elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Barrierefreiheit | Kontakt | English
Schriftgröße: [-] Text [+]

Multidisciplinary Optimization of Hydrogen Fuel Distribution System Architectures for Conceptual Aircraft Design

Garg, Sparsh und Neves, Diogo und Burschyk, Tim und Boggero, Luca und Nagel, Bjoern (2026) Multidisciplinary Optimization of Hydrogen Fuel Distribution System Architectures for Conceptual Aircraft Design. In: AIAA AVIATION 2026 Forum. American Institute of Aeronautics and Astronautics, Inc.. AIAA AVIATION 2026 Forum, 2026-06-08 - 2026-06-12, San Diego, CA, USA. doi: 10.2514/6.2026-4178.

[img] PDF
1MB

Offizielle URL: https://arc.aiaa.org/doi/abs/10.2514/6.2026-4178

Kurzfassung

The transition toward sustainable aviation has intensified the exploration of alternative propulsion technologies, with hydrogen fuel cells emerging as a promising candidate. This study addresses existing knowledge gaps in the design and integration of hydrogen fuel systems for aircraft, aiming to support informed decision-making during early conceptual design stages. A system architecture optimization (SAO) framework is employed to investigate the design space of the hydrogen fuel system for a fuel-cell-powered regional airliner. The work leverages the German Aerospace Center’s (DLR) collaborative engineering ecosystem, comprising the ADORE, MDAx, and RCE platforms, which collectively enable the integration of model-based systems engineering (MBSE) and multidisciplinary design analysis and optimization (MDAO) for automated architecture exploration. The Common Parametric Aircraft Configuration Schema (CPACS) serves as the central data model, ensuring consistent information exchange between tools and disciplines. The optimization problem is formulated to minimize both system mass and electrical power consumption, with several architectural design choices treated as decision variables. The performance of the NSGA-II evolutionary algorithm is benchmarked against a surrogate-assisted Bayesian optimization approach to evaluate their respective efficiencies in navigating the complex design space. Furthermore, the advantages of employing an automated architecting methodology are quantified through comparison with traditional, expert-driven approaches. This research not only demonstrates the applicability of SAO in a realistic aerospace engineering context but also establishes a foundation for future investigations into hydrogen fuel system architectures. The framework can be extended to incorporate broader system boundaries and more comprehensive design studies, thereby contributing to the development of next-generation sustainable aircraft propulsion systems.

elib-URL des Eintrags:https://elib.dlr.de/226660/
Dokumentart:Konferenzbeitrag (Vorlesung)
Titel:Multidisciplinary Optimization of Hydrogen Fuel Distribution System Architectures for Conceptual Aircraft Design
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Garg, Sparshsparsh.garg (at) dlr.dehttps://orcid.org/0009-0003-8567-6471227297519
Neves, DiogoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Burschyk, TimTim.Burschyk (at) dlr.dehttps://orcid.org/0000-0002-4241-0046227297520
Boggero, LucaLuca.Boggero (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Nagel, Bjoernbjörn.nagel (at) dlr.dehttps://orcid.org/0000-0001-8076-9853NICHT SPEZIFIZIERT
Datum:4 Juni 2026
Erschienen in:AIAA AVIATION 2026 Forum
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.2514/6.2026-4178
Verlag:American Institute of Aeronautics and Astronautics, Inc.
Status:veröffentlicht
Stichwörter:Dynamic multidisciplinary design analysis and optimization, Aircraft Design, automation
Veranstaltungstitel:AIAA AVIATION 2026 Forum
Veranstaltungsort:San Diego, CA, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:8 Juni 2026
Veranstaltungsende:12 Juni 2026
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Flugzeugtechnologien und Integration
Standort: Hamburg
Institute & Einrichtungen:Institut für Systemarchitekturen in der Luftfahrt
Hinterlegt von: Garg, Sparsh
Hinterlegt am:21 Sep 2026 07:41
Letzte Änderung:22 Sep 2026 08:13

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
OpenAIRE Validator logo electronic library verwendet EPrints
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.