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A comprehensive set of criteria for evaluating thermal management systems of aerial vehicles

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Abstract

Thermal management has become a significant concern in the design of advanced air vehicles. However, an effective evaluation method is needed when designers need to evaluate aircraft thermal management systems comprehensively. This paper proposes an evaluation method in which several evaluation directions concerned with thermal management systems (TMSs) are put forward to form an evaluation index system. The effect of temperature control, heat sink utilization efficiency, energy utilization efficiency, flight performance penalty, thermal endurance, space occupancy ratio, and economy are chosen as the direction of evaluation for TMS, considering its primary function, system performance, and impact on aerial vehicles. This method is comprehensive, intuitive, and user-friendly, along with the intensely subjective user-defined weight parameters, which provide rational metrics for thermal management techniques involved in aerial vehicles. The evaluation method could potentially be helpful for designers to comprehensively analyze the performance of aircraft thermal management systems and provide a basis for practical application. Two examples are provided to demonstrate the application of the method to evaluating TMS comprehensively.

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References

  1. Uyanna O, Najafi H. Thermal protection systems for space vehicles: A review on technology development, current challenges and future prospects. Acta Astronaut, 2020, 176: 341–356

    Article  Google Scholar 

  2. Liu S, Zhang B M. Experimental study on a transpiration cooling thermal protection system. Sci China Tech Sci, 2010, 53: 2765–2771

    Article  Google Scholar 

  3. Gvozdich G, Weise P, Von Spakovsky M. Invent: Study of the issues involved in integrating a directed energy weapon subsystem into a high performance aircraft system. In: Proceedings of the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Nashville, 2012

  4. van Heerden A, Judt D, Lawson C, et al. Framework for integrated dynamic thermal simulation of future civil transport aircraft. In: Proceedings of the AIAA Scitech 2020 Forum. San Diego, 2020

  5. Chapman J, Schnulo S, Nitzsche M. Development of a thermal management system for electrified aircraft. In: Proceedings of the AIAA Scitech 2020 Forum. San Diego, 2020

  6. Herber D, Allison J, Buettner R, et al. Architecture generation and performance evaluation of aircraft thermal management systems through graph-based techniques. In: Proceedings of the AIAA Scitech 2020 Forum. San Diego, 2020

  7. Sigthorsson D, Oppenheimer M, Doman D. Aircraft thermal endurance optimization part I: Using a mixed dual tank topology and robust temperature regulation. In: Proceedings of the AIAA Scitech 2019 Forum. San Diego, 2019

  8. Shustrov Y. “Starting mass”—A complex criterion of quality for aircraft on-board systems. Aircraft Design, 1998, 1: 193–203

    Article  Google Scholar 

  9. Aircraft Fuel Weight Penalty Due to Air Conditioning. SAE International, 2011, AIR1168/8A

  10. A R, Pang L, Jiang X, et al. Analysis and comparison of potential power and thermal management systems for high-speed aircraft with an optimization method. Energy Built Environ, 2021, 2: 13–20

    Article  Google Scholar 

  11. Figliola R S, Tipton R, Li H. Exergy approach to decision-based design of integrated aircraft thermal systems. J Aircraft, 2003, 40: 49–55

    Article  Google Scholar 

  12. German B. Tank heating model for aircraft fuel thermal systems with recirculation. J Propul Power, 2012, 28: 204–210

    Article  Google Scholar 

  13. Sigthorsson D, Oppenheimer M, Doman D, et al. Flight endurance enhancing thermal management part ii: Thermal endurance gauge and mission planning. In: Proceedings of the AIAA Scitech 2021 Forum. Nashville, 2021

  14. Huang G, Doman D, Rothenberger M, et al. Dimensional analysis, modeling, and experimental validation of an aircraft fuel thermal management system. J Thermophys Heat Transfer, 2019, 33: 1–11

    Article  Google Scholar 

  15. Solovitz S A, Arik M. System-level metrics for thermal management technology. J Thermal Sci Eng Appl, 2011, 3: 031009

