Küfmann, Philip und Bartels, Rainer und van der Wall, Berend G. und Schneider, Oliver und Holthusen, Hermann und Gomes, Jorge (2017) The First Wind Tunnel Test of the Multiple Swashplate System: Test Procedure and Principal Results. Journal of the American Helicopter Society, 62 (4), Seiten 1-13. American Helicopter Society. doi: 10.4050/JAHS.62.042002. ISSN 0002-8711.
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Kurzfassung
In September 2015, the DLR completed the first wind tunnel test of its patented Multiple Swashplate System in the DNW's Large Low-Speed Facility in the Netherlands. During these tests, the potential of this new active rotor control system to effectively reduce noise, vibration, and power consumption using several individual blade control strategies, including 2/rev inputs, was successfully demonstrated on two different model rotors without using actuators in the rotating frame. For a Mach-scaled Bo105 model, rotor power reductions of up to 4% in level flight and reductions of the weighted 4/rev vibratory hub loads of up to 77% in a descent flight condition were measured, and BVI noise levels were reduced by up to 4.5 dB by the application of 3/rev higher harmonic control, confirming findings from the HART II test. For the second model rotor using a contemporary blade geometry, the maximum reductions were measured at 3%, 52%, and 3.9 dB for power, vibration, and BVI noise, respectively.
elib-URL des Eintrags: | https://elib.dlr.de/114309/ | ||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||
Titel: | The First Wind Tunnel Test of the Multiple Swashplate System: Test Procedure and Principal Results | ||||||||||||||||||||||||||||
Autoren: |
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Datum: | 21 August 2017 | ||||||||||||||||||||||||||||
Erschienen in: | Journal of the American Helicopter Society | ||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||
Band: | 62 | ||||||||||||||||||||||||||||
DOI: | 10.4050/JAHS.62.042002 | ||||||||||||||||||||||||||||
Seitenbereich: | Seiten 1-13 | ||||||||||||||||||||||||||||
Verlag: | American Helicopter Society | ||||||||||||||||||||||||||||
ISSN: | 0002-8711 | ||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||
Stichwörter: | HHC, IBC, Multiple Swashplate System, helicopter, Vibration control, noise reduction | ||||||||||||||||||||||||||||
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 leise und komfortable Drehflügler (alt), L - Der Innovative Drehflügler (alt) | ||||||||||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Flugsystemtechnik > Hubschrauber | ||||||||||||||||||||||||||||
Hinterlegt von: | Küfmann, Philip | ||||||||||||||||||||||||||||
Hinterlegt am: | 25 Okt 2017 16:23 | ||||||||||||||||||||||||||||
Letzte Änderung: | 02 Nov 2023 13:28 |
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