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Thermodynamic analysis of a novel precooled supersonic turbine engine based on aircraft/engine integrated optimal design

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  • Cai, Changpeng
  • Chen, Haoying
  • Fang, Juan
  • Zheng, Qiangang
  • Chen, Cheng
  • Zhang, Haibo

Abstract

Aircraft and precooled engine efficient matching work is a key issue in the thermal cycle design of precooled engines, to solve this problem, an aircraft/precooled turbine engine integrated design method considering the fuel precooling impact mechanism is newly proposed. The impact of n-decane, ammonia, and hydrogen fuel precooling on aircraft design parameters and engine thrust requirements is revealed. Furthermore, a parameter optimal design method for fuel precooled engine is carried out to satisfy the multi-objective performance requirements of high specific thrust, low fuel consumption, high exergy efficiency, and low weight. The simulation results show that the n-decane fuel precooled engine reduces the takeoff weight of the aircraft by 4.23% and the fuel load by 11.6%, which has a better comprehensive performance than that of ammonia and hydrogen. Ammonia fuel has the maximum precooling heat sink and performance improvement space. After multi-objective optimization, it increases the maximum specific thrust by 7.3%, reduces fuel consumption by 2.2%, and improves the engine exergy efficiency by 2.7%, with only a 1.3% increase in rotating component weight. Ammonia and n-decane dual fuel precooling can achieve complementary advantages of high combustion heat value and high precooling heat sink, making it an ideal precooled engine scheme.

Suggested Citation

  • Cai, Changpeng & Chen, Haoying & Fang, Juan & Zheng, Qiangang & Chen, Cheng & Zhang, Haibo, 2023. "Thermodynamic analysis of a novel precooled supersonic turbine engine based on aircraft/engine integrated optimal design," Energy, Elsevier, vol. 280(C).
    • Handle: RePEc:eee:energy:v:280:y:2023:i:c:s0360544223015554
    DOI: 10.1016/j.energy.2023.128161
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    References listed on IDEAS

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    Cited by:

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    2. Wen, Jie & Wan, Chenxi & Xu, Guoqiang & Zhuang, Laihe & Dong, Bensi & Chen, Junjie, 2024. "Optimization of thermal management system architecture in hydrogen engine employing improved genetic algorithm," Energy, Elsevier, vol. 297(C).
    3. Lv, Chengkun & Huang, Qian & Wang, Ziao & Chang, Juntao & Yu, Daren, 2024. "Mode transition control law analysis of ammonia MIPCC aeroengine considering inlet–compressor safety matching," Energy, Elsevier, vol. 288(C).
    4. Huang, W.S. & Ning, H.Y. & Tang, G.H., 2025. "Investigation of high-compactness and high-efficiency TPMS precoolers for precooled aero-engine," Energy, Elsevier, vol. 319(C).
    5. Cai, Changpeng & Zheng, Qiangang & Wang, Yong & Chen, Haoying & Zhang, Haibo, 2024. "Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model," Energy, Elsevier, vol. 302(C).
    6. Zhang, Kai & Yu, Xuanfei & Zhang, Duo & Guo, Jian & Qin, Fei, 2025. "Evaluation of multi-mode shared combustor with different flame holder designs for an innovative turbo-ramjet combined cycle engine," Energy, Elsevier, vol. 323(C).
    7. Luo, Qiaodan & Zhao, Shengfeng & Zhou, Shiji & Yao, Lipan & Yang, Chengwu & Lu, Xingen & Zhu, Junqiang, 2024. "Influence of diversified dihedral stator on the thermodynamic performance and flow loss characteristics of a variable core driven fan stage," Energy, Elsevier, vol. 294(C).

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