A main rotor blade assembly for a rotary wing aircraft is provided including a main rotor blade root region, a main rotor blade inboard region arranged outboard of said main rotor blade root region, a main rotor blade main region arranged outboard of said main rotor blade inboard region, and a main rotor blade tip region arranged outboard of said main rotor blade main region. At least one of chord, twist, sweep, airfoil shape, and thickness/chord of the main rotor blade assembly has been optimized to achieve balanced high speed forward flight and hover relative to both efficiency and high thrust capability.


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    Titel :

    Dual rotor, rotary wing aircraft


    Beteiligte:
    HUNTER DAVID H (Autor:in) / THOMAS JUSTIN (Autor:in) / BEATTY ROBERT D (Autor:in) / TUOZZO NICHOLAS CHARLES (Autor:in) / EGOLF THOMAS ALAN (Autor:in) / LORBER PETER F (Autor:in) / MOFFITT ROBERT C (Autor:in) / WESTFALL SHAWN (Autor:in)

    Erscheinungsdatum :

    2020-11-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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