A counter-rotating propeller system (14) comprises a cyclic pitch system (60) connected to a first plurality of propeller blades (18) and a variable pitch system (100) connected to a second plurality of propeller blades (20). The first plurality of propeller blades (18) and the second plurality of propeller blades (20) are configured to rotate about a common axis (A).


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    Title :

    Cyclic pitch actuation system for counter-rotating propellers


    Additional title:

    Zyklisches Neigungsbetätigungssystem für gegenläufige Propeller
    Système d'actionnement de pas cyclique pour hélices contrarotatives


    Contributors:

    Publication date :

    2015-08-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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