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Performance analysis of hybrid electric and distributed propulsion system applied on a light aircraft

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  • Bravo, Guillem Moreno
  • Praliyev, Nurgeldy
  • Veress, Árpád

Abstract

Aircraft industry is still in the early stages of pure electric propulsion systems development, the main concern is the significant mass of batteries. As such, hybrid electric systems have gained much stakeholder attention in the recent years. At the same time, interest in distributed propulsion systems is also increasing, due to the improvement in aerodynamic efficiency compared to conventional configurations. This paper investigates these two fields, presenting the results of two correlated studies. The first study deals with:

Suggested Citation

  • Bravo, Guillem Moreno & Praliyev, Nurgeldy & Veress, Árpád, 2021. "Performance analysis of hybrid electric and distributed propulsion system applied on a light aircraft," Energy, Elsevier, vol. 214(C).
    • Handle: RePEc:eee:energy:v:214:y:2021:i:c:s0360544220319307
    DOI: 10.1016/j.energy.2020.118823
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    References listed on IDEAS

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    3. Sliwinski, Jacob & Gardi, Alessandro & Marino, Matthew & Sabatini, Roberto, 2017. "Hybrid-electric propulsion integration in unmanned aircraft," Energy, Elsevier, vol. 140(P2), pages 1407-1416.
    4. Yilmaz, Nadir & Atmanli, Alpaslan, 2017. "Sustainable alternative fuels in aviation," Energy, Elsevier, vol. 140(P2), pages 1378-1386.
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    Cited by:

    1. Wang, Mingkai & Xiaoyang, Guotai & He, Ruichen & Zhang, Shuguang & Ma, Jintao, 2023. "Bi-layer sizing and design optimization method of propulsion system for electric vertical takeoff and landing aircraft," Energy, Elsevier, vol. 283(C).
    2. Hashemi, Seyed Reza & Mahajan, Ajay Mohan & Farhad, Siamak, 2021. "Online estimation of battery model parameters and state of health in electric and hybrid aircraft application," Energy, Elsevier, vol. 229(C).

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