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Autor(en): Pettas, Vasilis
Salari, Mohammad
Schlipf, David
Cheng, Po Wen
Titel: Investigation on the potential of individual blade control for lifetime extension
Erscheinungsdatum: 2018
Dokumentart: Konferenzbeitrag
Konferenz: The Science of Making Torque from Wind TORQUE (2018, Mailand)
Seiten: 13
Erschienen in: Journal of physics, Conference series 1037 (2018), No. 032006
URI: http://nbn-resolving.de/urn:nbn:de:bsz:93-opus-ds-100700
http://elib.uni-stuttgart.de/handle/11682/10070
http://dx.doi.org/10.18419/opus-10053
ISSN: 1742-6588
Bemerkungen: This study was funded by the German Federal Ministry for Economic Affairs and Energy (BMWi) in the framework of the German joint research project ANWIND.
Zusammenfassung: In recent years the focus of wind energy industry is on reducing levelized cost of energy by rotor upscaling. Moreover, a current topic of interest to both industry and academia is the extension of lifetime to existing wind turbines approaching the end of initial design span. Thus, the need for load alleviation technologies integrated in the design process or for retrofit purposes is becoming more relevant. One of these is individual blade pitch control, a recurring topic in research, with known advantages and weaknesses namely the pitch actuator and bearing wear. The present work suggests such a system incorporating three independent controllers with input the root bending moments on the rotating frame. The linear system used for controller design is based on black box identification of non-linear simulations and filters are used both for the input and output. Different setups of the independent blade control scheme are applied on a 10 MW reference turbine, with a large and highly flexible rotor representative of the current industrial status, under wind conditions as defined by relevant certification standards. The investigation aims on evaluating the system’s performance based on the fatigue load alleviation potential for different components as well as identifying the tradeoff for each design choice. Finally, based on basic assumptions the reductions are translated to possible life time extension for each component based on a combined operation where the new controllers are applied for a percentage of the initial 20 year lifetime.
Enthalten in den Sammlungen:06 Fakultät Luft- und Raumfahrttechnik und Geodäsie

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