This paper discusses the preparations and plans to test an individual rotor blade pitch control system in the 40- by 80- Foot Wind Tunnel at the NASA Ames Research Center. The test will be performed on a full-scale BO-105 rotor system using a control system made by Henschel Flugzeug-Werke, GmbH, Germany. The Individual Blade Control (IBC) actuators have been designed to replace the pitchlinks of the rotor system. The paper prensets a brief historical perspective on the development of the individual blade control system and then describes the present IBC actuators and the wind tunnel test hardware. A discussion of the intended test matrix, expected potential benefits of IBC, and simulation results are included.


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    Titel :

    Full-scale wind tunnel investigation of a helicopter individual blade control system


    Weitere Titelangaben:

    Die Untersuchung eines individuellen Regelsystems für Rotorblätter, getestet in natürlicher Größe in einem Windkanal


    Beteiligte:
    Jacklin, S.A. (Autor:in) / Leyland, J.A. (Autor:in) / Blaas, A. (Autor:in)


    Erscheinungsdatum :

    1993


    Format / Umfang :

    11 Seiten, 16 Bilder, 2 Tabellen, 28 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    JACKLIN, STEPHEN / LEYLAND, JANE / BLAAS, ACHIM | AIAA | 1993


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    Full Scale Wind Tunnel Test of a Helicopter Individual Blade Control System

    Jacklin, S. A. / Nguyen, K. / Blass, A. et al. | British Library Conference Proceedings | 1994


    FULL-SCALE WIND TUNNEL TEST OF AN INDIVIDUAL BLADE CONTROL SYSTEM FOR A UH-60 HELICOPTER

    Jacklin, S. A. / Haber, A. / de Simone, G. et al. | British Library Conference Proceedings | 2002


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    Moser, H.H. | Engineering Index Backfile | 1961