In this paper, two hybrid-electric propulsion system configurations are presented as an example of hybrid-electric propulsion systems to decrease fuel consumption, greenhouse gas emissions, and flight costs. Today, most academic papers about electrified propulsion are theoretical, therefore conceptual applications with commercially available technologies have been implemented on the Cessna 172S, which is a very common aircraft, to understand the current state of electrification. In 2 h conceptual flight, 14.8% reduction in fuel consumption and flight greenhouse gas emissions; and nearly 14% cost reduction were achieved with battery hybrid-electric and fuel cell hybrid-electric propulsion system configurations.


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    Titel :

    Conceptual Application of Hybrid-Electric Propulsion System Configurations on Cessna 172S


    Weitere Titelangaben:

    Sustainable aviat.


    Beteiligte:
    Karakoc, T. Hikmet (Herausgeber:in) / Usanmaz, Öznur (Herausgeber:in) / Rajamani, Ravi (Herausgeber:in) / Oktal, Hakan (Herausgeber:in) / Dalkiran, Alper (Herausgeber:in) / Ercan, Ali Haydar (Herausgeber:in) / Akgul, Burak (Autor:in) / Ata, Ismail (Autor:in)

    Kongress:

    International Symposium on Electric Aircraft and Autonomous Systems ; 2021 December 16, 2021 - December 18, 2021


    Erschienen in:

    Advances in Electric Aviation ; Kapitel : 29 ; 221-228


    Erscheinungsdatum :

    22.08.2023


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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