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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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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/
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:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Kavvalos, Mavroudismavroudis.kavvalos (at) dlr.dehttps://orcid.org/0000-0001-9922-3690209947739
DLR-Supervisor:
BeitragsartDLR-SupervisorInstitution oder E-Mail-AdresseDLR-Supervisor-ORCID-iD
Thesis advisorSchnell, RainerRainer.Schnell (at) dlr.deNICHT SPEZIFIZIERT
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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