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Matching and performance analysis of a solid oxide fuel cell turbine-less hybrid electric propulsion system on aircraft

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Listed:
  • Guo, Fafu
  • Li, Chengjie
  • Liu, He
  • Cheng, Kunlin
  • Qin, Jiang

Abstract

Advanced low-carbon propulsion technology is one of the major initiatives to address aviation environmental challenges. In this paper, a solid oxide fuel cell turbine-less hybrid electric propulsion system is developed. It is a new engine, in which the power consumed by the compressor comes from a fuel cell, not a turbine. The aircraft's propulsion comes from the high-velocity exhaust discharged from the nozzles. To make the key fuel cell work properly and determine the system operating parameters, it is necessary to study the matching and performance of the hybrid electric propulsion system. In this study, a performance analysis model of the hybrid electric propulsion system is established. In particular, a one-dimensional fuel cell is simulated to obtain its localized thermal gradient. The results show that the hybrid electric propulsion system has a satisfactory performance under the design conditions. It is superior to the gas turbine-based engine in performance, and they have different performance trends. The operating range of compressor pressure ratio is determined. The sensitivity analysis shows that in addition to compressor pressure ratio, Mach number, reforming temperature, and fuel utilization have a great influence on the performance, which is worthy of further study.

Suggested Citation

  • Guo, Fafu & Li, Chengjie & Liu, He & Cheng, Kunlin & Qin, Jiang, 2023. "Matching and performance analysis of a solid oxide fuel cell turbine-less hybrid electric propulsion system on aircraft," Energy, Elsevier, vol. 263(PA).
    • Handle: RePEc:eee:energy:v:263:y:2023:i:pa:s0360544222025415
    DOI: 10.1016/j.energy.2022.125655
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    References listed on IDEAS

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    1. Chen, Hao & Yang, Chen & Zhou, Nana & Farida Harun, Nor & Oryshchyn, Danylo & Tucker, David, 2020. "High efficiencies with low fuel utilization and thermally integrated fuel reforming in a hybrid solid oxide fuel cell gas turbine system," Applied Energy, Elsevier, vol. 272(C).
    2. Ji, Zhixing & Qin, Jiang & Cheng, Kunlin & Guo, Fafu & Zhang, Silong & Dong, Peng, 2019. "Thermodynamics analysis of a turbojet engine integrated with a fuel cell and steam injection for high-speed flight," Energy, Elsevier, vol. 185(C), pages 190-201.
    3. Ribeirinha, P. & Abdollahzadeh, M. & Boaventura, M. & Mendes, A., 2017. "H2 production with low carbon content via MSR in packed bed membrane reactors for high-temperature polymeric electrolyte membrane fuel cell," Applied Energy, Elsevier, vol. 188(C), pages 409-419.
    4. Ji, Zhixing & Qin, Jiang & Cheng, Kunlin & Guo, Fafu & Zhang, Silong & Zhou, Chaoying & Dong, Peng, 2020. "Determination of the safe operation zone for a turbine-less and solid oxide fuel cell hybrid electric jet engine on unmanned aerial vehicles," Energy, Elsevier, vol. 202(C).
    5. Collins, Jeffrey M. & McLarty, Dustin, 2020. "All-electric commercial aviation with solid oxide fuel cell-gas turbine-battery hybrids," Applied Energy, Elsevier, vol. 265(C).
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