A helicopter (100) has a fuselage (102), a main rotor system (110) connected to the fuselage (102) and configured to rotate in a rotor direction, the main rotor system (110) comprising a retreating rotor blade side and an opposing advancing rotor blade side, and a first wing (106) extending from the fuselage (102) on the retreating rotor blade side. The helicopter comprises no tail rotor system and comprises no counterrotating rotor system coaxial with the main rotor system (110).


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    Title :

    HELICOPTER WITH WING AUGMENTED LIFT


    Additional title:

    HUBSCHRAUBER MIT FLÜGELN FÜR ERHÖHTEN AUFTRIEB
    HÉLICOPTÈRE DOTÉ D'UNE AILE POUR PORTANCE AUGMENTÉ


    Contributors:

    Publication date :

    2019-06-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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