    Article  Google Scholar 

  16. Hoang T, Baldauff R, Cheung K. Evaluation of a magnetically-driven bearingless pump for spacecraft thermal management. In: Proceedings of the 5th International Energy Conversion Engineering Conference and Exhibit (IECEC). St. Louis, 2007

  17. Meng S, Yang Q, Xie W, et al. Structure redesign of the integrated thermal protection system and fuzzy performance evaluation. AIAA J, 2016, 54: 3598–3607

    Article  Google Scholar 

  18. Porter M, Niksiar P, Espinoza Orías A. Multidimensional mechanics: Performance mapping of natural biological systems using permutated radar charts. PloS one, 2018, 13: e0204309

    Article  Google Scholar 

  19. Ma S, Jiang M, Tao P, et al. Temperature effect and thermal impact in lithium-ion batteries: A review. Prog Nat Sci-Mater Int, 2018, 28: 653–666

    Article  Google Scholar 

  20. Dunker C, Bornholdt R, Thielecke F, et al. Architecture and parameter optimization for aircraft electro-hydraulic power generation and distribution systems. SAE Technical Paper, 2015

  21. Deppen T, Hey J, Alleyne A, et al. A model predictive framework for thermal management of aircraft. In: Proceedings of the Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2015

  22. Wu S, Yang H, Han D, et al. Thermal analysis for hydraulic powering system of a certain type aircraft. CSAA/IET International Conference on Aircraft Utility Systems. Guiyang, 2018

  23. Huang Y, Tang Y, Yuan W, et al. Challenges and recent progress in thermal management with heat pipes for lithium-ion power batteries in electric vehicles. Sci China Tech Sci, 2021, 64: 919–956

    Article  Google Scholar 

  24. Dooley M, Lui N, Newman R, et al. Aircraft thermal management-heat sink challenge. SAE Technical Paper, 2014

  25. Morris R, Miller J, Limaye S. Fuel deoxygenation and aircraft thermal management. In: Proceedings of the Collection of Technical Papers—4th International Energy Conversion Engineering Conference. San Diego, 2006

  26. Fischer A. Future fuel heat sink thermal management system technologies. In: Proceedings of the Collection of Technical Papers—4th International Energy Conversion Engineering Conference. San Diego, 2006

  27. Pal D, Severson M. Liquid cooled system for aircraft power electronics cooling. In: Proceedings of the 16th InterSociety Conference on Thermal and Thermomechanical Phenomena in Electronic Systems. Orlando, 2017

  28. Chen W, Wang R, Li X, et al. Study of the heat transfer design of an integrated thermal management system for hypersonic vehicles using supercritical nitrogen as expendable coolant. Aerospace Sci Tech, 2022, 123: 107440

    Article  Google Scholar 

  29. Madruga S. Thermoelectric energy harvesting in aircraft with porous phase change materials. IOP Conf Ser Earth Environ Sci, 2019, 354: 012123

    Article  Google Scholar 

  30. Shi M, Sanders M, Alahmad A, et al. Design and analysis of the thermal management system of a hybrid turboelectric regional jet for the NASA ULI program. In: Proceedings of the AIAA Propulsion and Energy 2020 Forum. 2020. 3572

  31. Mao Y F, Li Y Z, Wang J X, et al. Cooling ability/capacity and exergy penalty analysis of each heat sink of modern supersonic aircraft. Entropy, 2019, 21: 223

    Article  Google Scholar 

  32. van Heerden A S J, Judt D M, Jafari S, et al. Aircraft thermal management: Practices, technology, system architectures, future challenges, and opportunities. Prog Aerospace Sci, 2022, 128: 100767

    Article  Google Scholar 

  33. Ahlers M. Aircraft Thermal Management, Encyclopedia of Aerospace Engineering. Wiley Online Library, 2010

  34. Xu Y, Yan Z, Xia W. A novel system for aircraft cabin heating based on a vapor compression system and heat recovery from engine lubricating oil. Appl Thermal Eng, 2022, 212: 118544

