Verlagslink DOI: 10.1243/09544100JAERO857
Titel: A knowledge-based approach for design and modelling of high lift actuation systems
Sprache: English
Autor/Autorin: Pfennig, M. 
Thielecke, F. 
Schlagwörter: high lift actuation system;system design;modelling and simulation;flight control;systems engineering;knowledge-based systems
Erscheinungsdatum: 2011
Verlag: Sage Publ.
Quellenangabe: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 3 (225): 302-311 (2011)
Zeitschrift oder Schriftenreihe: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 
Zusammenfassung (englisch): High lift actuation system design is a highly iterative process. Especially the preliminary design phase, which sets the course for the following design steps, is characterized by uncertain and changing data input. Despite the importance of this early design phase, a specialized and integrated computational support is not available. The objective of the research project WissBaSys is to offer knowledge-based design assistance focused on the preliminary design of high lift actuation systems. Moreover, information concerning a specific drive system architecture and component data can be used for an automated model generation leading to a significant time reduction and enhanced traceability. A capable approach for order reduction of shaft transmission models, as well as the concept for computer-aided modelling, is presented in this article.
URN: nbn:de:gbv:830-88218734
DOI: 10.15480/882.1534
ISSN: 2041-3025
Institut: Flugzeug-Systemtechnik M-7 
Dokumenttyp: (wissenschaftlicher) Artikel
Lizenzhinweis: Dieser Beitrag ist mit Zustimmung des Rechteinhabers aufgrund einer (DFG geförderten) Allianz- bzw. Nationallizenz frei zugänglich. This publication is with permission of the rights owner freely accessible due to an Alliance licence and a national licence (funded by the DFG, German Research Foundation) respectively.
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