Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.

    L'invention concerne des systèmes et des procédés de commande de pas d'aéronef. Un système de commande de pas d'aéronef (28) comprend un stabilisateur horizontal mobile (24) et un élévateur (26) couplé de façon mobile au stabilisateur horizontal. L'élévateur est couplé électroniquement au stabilisateur horizontal.


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    Title :

    AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR


    Additional title:

    SYSTEME DE COMMANDE DE PAS D'AERONEF AVEC ELEVATEUR A ENGRENAGE ELECTRONIQUE


    Contributors:

    Publication date :

    2017-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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