Regional passenger aircraft type of An-158 with a hybrid propulsion parametric concept

• Autorzy: Loginov, Vasyl , Ukrainets, Yevgen , Kravchenko, Igor , Yelans’ky, Olexandr , Fil, Serhii , Pushylin, Oleksii
• Języki publikacji: EN

Abstrakty

EN

This study proposes a concept for the design and development of a modification of the An-158 regional passenger aircraft equipped with a hybrid propulsion system. The propulsion configuration includes two turboprop engines and two electric engines, with multidirectional propellers positioned symmetrically at the wing tips. This innovative design reduces wingtip vortices, decreasing inductive drag and improving aerodynamic efficiency. Parametric analyses were conducted using the modular software systems “Integration 2.1” and “Propeller 2.2” for typical flight profiles of the An-158. Despite the added weight from hybrid components, the modified aircraft design demonstrated reduced fuel consumption and harmful emissions in taxiing, takeoff, and climb modes. These findings highlight the potential of hybrid propulsion to enhance environmental performance while maintaining operational efficiency.

Słowa kluczowe

EN

aircraft; regional aircraft; turboprop engine; harmful emissions; propeller; hybrid propulsion

• Czasopismo: Transactions on Aerospace Research
• Rocznik: 2024
• Tom: Nr 4 (277)
• Strony: 14--26
• Opis fizyczny: Bibliogr. 27 poz., rys., tab.

Twórcy

autor

Loginov, Vasyl

• Department of Programs and Projects FED JSC, 132 Sumska Str., Kharkiv, Ukraine, 61023,

autor

Ukrainets, Yevgen

• Department of the Design and Strength of Aircraft and Engines, Kharkov National Air Force University named after Ivan Kozhedub, 77/79 Sumska Str., Kharkiv, Ukraine, 61023

