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Volumn 1, Issue , 2010, Pages 111-121

Novel concept for realizing individual blade control (IBC) for helicopters

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT CONTROL SYSTEMS; HELICOPTER ROTORS; HELICOPTERS; HYDRAULIC ACTUATORS; ROTORS; TURBOMACHINE BLADES; VORTEX FLOW;

EID: 84880477447     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (16)

References (28)
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  • 2
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  • 5
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  • 6
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    • Active rotor control for helicopters: Individual blade control and swashplateless rotor designs
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    • Kessler, Ch.1
  • 7
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    • Second harmonic control on the helicopter rotor
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    • (1952) ARC Reports and Memoranda , Issue.2997
    • Steward, W.1
  • 8
    • 84946535841 scopus 로고
    • Higher harmonic rotor control: The possibilities of third and higher harmonic feathering for delaying the stall limit in helicopters
    • Payne, P.R.: Higher Harmonic Rotor Control: The Possibilities of Third and Higher Harmonic Feathering for Delaying the Stall Limit in Helicopters, Aircraft Engineering, Vol. 30, No. 8, pp. 222-226, 1958.
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    • Payne, P.R.1
  • 9
    • 0012753456 scopus 로고
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    • Arcidiacono, P.J.: Theoretical Performance of Helicopters Having Second and Higher Harmonic Feathering Control, Journal of the AHS, Vol. 6, No. 8, pp. 8-19, 1961.
    • (1961) Journal of the AHS , vol.6 , Issue.8 , pp. 8-19
    • Arcidiacono, P.J.1
  • 11
    • 0021816938 scopus 로고
    • On developing and flight testing a higher harmonic control system
    • Wood, E.R., Powers, R.W., Cline, J.H., Hammond, CE.: On Developing and Flight Testing a Higher Harmonic Control System, Journal of the AHS, Vol. 30, No. 1, pp. 3-20,1985.
    • (1985) Journal of the AHS , vol.30 , Issue.1 , pp. 3-20
    • Wood, E.R.1    Powers, R.W.2    Cline, J.H.3    Hammond, C.E.4
  • 13
    • 84921421829 scopus 로고
    • A simple system for helicopter individ-ual-blade-cohtrol and its application to gust alleviation
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    • Ham, N.D.1
  • 14
    • 0002772209 scopus 로고
    • Helicopter rotor lag damping augmentation through individual-blade-control
    • Ham, N.D., Behal, B.L., McKillip R.M.: Helicopter Rotor Lag Damping Augmentation Through Individual-Blade-Control, Vertica, Vol. 7, No. 4, pp. 361-371, 1983.
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  • 15
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    • Testing and evaluation of a stall-flutter-suppression system for helicopter rotors using individual-blade-control
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    • Quackenbush, T.R.1
  • 16
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  • 18
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  • 21
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  • 26
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  • 27
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.