    Article  Google Scholar 

  35. Fernández-Yáñez P, Romero V, Armas O, et al. Thermal management of thermoelectric generators for waste energy recovery. Appl Thermal Eng, 2021, 196: 117291

    Article  Google Scholar 

  36. Seki N, Morioka N, Saito H, et al. A study of air/fuel integrated thermal management system. SAE Technical Paper, 2015. 2015-01-2419

  37. Li D, Dong S, Wang J, et al. State-of-the-art and some considerations on thermal load analysis and thermal management for hydraulic system in MEA. J Eng, 2018, 2018: 399–405

    Article  Google Scholar 

  38. Oppenheimer M, Sigthorsson D, Doman D. Control of fuel thermal management systems with transport delays. In: Proceedings of the AIAA Scitech 2019 Forum. San Diego, 2019

  39. Sigthorsson D, Oppenheimer M, Doman D, et al. Aircraft thermal endurance optimization part II: Using a simple dual tank topology and robust temperature regulation. In: Proceedings of the AIAA Scitech 2019 Forum. San Diego, 2019

  40. Doman D B. Fuel flow topology and control for extending aircraft thermal endurance. J Thermophysics Heat Transfer, 2018, 32: 35–50

    Article  Google Scholar 

  41. Newman R, Dooley M, Lui C. Efficient propulsion, power, and thermal management integration. In: Proceedings of the 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. San Jose, 2013

  42. Yu J, Yu J, Chen F, et al. Numerical study of tip leakage flow control in turbine cascades using the DBD plasma model improved by the parameter identification method. Aerospace Sci Tech, 2019, 84: 856–864

    Article  Google Scholar 

  43. Sanchez F, Huzaifa A M, Liscouët-Hanke S. Ventilation considerations for an enhanced thermal risk prediction in aircraft conceptual design. Aerospace Sci Tech, 2021, 108: 106401

    Article  Google Scholar 

  44. Liscouet-Hanke S, Tfaily A, Esdras G. Parametric 3D modeling for integration of aircraft systems in conceptual design. In: Proceedings of the 62nd CASI Aeronautics Conference and AGM 3rd GARDN Conference. Marquette, 2015

  45. Banerjee S K, Thomas P, Cai X. CATIA V5-based parametric aircraft geometry modeler. SAE Int J Aerosp, 2013, 6: 311–321

    Article  Google Scholar 

  46. Sanchez F, Liscouet-Hanke S, Boutin Y, et al. Multi-level modeling methodology for aircraft thermal architecture design. SAE Technical Papers, 2018

  47. Cheng K, Qin J, Sun H, et al. Performance comparison on wall cooling and heat supply for power generation between fuel- and liquid metal-cooled scramjet. Aerospace Sci Tech, 2019, 93: 105294

    Article  Google Scholar 

  48. Gou J J, Chang Y, Yan Z W, et al. The design of thermal management system for hypersonic launch vehicles based on active cooling networks. Appl Thermal Eng, 2019, 159: 113938

    Article  Google Scholar 

  49. He L, Liu Y, Yang K, et al. The discovery of Q-markers of Qiliqiangxin Capsule, a traditional Chinese medicine prescription in the treatment of chronic heart failure, based on a novel strategy of multidimensional “radar chart” mode evaluation. Phytomedicine, 2021, 82: 153443

    Article  Google Scholar 

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Authors and Affiliations

  1. School of Energy and Power Engineering, Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

    HuiNing Yin, YiMin Xuan, WenLei Lian & TianYi Wang

Authors
  1. HuiNing Yin
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  2. YiMin Xuan
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  3. WenLei Lian
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  4. TianYi Wang
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Corresponding author

Correspondence to YiMin Xuan.

Additional information

This work was supported by the 1912 Project of China (Grant No. 2019-JCJQ-DA-001-108).

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Yin, H., Xuan, Y., Lian, W. et al. A comprehensive set of criteria for evaluating thermal management systems of aerial vehicles. Sci. China Technol. Sci. 66, 2093–2107 (2023). https://doi.org/10.1007/s11431-022-2269-4

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