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.


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    Titel :

    Aircraft pitch control system with electronically geared elevator


    Beteiligte:
    AHN THOMAS (Autor:in) / TANNER CLINTON ERIC (Autor:in) / NELSON THOMAS (Autor:in) / BLACK SCOTT (Autor:in)

    Erscheinungsdatum :

    25.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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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