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The Growth Engine Concept and Its Potential for an Electrified Aviation Future
Mälardalen University, School of Business, Society and Engineering, Future Energy Center.
Mälardalen University, School of Business, Society and Engineering, Future Energy Center.ORCID iD: 0000-0002-8466-356X
AURA-AERO, Cugnaux, 312 70, France.
2024 (English)In: Journal of engineering for gas turbines and power, ISSN 0742-4795, E-ISSN 1528-8919, Vol. 146, no 7, article id 070901Article in journal (Refereed) Published
Abstract [en]

The emerging need for cost- and energy-efficient propulsion systems have shifted the research interest to radical concepts, with several challenges to overcome in order to enter into service. However, revitalizing old yet provably successful engine designs-a practice followed by engine manufacturers over the years-can provide low-risk alternative solutions to move immediate market demands. The paper reviews this approach, known as concept of growth engines or core commonality, and investigates how a geometrically fixed or geometrically similar engine core can be utilized across a family of engines. The development programs of the highly successful CFM56 and PT6 engine families are analyzed, proving the success of this concept over the years. The idea is based on the engineering paradigm of product families and is briefly presented from a theoretical perspective. Implementation methods and simulation tools to initiate, conceptualize, design, and evaluate an engine family program are reviewed. The potential application of engine core commonality into electrified propulsion systems is investigated. Design challenges and opportunities that electrification imposes to the growth engine concept are discussed. Finally, the concept of growth electrified propulsion systems is introduced, conveying future research directions to achieve a successful family of engines for electrified applications.

Place, publisher, year, edition, pages
ASME International , 2024. Vol. 146, no 7, article id 070901
Keywords [en]
CFM56, core commonality, electrification, engine family, engine variant, growth engines, PT6, Electric utilities, Energy efficiency, Cost-efficient, Energy efficient, Engine variants, Growth engine, Propulsion system, Engines
National Category
Energy Engineering
Identifiers
URN: urn:nbn:se:mdh:diva-66335DOI: 10.1115/1.4063193ISI: 001240440800016Scopus ID: 2-s2.0-85187710513OAI: oai:DiVA.org:mdh-66335DiVA, id: diva2:1848194
Available from: 2024-04-02 Created: 2024-04-02 Last updated: 2025-11-24Bibliographically approved
In thesis
1. On the Design and Analysis of Electrified Aero-engine Families
Open this publication in new window or tab >>On the Design and Analysis of Electrified Aero-engine Families
2026 (English)Doctoral thesis, comprehensive summary (Other academic)
Abstract [en]

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.

Place, publisher, year, edition, pages
Västerås: Mälardalens universitet, 2026
Series
Mälardalen University Press Dissertations, ISSN 1651-4238 ; 455
National Category
Environmental Engineering Vehicle and Aerospace Engineering
Research subject
Energy- and Environmental Engineering
Identifiers
urn:nbn:se:mdh:diva-74488 (URN)978-91-7485-738-2 (ISBN)
Public defence
2026-01-23, Delta, Mälardalen University, Västerås, 09:00 (English)
Opponent
Supervisors
Available from: 2025-11-25 Created: 2025-11-24 Last updated: 2026-01-02Bibliographically approved

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Kavvalos, MavroudisKyprianidis, Konstantinos

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