Pitch controller for helicopter rotors uses hub-mounted actuators located symmetrically between rotor blades. New controller designed for X-wing rotors requiring collective pitch control; pitch of all blades must be changed by same amount. Collective control allows rotor trimmed during variety of flight regimes, particularly during hovering and fixed-wing flight.


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    Titel :

    Pitch Control for Helicopter Rotors


    Beteiligte:
    Jeffery, P. (Autor:in) / Luecke, G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1986-11-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Jet-propelled helicopter rotors

    Klemin, A. | Engineering Index Backfile | 1949


    Application of Circulation Control to Helicopter Rotors

    R.N. GREENMAN / M.G. GAFFNEY | NTIS | 1957


    Unsteady Aerodynamics of Helicopter Rotors

    W. P. Jones / W. J. McCroskey / J. J. Costes | NTIS | 1972


    Unsteady aerodynamics of helicopter rotors

    Jones, W. P. / McCroskey, W. J. / Costes, J. J. | TIBKAT | 1972


    Smooth pitch control for propellers and rotors

    HINKS WILLIAM L | Europäisches Patentamt | 2019

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