Design of a Battery Pack for the Power System of an All-Electric Aircraft by Cell Characterization

Bossi Giuseppe
First
;Floris Andrea
Second
;Damiano Alfonso
Last
2023-01-01

Abstract

The battery characterization and modelling of a Lithium-ion battery aimed at supporting the design of the energy storage system of an All-Electric Aircraft (AEA) is presented. Specifically, the developed model is employed to evaluate the energy and power performance of a battery pack designed for the AEA concept X- 57 Maxwell Mod.II. The preliminary battery pack sizing is performed referring to a project-flight mission-oriented to air city taxing. The evaluation of the design targets satisfaction has been verified through a simulation study based on the proposed battery modelling. The comparison between the simulation and preliminary results confirms the need of employing a battery dynamic model for designing AEA's battery pack that satisfies all targets imposed.
2023
Inglese
Proc. of 2023 International Conference on Clean Electrical Power, ICCEP 2023
9798350348378
76
82
7
2-s2.0-85173615967
2023 International Conference on Clean Electrical Power (ICCEP 2023)
Contributo
Esperti anonimi
27-29 June 2023
Terrasini (Italy)
internazionale
scientifica
all electric aircraft; Battery modelling and characterization; battery pack design
Goal 7: Affordable and clean energy
Goal 13: Climate action
no
4 Contributo in Atti di Convegno (Proceeding)::4.1 Contributo in Atti di convegno
Bossi, Giuseppe; Floris, Andrea; Campagna, Nicola; Miceli, Rosario; Damiano, Alfonso
273
5
4.1 Contributo in Atti di convegno
none
info:eu-repo/semantics/conferencePaper
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