃油系统温升特性研究[J]. 制造业自动化, 2017, 39(7): 92-95, 118. |
WANG H Y, YANG Y M, SHAN Y J. Investigation on fuel temperature rise characteristics of an aero-engine[J]. Manufacturing Automation, 2017, 39(7): 92-95, 118 (in Chinese). | |
28 | WEN J, HUANG H R, LI H W, et al. Thermal and hydraulic performance of a compact plate finned tube air-fuel heat exchanger for aero-engine[J]. Applied Thermal Engineering, 2017, 126: 920-928. |
29 | 杨世铭, 陶文铨. 传热学[M]. 4版. 北京: 高等教育出版社, 2006: 243-252, 474-477, 555-559. |
YANG S M, TAO W Q. Heat transfer[M]. 4th ed. Beijing: Higher Education Press, 2006: 243-252, 474-477, 555-559 (in Chinese). | |
30 | SCHLUNDER E U. Heat exchanger design handbook[M]. New York: Hemisphere Publishing, 1983: 460-463. |
31 | ALPEREN M A, KAYABA?I E, KURT H. Detailed comparison of the methods used in the heat transfer coefficient and pressure loss calculation of shell side of shell and tube heat exchangers with the experimental results[J]. Energy Sources, Part A: Recovery, Utilization, and Environmental Effects, 2019, 45(2): 5661-5680. |
32 | 冯贤明. 空调制冷系统的稳态及动态特性模拟[D]. 桂林: 桂林电子科技大学, 2012. |
FENG X M. The steady and dynamic characteristics simulation of air-condition refrigeration system[D]. Guilin: Guilin University of Electronic Technology, 2012 (in Chinese). | |
33 | SáNTA R. The analysis of two-phase condensation heat transfer models based on the comparison of the boundary condition[J]. Acta Polytechnica Hungarica, 2012, 9(6): 167-180. |
34 | 王冬兰, 朱卫兵, 平登科, 等. 燃-滑油换热器壳侧换热特性研究[J]. 推进技术, 2016, 37(5): 900-906. |
WANG D L, ZHU W B, PING D K, et al. A study of heat transfer characteristics on shell-side of fuel-oil heat exchanger[J]. Journal of Propulsion Technology, 2016, 37(5): 900-906 (in Chinese). | |
35 | BRUNO T J, HUBER M L, LAESECKE A R, et al. Thermodynamic, transport, and chemical properties of reference JP-8: 6659[R]. Gaithersburg: National Institute of Standards and Technology, 2010. |
36 | BELL I H, WRONSKI J, QUOILIN S, et al. Pure and pseudo-pure fluid thermophysical property evaluation and the open-source thermophysical property library CoolProp[J]. Industrial & Engineering Chemistry Research,2014, 53(6): 2498-2508. |
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