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/ | ||||||||
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| 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: |
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| DLR Supervisors: |
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| 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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