autor

Kravchenko, Igor

• SE “Ivchenko-Progress”, 2 Ivanova St., Zaporozhye, Ukraine, 69068

autor

Yelans’ky, Olexandr

• SE “Ivchenko-Progress”, 2 Ivanova St., Zaporozhye, Ukraine, 69068

autor

Fil, Serhii

• SE “Antonov”, 1 Tupolev Str., Kyiv, Ukraine, 03062

autor

Pushylin, Oleksii

• SE “Ivchenko-Progress”, 2 Ivanova St., Zaporozhye, Ukraine, 69068

Bibliografia

• [1] Airbus i Siemens budut sozdavat’ elektricheskie i gibridnye aviacionnye dvigateli [Airbus and Siemens to create electric and hybrid aviation engines]. Habr. 2020. Available from: https://habr.com/ru/post/392869/. [in Russian].
• [2] 5 sovremennyh tendencij v aerokosmicheskoj otrasli [5 modern trends in the aerospace industry]. Soften. 2020. Available from: https://www.soften.com.ua/blogs/ansys/5-sovremennykh-tendentsij-v-aerokosmicheskoj-otrasli.html. [in Russian].
• [3] Anipko OB, Loginov VV. Analiz rabochego processa v oblasti sreza vyhodnogo ustrojstva dvigatelya, raspolozhennogo pod krylom samoleta [Analysis of the working process in the exhaust area of an engine located under the wing of an aircraft]. Integrirovannye tekhnologii i energosberezhenie. 2008;2:37-50. [in Russian].
• [4] Anipko OB, Bashinskij VG, Loginov VV, Semenov VB. Integraciya silovoj ustanovki i planera transportnogo samoleta [Integration of powerplant and airframe of a transport aircraft]. Zaporozh’e: AO “Motor Sich”; 2013. 329 p. [in Russian].
• [5] Orders and deliveries - Commercial Aircraft. Airbus. 2021. Available from: https://www.airbus.com/en/products-services/commercial-aircraft/market/orders-and-deliveries.
• [6] Commercial Market Outlook 2021-2040. Boeing. 2021. Available from: https://www.boeing.com/commercial/market/commercial-market-outlook/#/interactive-forecast.
• [7] Boeing and Embraer serious about new conventional aircraft soon. Aviation Week. 2021. Available from: https://aviationweek.com/aerospace/boeing-embraer-serious-about-new-conventional-aircraft-soon.
• [8] Why Embraer decided to invest in a new turboprop aircraft. Simple Flying. 2021. Available from: https://simpleflying.com/why-embraer-decided-to-invest-in-a-new-turboprop-aircraft/.
• [9] Embraer unveils new turboprop aircraft design. Aeronautics Online. 2021. Available from: https://aeronauticsonline.com/embraer-unveils-new-turboprop-aircraft-design/.
• [10] Gladin J, Perullo C, Tai J, Mavris D. A parametric study of hybrid electric gas turbine propulsion as a function of aircraft size class and technology level. Proc AIAA. 2017. DOI:10.2514/6.2017-0338.
• [11] Perullo C, Mavris D. A review of hybrid-electric energy management and its inclusion in vehicle sizing. Aircraft Eng Aerosp Technol. 2014;86:550-7. DOI:10.1108/AEAT-04-2014-0041.
• [12] Ang AWX, Gangoli Rao A, Kanakis T, Lammen W. Performance and analysis of an electrically assisted propulsion system for short-range civil aircraft. Proc Inst Mech Eng G J Aerosp Eng. 2019;233(4):1490-502. DOI:10.1177/0954410017754146.
• [13] Brdnik A. Market and technological perspectives for the new generation of regional passenger aircraft. Energies. 2019;12:1864. DOI:10.3390/en12101864.
• [14] Palkin VA. Obzor rabot v SSHA i Evrope po aviacionnym dvigatelyam dlya samoletov grazhdanskoj aviacii 2020-2040-h godov [Review of work in the USA and Europe on aircraft engines for civil aviation of the 2020-2040s]. Aviacionnye dvigateli. 2019;3(4):63-83. [in Russian].
• [15] Areas of innovation. Safran Group. 2021. Available from: https://www.safran-group.com/group/innovation/areas-innovation.
• [16] Makarenko N. Gibridnyj dvigatel’ dlya samoleta: proryv ili otlozhennoe reshenie [Hybrid engine for an aircraft: breakthrough or deferred solution]. Nauka i Tekhnika. 2020. Available from: https://naukatehnika.com/gibridnyj-dvigatel-dlya-samoleta.html. [in Russian].
• [17] Hoelzen J, Liu Y, Bensmann B, Winnefeld C, Elham A, Friedrichs J, et al. Conceptual design of operation strategies for hybrid electric aircraft. Energies. 2018;11(1):217. DOI:10.3390/en11010217.
• [18] Strack M, Chiozzotto GP, Iwanizki M, Plohr M, Kuhn M. Conceptual design assessment of advanced hybrid electric turboprop aircraft configurations. In: Proceedings of the 17th AIAA Aviation Technology, Integration, and Operations Conference; 2017; Denver, CO, USA. p. 1-20.
• [19] Kim HD, Perry AT, Ansell PJ. A review of distributed electric propulsion concepts for air vehicle technology. Proc AIAA/IEEE Electric Aircraft Technol Symp. 2018; Cincinnati, OH, USA. p. 77-97.
• [20] Jansen RH, Bowman C, Jankovsky A. Overview of NASA electrified aircraft propulsion research for large subsonic transports. AIAA Tech Conf. 2017. DOI:10.2514/6.2017-0338.
• [21] Brelje BJ, Martins JR. Electric, hybrid, and turboelectric fixed-wing aircraft: a review of concepts, models, and design approaches. Prog Aerosp Sci. 2018. DOI:10.1016/j.paerosci.2018.06.004.
• [22] Biser S, Wortmann G, Ruppert S. Predesign considerations for the DC link voltage DOI:10.3390/aerospace6120126.
• [23] Hyun KD, Perry AT, Phillip AJ. A review of distributed electric propulsion concepts for air vehicle technology [A review of distributed electric propulsion concepts for air vehicle technology]. Proc AIAA/IEEE Electric Aircraft Technol Symp. 2018; Cincinnati, OH, USA. DOI:10.2514/6.2018-4998.
• [24] Wiart L, Atinault O, Paluch B, Hue D, Grenon R. Development of NOVA aircraft configurations for large engine integration studies. Proc 33rd AIAA Appl Aerodyn Conf. 2015;Dallas, TX, USA. DOI:10.2514/6.2015-2254.
• [25] Uranga A, Drela M, Greitzer EM. Boundary layer ingestion benefit of the D8 transport aircraft. AIAA J. 2017; 55(11). DOI:10.2514/1.J055755.
• [26] Shmyrov V, Loginov V, Fil S, Khaustov A, Bondarchuk O, Kalashnikov A, et al. The modernization concept of aircraft An-26 and An-140 based on the use of a hybrid power system. EEJET. 2020;5(1):6-17. DOI:10.15587/1729-4061.2020.212150.
• [27] van Holsteijn MR, Gangoli Rao A, Yin F. Operating characteristics of an electrically assisted turbofan engine. Proc ASME Turbo Expo. 2020; GT2020-15355: V001T01A028. DOI:10.1115/GT2020-15355

Identyfikatory

DOI

10.2478/tar-2024-0020