van der Wall, Berend G. und Lehmann, Paul Hermann (2018) About the Impact of Wind Turbine Blade Tip Vortices on Helicopter Rotor Trim and Rotor Blade Motion. CEAS Aeronautical Journal, 9 (1), Seiten 1-18. Springer. doi: 10.1007/s13272-017-0276-x. ISSN 1869-5590.
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Kurzfassung
With increasing numbers of large wind turbines on-shore and off-shore, interactions of their wake with helicopters become a subject worth investigating. In this paper the wake is modeled as a tip vortex helix with a vortex strength estimated from the wind turbine thrust. Helicopter rotors of different size and hub layout are subjected to the wake and the collective and cyclic control inputs required to keep the trim are compared to the maximum available control range of the rotorcraft. In addition the blade flapping response due to the vortex influence without pilot action is computed and compared to maximum allowed flapping angles. It is found that typical on-shore wind turbines could be a hazard for ultralight helicopters, but not for larger helicopters. Large off-shore wind turbines, however, could even be a danger for small helicopters that may be used for maintenance. In addition the results are compared to fixed-wing wake vortex interaction with a helicopter as given in the literature.
elib-URL des Eintrags: | https://elib.dlr.de/112960/ | ||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||
Titel: | About the Impact of Wind Turbine Blade Tip Vortices on Helicopter Rotor Trim and Rotor Blade Motion | ||||||||||||
Autoren: |
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Datum: | 20 Januar 2018 | ||||||||||||
Erschienen in: | CEAS Aeronautical Journal | ||||||||||||
Referierte Publikation: | Ja | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Ja | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
Band: | 9 | ||||||||||||
DOI: | 10.1007/s13272-017-0276-x | ||||||||||||
Seitenbereich: | Seiten 1-18 | ||||||||||||
Verlag: | Springer | ||||||||||||
ISSN: | 1869-5590 | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | Wake vortex interaction, helicopter rotor trim, rotor blade motion | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||
HGF - Programmthema: | Hubschrauber | ||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||
DLR - Forschungsgebiet: | L RR - Rotorcraft Research | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Der Innovative Drehflügler (alt) | ||||||||||||
Standort: | Braunschweig | ||||||||||||
Institute & Einrichtungen: | Institut für Flugsystemtechnik > Hubschrauber | ||||||||||||
Hinterlegt von: | van der Wall, Prof. Dr. Berend G. | ||||||||||||
Hinterlegt am: | 15 Feb 2018 15:17 | ||||||||||||
Letzte Änderung: | 21 Nov 2023 08:01 |
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