A vehicle control surface, such as an aircraft horizontal stabilizer, is hydraulically controlled using solenoid operated valves (SOVs) controlling directional control valves and/or rate control valves with small numbers of ports, e.g. a four port three position directional control value and/or a four port two position rate control valve.


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    Titel :

    Horizontal stabilizer trim actuator systems and methods


    Beteiligte:
    JOSEPH DEREK M (Autor:in) / ECK KEVIN B (Autor:in) / FEET CHRISTOPHER D (Autor:in) / MESHESHA YONAS T (Autor:in) / SODERQUIST TIMOTHY J (Autor:in) / HANCE BARRY D (Autor:in)

    Erscheinungsdatum :

    2022-02-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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