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On the Design and Analysis of Electrified Aero-engine Families

Kavvalos, Mavroudis (2026) On the Design and Analysis of Electrified Aero-engine Families. Dissertation, Mälardalen University.

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Official URL: https://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-74488

Abstract

Rather than designing a new engine from scratch for every aircraft application, manufacturers often develop families of engines that share a common core; typically comprising the high-pressure compressor, combustor, and high-pressure turbine. This strategy reduces cost, shortens development time, and mitigates technical risk, making it an attractive option in today’s evolving aerospace landscape. Common-core variants are always associated with performance penalties compared to individually optimized clean-sheet engines because the initial core design is compromised to allow for adjustment of its component map entry points, but there is a high potential for better economics of the entire engine program.

To address these challenges, this thesis introduces a simulation methodology for assessing both conventional and electrified aero-engine architectures, including turbofans, turboprops, and distributed electric propulsion systems. Based on a multi-point synthesis approach, the framework supports performance evaluation across multiple fidelity levels: from 0D thermodynamic cycle modeling, to 1D mean-line design, and up to 2D throughflow component analysis.A particular focus is placed on electrically driven propulsors, evaluated both as standalone units and within turbo-electric configurations. These include variants featuring variable geometry, such as variable pitch fans and variable area nozzles, when necessary.

Building on the standalone engine modeling foundation, a novel methodology is introduced for simulating common-core engine variants within an aero-engine family. This extends the multi-point synthesis approach by treating the design point of each variant as an additional off-design condition of the baseline (first-to-enter-the-market) engine. To demonstrate its application, an electrified turboprop engine family is designed and analyzed across a range of power growth scenarios. Clean-sheet engine designs are developed in parallel to serve as benchmarks, enabling quantification of the performance penalties associated with enforcing commonality across various levels of power growth.

Item URL in elib:https://elib.dlr.de/223668/
Document Type:Thesis (Dissertation)
Additional Information:External Reviewer: Konstantinos Kyprianidis, Mälardalen University, Sweden; Anestis I. Kalfas, Aristotle University of Thessaloniki; Ioanna Aslanidou, Mälardalen University, Sweden
Title:On the Design and Analysis of Electrified Aero-engine Families
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kavvalos, Mavroudismavroudis.kavvalos (at) dlr.dehttps://orcid.org/0000-0001-9922-3690209947739
DLR Supervisors:
ContributionDLR SupervisorInstitution or E-MailDLR Supervisor's ORCID iD
Thesis advisorSchnell, RainerRainer.Schnell (at) dlr.deUNSPECIFIED
Date:2 January 2026
Journal or Publication Title:On the Design and Analysis of Electrified Aero-engine Families
Open Access:No
Number of Pages:226
Status:Published
Keywords:common-core, core commonality, growth engine, performance, conceptual design, turboprops, electrification, multi-point synthesis, mean-line analysis, throughflow, multi-stage axial compressor
Institution:Mälardalen University
Department:Department of Engineering Sciences
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Future Engines and Engine Integration
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Kavvalos, Mavroudis
Deposited On:27 Mar 2026 20:38
Last Modified:27 Mar 2026 20:39

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