Kavvalos, Mavroudis (2026) On the Design and Analysis of Electrified Aero-engine Families. Dissertation, Mälardalen University.
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Offizielle URL: https://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-74488
Kurzfassung
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.
| elib-URL des Eintrags: | https://elib.dlr.de/223668/ | ||||||||
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| Dokumentart: | Hochschulschrift (Dissertation) | ||||||||
| Zusätzliche Informationen: | External Reviewer: Konstantinos Kyprianidis, Mälardalen University, Sweden; Anestis I. Kalfas, Aristotle University of Thessaloniki; Ioanna Aslanidou, Mälardalen University, Sweden | ||||||||
| Titel: | On the Design and Analysis of Electrified Aero-engine Families | ||||||||
| Autoren: |
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| DLR-Supervisor: |
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| Datum: | 2 Januar 2026 | ||||||||
| Erschienen in: | On the Design and Analysis of Electrified Aero-engine Families | ||||||||
| Open Access: | Nein | ||||||||
| Seitenanzahl: | 226 | ||||||||
| Status: | veröffentlicht | ||||||||
| Stichwörter: | 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 | ||||||||
| Abteilung: | Department of Engineering Sciences | ||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
| HGF - Programm: | Luftfahrt | ||||||||
| HGF - Programmthema: | Umweltschonender Antrieb | ||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||
| DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Triebwerkskonzepte und -integration | ||||||||
| Standort: | Köln-Porz | ||||||||
| Institute & Einrichtungen: | Institut für Antriebstechnik > Fan- und Verdichter | ||||||||
| Hinterlegt von: | Kavvalos, Mavroudis | ||||||||
| Hinterlegt am: | 27 Mär 2026 20:38 | ||||||||
| Letzte Änderung: | 27 Mär 2026 20:39 |
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