Systematic Architecture Generation for the Design of Aircraft Propulsive Systems
Year: 2026
Type: article
Abstract: Sustainability objectives in the aeronautical industry push companies toward novel aircraft propulsive systems (e.g., hybrid electric or hydrogen-based). Coupled with reliability constraints for certification, this creates a potentially highly complex propulsive architecture design. Thus, tools and methods are needed to explore this growing system design space efficiently. Several critical features have been identified by system architects in one of the leading companies in this domain: consideration of parallel functional chains for safety and redundancy reasons, systematic exploration of the design space, and the possibility to systematically generate from functional domain onto the physical domain of the system architecture. The article proposed a Design Structure Matrix (DSM)-based system architecture generation and design methodology with the objective to consider both parallel and branching system architectures, while supporting this systematic generation from the functional to the physical domain. The methodology was compared with previous case studies. Moreover, it has been tested and validated in the industrial setting. Both the generation process and the constraints were tested for the design of aircraft propulsive systems. The aim of this research is to propose a first step allowing for systematic exploration of system architectures that can be further integrated into existing simulation workflows, enabling the performance of propulsion architectures to be estimated systematically and more quickly than with manual analyses.
Source: Journal of Mechanical Design
DOI: 10.1115/1.4071910
Authors: Enzo Della Bella, Marija Jankovic, Valérie Pommier-Budinger, Scott Delbecq, Joël Jezegou, Alain Lefebvre
Language: English
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green
Award: G8351670659
OpenAlex ID: W7160876170
