Coupled hybrid electric aircraft design and strategic airline planning

Master Thesis (2023)
Author(s)

E. Scheers (TU Delft - Aerospace Engineering)

Contributor(s)

Maurice F.M. Hoogreef – Mentor (TU Delft - Flight Performance and Propulsion)

P. Proesmans – Mentor (TU Delft - Flight Performance and Propulsion)

B.F. F Santos – Coach (TU Delft - Air Transport & Operations)

F. Oliviero – Coach (TU Delft - Flight Performance and Propulsion)

Faculty
Aerospace Engineering
Copyright
© 2023 Elise Scheers
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 Elise Scheers
Graduation Date
13-03-2023
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
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Abstract

With the aviation sector growing each year, the need for a reduced climate impact is becoming increasingly important. Electrification of the propulsion system is believed to offer promising avenues in achieving this reduction. Additionally, airlines operating these aircraft have to adapt their operations and network to optimally utilize these aircraft. This research presents a methodology for the coupled design of a hybrid-electric aircraft fleet with strategic airline planning to optimally serve a specific network. The objective is to maximize the airline profit and minimize the network CO2 emissions. Aircraft design trade-offs in payload, range and runway length will guide the creation of new aircraft until the optimal aircraft fleet is determined. The methodology is tested in a case study for the regional airline network of SATA Air Acores. The study investigates the impact of introducing new hybrid-electric aircraft designs in the fleet on the creation of new aircraft, the aircraft allocation and the network performance. By directly integrating hybrid-electric aircraft design (having a parallel hybrid architecture) with strategic airline planning, it is possible to reduce the network CO2emissions by -11% at the cost of an airline profit decrease of -13%. When including a climate optimization, an additional reduction of network CO2 emissions is achieved of -27% with a small additional decrease in profit of -1%. Network profitability and climate impact are mainly dictated by the fleet diversity and the assumed technology level of the batteries employed in the aircraft. This research highlights the importance of including climate optimization in the design of new aircraft and the need for more advanced hybrid-electric propulsion architectures (such as distributed propulsion systems) to further contribute to climate impact reduction.

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