Energy consumption of Aircraft with new propulsion systems and storage media

Yri Amandine Kambiri; Thierry Druot; Pascal Roches; Nicolas Peteilh; Nicolas Monrolin; Xavier Carbonneau

doi:10.2514/6.2024-1707

Proceedings/Recueil Des Communications Année : 2024

Energy consumption of Aircraft with new propulsion systems and storage media

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Yri Amandine Kambiri

Fonction : Auteur

ENAC, University of Toulouse

Institut Supérieur de l'Aéronautique et de l'Espace

Thierry Druot

Fonction : Auteur

ENAC, University of Toulouse

Pascal Roches

Fonction : Auteur

ENAC, University of Toulouse

Nicolas Peteilh

Fonction : Auteur
PersonId : 734851
IdHAL : nicolas-peteilh
ORCID : 0000-0003-0142-3374
IdRef : 253120691

Ecole Nationale de l'Aviation Civile

Nicolas Monrolin

Fonction : Auteur
PersonId : 1351093
IdHAL : nicolasmonrolin
ORCID : 0000-0002-3282-1271

Ecole Nationale de l'Aviation Civile

Université de Toulouse

Xavier Carbonneau

Fonction : Auteur

Institut Supérieur de l'Aéronautique et de l'Espace

Résumé

The transition from fossil fuels to the use of sustainable energy sources is an important challenge for aviation. A particularly critical question is to identify the best mix of energies for the future air transport system. In this quest, the capability to simulate various complex scenarios, varying assumptions, models, and objectives, will play an important part. This paper provides a simple and very rapid tool to evaluate the energy consumption of parametric airplane configurations with thermal propulsion powered by kerosene, methane, hydrogen, or electric propulsion powered by hydrogen fuel cells or batteries. The maturity of the different technologies is driven by a small number of global indices that are easy to connect with state of the art or forecasts. The user can freely select the capacity, range, speed, and propulsion system of the airplane, and simulate its operations over any missions within its payload-range envelope. The tool has been validated on its capability to reproduce the characteristic weights of a range of very different aircraft, from A380 to general aviation airplanes. Finally, three use cases are presented. The first one allowed us to identify the level of technological challenge of the Alice aircraft project from EVIATION. The second one is a short mapping of the transportation potential of five different propulsion systems for the segment of 19-passenger commuter airplanes. The third use case puts the thermal hydrogen aircraft in the perspective of existing kerosene airplanes in terms of energy and structural efficiency, and reveals an optimum of the hydrogen technology.

Mots clés

Energy transition Hydrogen SAF Sustainable Aviation Fuel fuel cell aircraft design multidisciplinary optimization MDO

Domaines

Mathématiques [math] Sciences de l'ingénieur [physics]

Fichier principal

Ghost_airplane_for_AIAA.pdf (1.4 Mo)

Alice Pareto Front.png (36.95 Ko)

Alice Transport Efficiencies.png (41.29 Ko)

Alice Transport Energy Efficiency at Design.png (60.77 Ko)

Alice Transport Energy Efficiency in Operation.png (44.57 Ko)

Alice Transport Mass Efficiency at Design.png (59.21 Ko)

Alice trade aero-structure.png (45.28 Ko)

Alice trade energy_density-best_range.png (46.99 Ko)

Capture d’écran (61).png (39.98 Ko)

Capture d’écran (62).png (4.31 Ko)

Capture d’écran (63).png (36.2 Ko)

Estimated_MTOW_vs_Published_MTOW.png (57.23 Ko)

Estimated_OWE_vs_Published_OWE.png (62.46 Ko)

Generalized_Power_Index_Regression (1).png (57.22 Ko)

Generalized_Power_Index_Regression.png (57.22 Ko)

PDF of MTOW relative error.png (21.78 Ko)

PDF of OWE relative error.png (23.15 Ko)

PSFC_regression.png (51.33 Ko)

Piston_mass_regression.png (44.5 Ko)

Potential_transport_efficiency.png (71.9 Ko)

Potential_transport_efficiency_long_range_v2.png (116.13 Ko)

Potential_transport_efficiency_overview.png (89.62 Ko)

Regression_Basic_MWE_MTOW.png (56.87 Ko)

Regression_OWE_MTOW.png (54.87 Ko)

TSFC_model_comparison_V2.png (74.53 Ko)

TSFC_regression_Mach0.78.png (39.76 Ko)

TSFC_regression_Mach0.82.png (35.16 Ko)

Theoretical_LoD.png (36.5 Ko)

Turbofan_mass_regression.png (45.88 Ko)

Turboshaft_mass_regression.png (48.61 Ko)

alice.png (59.87 Ko)

bactt1.png (40.3 Ko)

batt1.png (34.14 Ko)

bestbat.png (42.48 Ko)

bestran.png (76.24 Ko)

commuter_design_potential.png (79.48 Ko)

eff.png (63.73 Ko)

efff.png (70.97 Ko)

efffp.png (74.37 Ko)

gravim_index.png (124.35 Ko)

hf.png (38.3 Ko)

imth.png (141.82 Ko)

lod model.png (38.94 Ko)

long_range.png (70.68 Ko)

m_furn_VS_range.pdf (12.43 Ko)

main.pdf (357.8 Ko)

max_range_for_CS23.png (51.02 Ko)

maxran.png (40.18 Ko)

parefr.png (35.78 Ko)

pareto.png (35.78 Ko)

pkrange.png (39.37 Ko)

psfc_pro.png (33.61 Ko)

reg owe_mtow.png (53.86 Ko)

reg_baz_mtow.png (58.69 Ko)

tableghost.png (27.34 Ko)

thi3.png (15.28 Ko)

thierry1.png (8.6 Ko)

tranef.png (52.34 Ko)

transport.png (36.92 Ko)

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https://enac.hal.science/hal-04456943

Soumis le : mercredi 14 février 2024-11:24:31

Dernière modification le : jeudi 14 novembre 2024-16:40:07

Dates et versions

hal-04456943 , version 1 (14-02-2024)

Licence

Paternité - Pas de modifications

Identifiants

HAL Id : hal-04456943 , version 1
DOI : 10.2514/6.2024-1707

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Yri Amandine Kambiri, Thierry Druot, Pascal Roches, Nicolas Peteilh, Nicolas Monrolin, et al.. Energy consumption of Aircraft with new propulsion systems and storage media. AIAA SCITECH 2024 Forum, American Institute of Aeronautics and Astronautics, 2024, ⟨10.2514/6.2024-1707⟩. ⟨hal-04456943⟩

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Energy consumption of Aircraft with new propulsion systems and storage media

Résumé

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Dates et versions

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