Exploration and Sizing of a Large Passenger Aircraft with Distributed Ducted Electric Fans
| Autor: | Emmanuel Benard, Alessandro Sgueglia, Nathalie Bartoli, Joseph Morlier, Olivier Atinault, Peter Schmollgruber |
|---|---|
| Přispěvatelé: | ONERA, Université de Toulouse ( ONERA, Université de Toulouse (F-31055 Toulouse - France) ), ONERA-PRES Université de Toulouse, DAAA, ONERA, Université Paris Saclay ( DAAA, ONERA, Université Paris Saclay (F-92190 Meudon - France) ), ONERA-Université Paris-Saclay, Institut Supérieur de l'Aéronautique et de l'Espace ( ISAE-SUPAERO ), Institut Clément Ader ( ICA ), Institut Supérieur de l'Aéronautique et de l'Espace ( ISAE-SUPAERO ) -IMT École nationale supérieure des Mines d'Albi-Carmaux ( IMT Mines Albi ) -Université Toulouse III - Paul Sabatier ( UPS ), Université Fédérale Toulouse Midi-Pyrénées-Université Fédérale Toulouse Midi-Pyrénées-Centre National de la Recherche Scientifique ( CNRS ) -Institut National des Sciences Appliquées - Toulouse ( INSA Toulouse ), Institut National des Sciences Appliquées ( INSA ) -Institut National des Sciences Appliquées ( INSA ), ONERA / DTIS, Université de Toulouse [Toulouse], DAAA, ONERA, Université Paris Saclay (COmUE) [Meudon], Département Conception et conduite des véhicules Aéronautiques et Spatiaux (DCAS), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO), Institut Clément Ader (ICA), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3), Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi), Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT), Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA)-Centre National de la Recherche Scientifique (CNRS)-Université Toulouse III - Paul Sabatier (UT3), Université Fédérale Toulouse Midi-Pyrénées-Université Fédérale Toulouse Midi-Pyrénées-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi), Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT)-Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO) |
| Jazyk: | angličtina |
| Rok vydání: | 2018 |
| Předmět: |
020301 aerospace & aeronautics
Computer science 02 engineering and technology Aerodynamics Hybrid aircraft Propulsion Sizing tool 01 natural sciences 7. Clean energy Automotive engineering Sizing 010305 fluids & plasmas 0203 mechanical engineering Work (electrical) Electrically powered spacecraft propulsion visual_art Electric aircraft [ PHYS.MECA.MEMA ] Physics [physics]/Mechanics [physics]/Mechanics of materials [physics.class-ph] 0103 physical sciences Electronic component Airframe Fast [SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph] visual_art.visual_art_medium Energy source |
| Zdroj: | 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2018, Florida, United States. 2018 Proceedings of AIAA Aerospace Sciences Meeting (Scitech) AIAA-Scitech 2018 AIAA-Scitech 2018, Jan 2018, Kissimmee, United States. pp. 1-33, ⟨10.2514/6.2018-1745⟩ AIAA-Scitech 2018, Jan 2018, Kissimmee, United States. pp. 1-33 |
| DOI: | 10.2514/6.2018-1745⟩ |
| Popis: | International audience; In order to reduce the CO2 emissions, a disruptive concept in aircraft propulsion has to be considered. As studied in the past years hybrid distributed electric propulsion is a promising option. In this work the feasibility of a new concept aircraft, using this technol- ogy, has been studied. Two different energy sources have been used: fuel based engines and batteries. The latters have been chosen because of their flexibility during operations and their promising improvements over next years. The technological horizon considered in this study is the 2035: thus some critical hypotheses have been made for electrical compo- nents, airframe and propulsion. Due to the uncertainty associated to these data, sensivity analyses have been performed in order to assess the impact of technologies variations. To evaluate the advantages of the proposed concept, a comparison with a conventional aircraft (EIS 2035), based on evolutions of today’s technology (airframe, propulsion, aerodynamics) has been made. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|