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Mission-Level Design Studies for Efficient Hybrid-Electric Regional Aircraft Concepts
Mälardalen University, School of Business, Society and Engineering, Future Energy Center.
Mälardalen University, School of Business, Society and Engineering, Future Energy Center.ORCID iD: 0000-0001-6101-2863
Department of Mechanical Engineering Aristotle University of Thessaloniki, Thessaloniki, 54124, Greece.
2024 (English)In: International Journal of Gas Turbine, Propulsion and Power Systems, ISSN 1882-5079, Vol. 15, no 1, p. 48-56Article in journal (Refereed) Published
Abstract [en]

This work delves into the design and operation of a series/parallel partial hybrid-electric architecture for regional aircraft. Employing a comprehensive approach, this study leverages mission-level analysis to optimize a 19-passenger hybrid-electric aircraft. The conceptual design framework employed is based on the OpenConcept library, and a systematic computational scheme is developed to effectively investigate the concept’s performance, utilizing the supplied and shaft power ratios. Through the examination of three distinct mission ranges and consideration of two technological scenarios, this work offers valuable insights. For the longest mission, an aircraft design optimization problem is posed, and a 23% reduction in total energy consumption is achieved for the optimistic technological scenario. On the other hand, the focus shifts to optimize the power management for shorter missions, where a 26% and a 32% reduction in energy consumption are achieved for the typical and short missions. The results highlight the potential of hybrid-electric propulsion for regional aircraft.

Place, publisher, year, edition, pages
Gas Turbine Society of Japan , 2024. Vol. 15, no 1, p. 48-56
Keywords [en]
Conceptual design, Hybrid electric aircraft, Aircraft concepts, Computational schemes, Design and operations, Design frameworks, Design studies, Level design, Performance, Power ratio, Series-parallel, Shaft power, Energy utilization
National Category
Energy Engineering
Identifiers
URN: urn:nbn:se:mdh:diva-66339DOI: 10.38036/jgpp.15.1_48Scopus ID: 2-s2.0-85188102039OAI: oai:DiVA.org:mdh-66339DiVA, id: diva2:1848185
Note

Article; Export Date: 02 April 2024; Cited By: 0

Available from: 2024-04-02 Created: 2024-04-02 Last updated: 2024-09-09Bibliographically approved
In thesis
1. Integrated Methodologies for Electrified Aircraft Design: From Conceptualization to Optimization
Open this publication in new window or tab >>Integrated Methodologies for Electrified Aircraft Design: From Conceptualization to Optimization
2024 (English)Doctoral thesis, comprehensive summary (Other academic)
Abstract [en]

This work explores the design and optimization of electrified configurations in aviation, focusing on the application and adaptation of these technologies across various aircraft classes. It utilizes a range of methodologies, including the development of a novel engine design approach, multi-disciplinary frameworks and the integration of surrogate modeling techniques, to enhance the conceptual design process and facilitate efficient exploration of complex design spaces.

This work demonstrates that electrified systems can significantly improve fuel efficiency and reduce emissions, particularly in short-haul applications where the current limitations of battery technology are less restrictive. The work identifies critical design trade-offs, such as the impact of battery weight on overall aircraft performance and the benefits of distributed propulsion systems in reducing aerodynamic drag and enhancing energy efficiency.

An uncertainty analysis further reveals the critical role of technological advancements in electrical powertrain components and their implications for the operational viability of electrified aircraft. The findings indicate that while near-term benefits can be achieved with current hybrid configurations, fully electrified aircraft will depend on future improvements in battery energy density and powertrain technologies.

Through these diverse methodologies and analyses, this work contributes to a deeper understanding of the challenges and opportunities in electrified aircraft design, offering insights that are crucial for advancing sustainable aviation.

Place, publisher, year, edition, pages
Västerås: Mälardalen University, 2024. p. 254
Series
Mälardalen University Press Dissertations, ISSN 1651-4238 ; 418
Keywords
Multi-disciplinary, Optimization, Electrified Propulsion, Uncertainty Analysis
National Category
Aerospace Engineering
Research subject
Energy- and Environmental Engineering
Identifiers
urn:nbn:se:mdh:diva-68386 (URN)978-91-7485-677-4 (ISBN)
Public defence
2024-11-08, Lambda, Mälardalens universitet, Västerås, 13:15 (English)
Opponent
Supervisors
Available from: 2024-09-10 Created: 2024-09-09 Last updated: 2024-10-10Bibliographically approved

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Diamantidou, EiriniZaccaria, Valentina

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