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Performance analysis of a thermal management system based on hydrocarbon-fuel regenerative cooling technology for scramjets

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  • Dang, Chaolei
  • Cheng, Kunlin
  • Xu, Jing
  • Fan, Junhao
  • Qin, Jiang
  • Liu, Guodong

Abstract

Thermal protection and power generation are two of the major technical challenges in developing hypersonic vehicles with long-range/endurance. This research is aimed to provide a system for thermal protection and power generation for hydrocarbon-fueled scramjets. This study proposed a thermal management system based on fuel vapor turbine (FVT) and closed-Brayton-cycle (CBC) to generate power, and a bypass loop is connected with CBC in parallel to ensure thermal protection demand. A performance analysis model considering the combustor and cooling channels is established. The combustion and heat transfer process are described in a quasi-one-dimensional way, while FVT and CBC are described in a zero-dimensional form. Results indicate that large CBC power generation efficiency (ηPG,CBC) and FVT expansion ratio (πFVT) can improve power generation with the same thermal protection performance. Because of the integrated variation law of cooling heat exchange and ηPG,CBC, there exists an optimal value of fuel outlet temperature (Tf3) while meeting the thermal protection requirement. The high Mach number and low equivalence ratio both require a significant increase in the cooling capability of fuel, and it is feasible to sacrifice the power generation of the CBC subsystem to meet the thermal protection demand.

Suggested Citation

  • Dang, Chaolei & Cheng, Kunlin & Xu, Jing & Fan, Junhao & Qin, Jiang & Liu, Guodong, 2023. "Performance analysis of a thermal management system based on hydrocarbon-fuel regenerative cooling technology for scramjets," Energy, Elsevier, vol. 285(C).
    • Handle: RePEc:eee:energy:v:285:y:2023:i:c:s036054422302114x
    DOI: 10.1016/j.energy.2023.128720
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    References listed on IDEAS

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    1. Chen, Wei-Hsin & Chiou, Yi-Bin, 2020. "Geometry design for maximizing output power of segmented skutterudite thermoelectric generator by evolutionary computation," Applied Energy, Elsevier, vol. 274(C).
    2. Zhang, Duo & Qin, Jiang & Feng, Yu & Ren, Fengzhi & Bao, Wen, 2014. "Performance evaluation of power generation system with fuel vapor turbine onboard hydrocarbon fueled scramjets," Energy, Elsevier, vol. 77(C), pages 732-741.
    3. Cheng, Kunlin & Qin, Jiang & Zhang, Duo & Bao, Wen & Jing, Wuxing, 2022. "Performance evaluation for a combined power generation system of closed-Brayton-cycle and thermoelectric generator with finite cold source at room temperature on hypersonic vehicles," Energy, Elsevier, vol. 254(PC).
    4. Xu, Qing & Li, Haowei & Feng, Yaoxun & Li, Xiaoning & Ling, Changming & Zhou, Chaoying & Qin, Jiang, 2020. "Dynamic thermo-physical characteristics of high temperature gaseous hydrocarbon fuel thermal power generation for regeneratively cooled hypersonic propulsion system," Energy, Elsevier, vol. 211(C).
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    6. Dang, Chaolei & Cheng, Kunlin & Fan, Junhao & Wang, Yilin & Qin, Jiang & Liu, Guodong, 2023. "Performance analysis of fuel vapor turbine and closed-Brayton-cycle combined power generation system for hypersonic vehicles," Energy, Elsevier, vol. 266(C).
    7. Cheng, Kunlin & Xu, Jing & Dang, Chaolei & Qin, Jiang & Jing, Wuxing, 2022. "Performance evaluation of fuel indirect cooling based thermal management system using liquid metal for hydrocarbon-fueled scramjet," Energy, Elsevier, vol. 260(C).
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    Cited by:

    1. Dang, Chaolei & Xu, Jing & Chen, Zhichao & Cheng, Kunlin & Qin, Jiang & Liu, Guodong, 2024. "Comparative study of different layouts in the closed-Brayton-cycle-based segmented cooling thermal management system for scramjets," Energy, Elsevier, vol. 301(C).

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