A main rotor blade assembly with a high negative pitching moment airfoil section having a pitching moment coefficient beyond (more negative than) -0.035 at Mach Numbers below 0.80 and a blade taper of 1:5 or greater.. The main rotor blade preferably limits blade torsional bending and an aft loaded tip airfoils to approximately 'no more' than that of conventional effective rotor blade designs based on conventional tip airfoil sections.


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    Titel :

    ROTOR BLADE ASSEMBLY WITH HIGH PITCHING MOMENT AIRFOIL SECTION FOR A ROTARY WING AIRCRAFT


    Weitere Titelangaben:

    ROTORBLATTANORDNUNG MIT SCHAUFELBLATTPROFIL MIT HOHEM KIPPMOMENT FÜR EINEN DREHFLÜGLER
    ENSEMBLE PALE DE ROTOR AVEC SECTION DE PALE A MOMENT DE FORTE INCLINAISON POUR AERONEF A VOILURE TOURNANTE


    Beteiligte:
    MOFFITT ROBERT C (Autor:in) / DUH JAMES E (Autor:in) / BEREZIN CHARLES (Autor:in)

    Erscheinungsdatum :

    15.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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