A rotorcraft rotor blade (400) assembly includes a stub spar (402) extending less than a full span of the rotor blade assembly (400). An upper skin portion (404) extends substantially the full span of the rotor blade assembly (400). A lower skin portion (406) extends substantially the full span of the rotor blade assembly (400). The stub spar (402) is positioned between the upper skin portion (404) and the lower skin portion (406).


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    Title :

    ROTORCRAFT ROTOR BLADE ASSEMBLY


    Additional title:

    ROTORBLATTANORDNUNG EINES DREHFLÜGELFLUGZEUGS
    ENSEMBLE PALE DE ROTOR D'UN GIRAVION


    Contributors:

    Publication date :

    2018-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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