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Investigation on the Performance Characteristics of 2-Stroke Heavy Fuel Light Aeroengine (2SHFLA) with Different Fuel Injection Systems: Modeling and Comparative Simulation

Author

Listed:
  • Yuan Qiao

    (State Key Laboratory of Automotive Safety and Energy, School of Vehicle and Mobility, Tsinghua University, Beijing 100084, China)

  • Li Lin

    (State Key Laboratory of Automotive Safety and Energy, School of Vehicle and Mobility, Tsinghua University, Beijing 100084, China)

  • Wei Zhong

    (State Key Laboratory of Automotive Safety and Energy, School of Vehicle and Mobility, Tsinghua University, Beijing 100084, China)

  • Kaisheng Huang

    (State Key Laboratory of Automotive Safety and Energy, School of Vehicle and Mobility, Tsinghua University, Beijing 100084, China
    The Joint Laboratory for Internet of Vehicles, Ministry of Education-China Mobile Communications Corporation, Beijing 100084, China
    Collaborative Innovation Center of Electric Vehicles in Beijing, Beijing 100081, China)

Abstract

Extensive application of small and medium-sized unmanned aerial vehicles (UAVs) have already made the development of corresponding power system a research hotspot nowadays. Two-stroke heavy fuel light aeroengine (2SHFLA) is selected as the research focus in this paper. The working principle of 2SHFLA with different fuel injection systems is elaborated systematically. By dividing the initial prototype engine into several subsystems, the simulation platform is set up with its key model parameters accurately calibrated against the test data. Simulation platforms of the other two types of engines are subsequently constructed based on the pre-calibrated simulation platform of the initial prototype engine. Afterwards, comparative simulation is performed and the corresponding simulation results include: (1) comparison of performance characteristics of the initial prototype engine fueled with regular gasoline/heavy fuel; (2) comprehensive comparison of the performance characteristics of all the three types of engine.

Suggested Citation

  • Yuan Qiao & Li Lin & Wei Zhong & Kaisheng Huang, 2020. "Investigation on the Performance Characteristics of 2-Stroke Heavy Fuel Light Aeroengine (2SHFLA) with Different Fuel Injection Systems: Modeling and Comparative Simulation," Energies, MDPI, vol. 13(19), pages 1-39, October.
    • Handle: RePEc:gam:jeners:v:13:y:2020:i:19:p:5136-:d:423001
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    References listed on IDEAS

    as
    1. Sousa, Jorge & Paniagua, Guillermo & Collado Morata, Elena, 2017. "Thermodynamic analysis of a gas turbine engine with a rotating detonation combustor," Applied Energy, Elsevier, vol. 195(C), pages 247-256.
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    3. Fu-Kang Ma & Jun Wang & Yao-Nan Feng & Yan-Gang Zhang & Tie-Xiong Su & Yi Zhang & Yu-Hang Liu, 2017. "Parameter Optimization on the Uniflow Scavenging System of an OP2S-GDI Engine Based on Indicated Mean Effective Pressure (IMEP)," Energies, MDPI, vol. 10(3), pages 1-20, March.
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