Research Article

Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System

Volume: 03 Number: 01 June 28, 2022
EN

Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System

Abstract

Thanks to its typical limited speeds and altitudes, Urban Air Mobility represents an interesting application for electric and hybrid-electric power systems. In addition, short-range requirements are compatible with limited performance of today batteries, conversely to their current inapplicability for commercial aviation purposes. For the present study, a parallel Hybrid Electric Propulsion System for a coaxial-rotor Air Taxi has been implemented in Simulink and tested on four different sets of operating conditions, with a transient signal as input for Power Lever Angle command. The goal of this investigation is to analyse transient behaviour of the hybrid electric propulsion system in question, to underline the role of electric motors in assisting thermal engine during transients, and, in particular, it focuses on the benefits deriving from the adoption of a coordination block which adapts torque split between the two power sources on the basis of actual engine response.

Keywords

Supporting Institution

Italian Ministry for Education, University and Research

Project Number

PON SMEA 03PE_00067_5

References

  1. Donateo, T., De Pascalis, C., Strafella, L. and Ficarella, A., 2021, Off-line and On-line Optimization of the Energy Management Strategy in a Hybrid Electric Helicopter for Urban Air-Mobility. Aerospace Science and Technology, 113
  2. Wang, C., Li, Y.G. and Yang, B.Y., 2017, Transient performance simulation of aircraft engine integrated with fuel and control systems. Applied Thermal Engineering, 114, pp.1029-1037

Details

Primary Language

English

Subjects

Aerospace Engineering

Journal Section

Research Article

Publication Date

June 28, 2022

Submission Date

January 11, 2022

Acceptance Date

April 30, 2022

Published in Issue

Year 2022 Volume: 03 Number: 01

APA
Donateo, T., Spada Chiodo, L., & Ficarella, A. (2022). Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System. International Journal of Aviation Science and Technology, 03(01), 4-12. https://izlik.org/JA95MT67DG
AMA
1.Donateo T, Spada Chiodo L, Ficarella A. Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System. IJAST. 2022;03(01):4-12. https://izlik.org/JA95MT67DG
Chicago
Donateo, Teresa, Ludovica Spada Chiodo, and Antonio Ficarella. 2022. “Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System”. International Journal of Aviation Science and Technology 03 (01): 4-12. https://izlik.org/JA95MT67DG.
EndNote
Donateo T, Spada Chiodo L, Ficarella A (June 1, 2022) Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System. International Journal of Aviation Science and Technology 03 01 4–12.
IEEE
[1]T. Donateo, L. Spada Chiodo, and A. Ficarella, “Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System”, IJAST, vol. 03, no. 01, pp. 4–12, June 2022, [Online]. Available: https://izlik.org/JA95MT67DG
ISNAD
Donateo, Teresa - Spada Chiodo, Ludovica - Ficarella, Antonio. “Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System”. International Journal of Aviation Science and Technology 03/01 (June 1, 2022): 4-12. https://izlik.org/JA95MT67DG.
JAMA
1.Donateo T, Spada Chiodo L, Ficarella A. Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System. IJAST. 2022;03:4–12.
MLA
Donateo, Teresa, et al. “Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System”. International Journal of Aviation Science and Technology, vol. 03, no. 01, June 2022, pp. 4-12, https://izlik.org/JA95MT67DG.
Vancouver
1.Teresa Donateo, Ludovica Spada Chiodo, Antonio Ficarella. Effect of Coordination on Transient Response of a Hybrid Electric Propulsion System. IJAST [Internet]. 2022 Jun. 1;03(01):4-12. Available from: https://izlik.org/JA95MT67DG

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