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Warianty tytułu
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Abstrakty
This study examines key indicators and criteria for assessing the efficiency of hybrid turbo-electric propulsion system (HTEPS) configurations for passenger aircraft. A comprehensive review of scientific and technical literature was conducted to identify the most relevant efficiency metrics for HTEPS, with a focus on hybrid-electric propulsion and fuel cell integration. The Evektor EV-55 Outback light multipurpose aircraft, known for its short takeoff and landing capabilities, was selected as a reference model. The study highlights the advantages of all-electric propulsion for a nine-seater aircraft, discussing the impact of hybridization on fuel efficiency, performance, and cost-effectiveness. Two hybridization architectures-sequential and parallel-are evaluated, with the sequential architecture deemed more suitable for small aircraft due to its simplicity and feasibility. The findings confirm that utilizing an engine with lower rated power, in combination with a hybrid-electric system, is a more efficient and cost-effective approach compared to conventional higher-powered engines. The paper concludes with recommendations for optimizing HTEPS configurations and future research directions in hybrid-electric aviation.
Czasopismo
Rocznik
Tom
Strony
85--97
Opis fizyczny
Bibliogr. 28 poz., fot., rys., wzory
Twórcy
autor
- SE Ivchenko-Progress, 2, Ivanova St., Zaporozhzhia, 69068 Ukraine
autor
- JSC FED, 132, Sumska St., Kharkiv, 61023 Ukraine
Bibliografia
- [1] Moore MD, Fredericks B. Misconceptions of electric propulsion aircraft and their emergent aviation markets. In: AIAA SciTech. 2014. doi:10.2514/6.2014-0535.
- [2] Pornet C. Hybrid and universally-electric aircraft concepts. AccessScience, McGraw-Hill Yearbook of Sciences and Technology. McGraw-Hill Education; 2014. doi:10.1036/1097-8542.YB150553.
- [3] MIT Electric Vehicle Team. A guide to understanding battery specifications. December 2008. Available from: https://web.mit.edu/evt/summary_battery_specifications.pdf [Accessed 15 Jan 2020].
- [4] National Academies of Engineering (NAE). Commercial aircraft propulsion and energy systems research: reducing global carbon emissions. Washington, DC: The National Academies Press; 2016. Available from: https://www.nap.edu/catalog/23490/commercial-aircraft-propulsion-and-energy-systems-research-reducing-global-carbon. ISBN: 978-0-309-44096-7 [Accessed 15 Oct 2019].
- [5] Bradley MK, Droney CK. Subsonic ultra green aircraft research: Phase 2. Volume 2; hybrid electric design exploration. Hampton, VA: NASA Langley Research Center; 2015.
- [6] Stoia T, Balan C, Atreya S, O’Neil P. Solid oxide fuel cell-steam reformation power system configuration options for an all-electric commuter airplane flight demonstrator. In: Proceedings of the 2018 Aviation Technology, Integration, and Operations Conference; 2018 June 25-29; Atlanta, GA. p. 3358.
- [7] Papathakis KV, Schnarr OC, Lavelle TM, Borer NK, Stoia T, Atreya S. Integration concept for a hybrid-electric solid-oxide fuel cell power system into the X-57 Maxwell. In: Proceedings of the 2018 Aviation Technology, Integration, and Operations Conference; 2018 June 25-29; Atlanta, GA. p. 3359.
- [8] Van Wensveen J, Peter F, Rau T, Hornung M. Assessment of a fuel cell-powered full-electric subsystem architecture for the Avacon research baseline aircraft. In: Proceedings of the German Aerospace Congress 2019; 2019 Sept 30-Oct 2; Darmstadt, Germany.
- [9] Vision. Available from: https://www.h2fly.de/vision [Accessed 20 Apr 2023].
- [10] H2FLY. Available from: https://www.h2fly.de/_files/ugd/f0c744_ce6466330eb842588d1b6892aa28e855.pdf [Accessed 20 Apr 2023].
- [11] Pornet C, Gologan PC, Vratny A, Seitz O, Schmitz AT, Isikveren M, et al. Methodology for sizing and performance assessment of hybrid energy aircraft. J Aircraft. 2015;52(1):341-52. doi:10.2514/1.C032716.
- [12] Pornet C. Conceptual design methods for sizing and performance of hybrid-electric transport aircraft. 2018. 122 p. doi:10.106/j.paerosci.2015.09.002.
- [13] Pornet C, Gologan C, Vratny PC. Methodology for sizing and performance assessment of hybrid energy aircraft. 2013. AIAA 2013-4415. Session: Powerplant Performance. doi:10.2514/6.2013-4415.
- [14] Gibson AR, Hall DW, Waters M, Masson P, Schiltgen BT, Foster T, et al. The potential and challenge of turboelectric propulsion for subsonic transport aircraft. 2010. doi:10.2514/6.2010-276.
- [15] Hepperle M. Electric flight - potential and limitations. STO-MP-AVT-209; 2012.
- [16] Scholz AE, Michelmann J, Hornung M. Fuel cell hybrid-electric aircraft: design, operational, and environmental impact. AIAA 2022-2333. Session: Hydrogen and Geoengineering; 2021. doi:10.2514/6.2022-2333.
- [17] Töpler J, Lehmann J. Hydrogen and fuel cell: technologies and market perspectives. Berlin: Springer; 2014. 286 p. ISBN: 978-3-662-44971-4. doi:10.1007/978-3-662-44972-1.
- [18] Sohel AA, Talukder MAS, Mamun MAH. Constant pitch propeller design for low subsonic airplane. Global J Res Eng A Mech Mech Eng. 2014;14(6).
- [19] Veldhuis LLM. Review of propeller-wing aerodynamic interference. In: Proceedings of the 24th International Congress of the Aeronautical Sciences (ICAS 2004); 2004. p. 1-21.
- [20] Morgado J, Silvestre M, Pascoa JC. Validation of new formulations for propeller analysis. J Propul Power. 2015;31(1):467-77.
- [21] Tremmel M, Taulbee DB, Sonnenmeier JR. Numerical determination of circulation for a swept propeller. J Aircraft. 2001;38(6):1085-92.
- [22] Worobel R. Computer program user’s manual for advanced general aviation propeller study. NASA Contractor Report 2066. 1972. 78 p.
- [23] Zhang Y, Haixin C, Yufei Z. Numerical research of a propeller plane based on actuator disc model. In: Proceedings of the 7th European Conference for Aeronautics and Space Sciences (EUCASS); 2017. doi:10.13009/EUCASS2017-194.
- [24] Evektor. EV-55 Outback. Available from: https://www.evektor.cz/aircraft-technical-specification/ev-55-outback [Accessed 02 Apr 2023].
- [25] Aircraft review: Evektor EV-55 Outback by Auctusdelineations. Available from: https://xplanereviews.com/index.php?/forums/topic/648-aircraft-review-evektor-ev-55-outback-by-auctusdelineations/ [Accessed 02 Apr 2023].
- [26] E15.cz. Available from: https://www.e15.cz/galerie/byznys/prumysl-a-energetika/240489/vyrobce-letadel-evektor-klesa-k-zemi-kvuli-vyvoji-noveho-stroje-tone-v-hluboke-ztrate?foto=0.
- [27] Pornet C, Isikveren AT. Conceptual design of hybrid-electric transport aircraft. Elsevier. Germany; 2015.
- [28] Isikveren AT, Kaiser S, Pornet C, Vratny PC. Pre-design strategies and sizing techniques for dual-energy aircraft. Aircr Eng Aerosp Technol J. 2014;86(6):525-42.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b2d264a7-e4c2-4b87-8ed8-6b234f460a97
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