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Performance evaluation of multicombustor engine for Mach3+-Level propulsion system

Author

Listed:
  • Deng, Li
  • Chen, Min
  • Tang, Hailong
  • Zhang, Jiyuan

Abstract

Turbine-based combined cycles are widely considered as a propulsion system for hypersonic vehicles. The inadequate performance of turbine-based engines has resulted in thrust traps, thereby limiting the development of turbine-based combined cycles. To satisfy the performance requirements over a wide speed range, a novel Mach 3+-level multicombustor engine is proposed, and its performance potential is investigated, where an intermediate bypass burner reheats the core airflow to generate more cycle work and the second bypass duct heated by a bypass afterburner provides the main source of the engine thrust at high Mach numbers. Results show that the multicombustor engine extends the flight envelope from Mach 2.5 to 3.5 and increases the thrust by 32% compared with the conventional engine. The application of an intermediate bypass burner reduces the turbine pressure ratio by 43%, thereby reducing the number of turbine stages. The concept of a multicombustor engine is promising for designing the power systems of hypersonic vehicles.

Suggested Citation

  • Deng, Li & Chen, Min & Tang, Hailong & Zhang, Jiyuan, 2024. "Performance evaluation of multicombustor engine for Mach3+-Level propulsion system," Energy, Elsevier, vol. 295(C).
    • Handle: RePEc:eee:energy:v:295:y:2024:i:c:s0360544224007643
    DOI: 10.1016/j.energy.2024.130992
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    References listed on IDEAS

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    1. Zhang, Jiyuan & Tang, Hailong & Chen, Min, 2019. "Linear substitute model-based uncertainty analysis of complicated non-linear energy system performance (case study of an adaptive cycle engine)," Applied Energy, Elsevier, vol. 249(C), pages 87-108.
    2. Lv, Chengkun & Xu, Haiqi & Chang, Juntao & Wang, Youyin & Chen, Ruoyu & Yu, Daren, 2022. "Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor," Energy, Elsevier, vol. 261(PB).
    3. Chen, Xu, 2020. "Novel dual-population adaptive differential evolution algorithm for large-scale multi-fuel economic dispatch with valve-point effects," Energy, Elsevier, vol. 203(C).
    4. Ji, Zhixing & Qin, Jiang & Cheng, Kunlin & Liu, He & Zhang, Silong & Dong, Peng, 2019. "Performance evaluation of a turbojet engine integrated with interstage turbine burner and solid oxide fuel cell," Energy, Elsevier, vol. 168(C), pages 702-711.
    5. Zhao, Wei & Huang, Chen & Zhao, Qingjun & Ma, Yingqun & Xu, Jianzhong, 2018. "Performance analysis of a pre-cooled and fuel-rich pre-burned mixed-flow turbofan cycle for high speed vehicles," Energy, Elsevier, vol. 154(C), pages 96-109.
    6. Sun, Hongchuang & Qin, Jiang & Li, Haowei & Huang, Hongyan & Yan, Peigang, 2019. "Research of a combined power and cooling system based on fuel rotating cooling air turbine and organic Rankine cycle on hypersonic aircraft," Energy, Elsevier, vol. 189(C).
    7. Dong, Pengcheng & Tang, Hailong & Chen, Min & Zou, Zhengping, 2018. "Overall performance design of paralleled heat release and compression system for hypersonic aeroengine," Applied Energy, Elsevier, vol. 220(C), pages 36-46.
    8. Li, Hui & Zou, Zhengping & Chen, Yiming & Du, Pengcheng & Fu, Chao & Wang, Yifan, 2023. "Experimental insights into thermal performance of a microtube precooler with drastic coolant properties variation and precooling impacts on turbojet engine operation," Energy, Elsevier, vol. 278(PA).
    9. Li, Shuijia & Gong, Wenyin & Hu, Chengyu & Yan, Xuesong & Wang, Ling & Gu, Qiong, 2021. "Adaptive constraint differential evolution for optimal power flow," Energy, Elsevier, vol. 235(C).
    10. Wang, Cong & Yu, Xuanfei & Ha, Chan & Liu, Zekuan & Fang, Jiwei & Qin, Jiang & Shao, Jiahui & Huang, Hongyan, 2023. "Thermodynamic analysis for a novel chemical precooling turbojet engine based on a multi-stage precooling-compression cycle," Energy, Elsevier, vol. 262(PA).
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