An integrated three function valve (ITFV) for an actuator of a flight control surface. The ITFV includes: an inner spool configured to be actuated in a first direction and a second direction responsive to a pressure differential acting across the inner spool; and an intermediate spool configured to be actuated in the first direction and second direction between an active position and a bypass position. The inner spool is located within the intermediate spool.


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    Titel :

    HYDRAULIC VALVE


    Beteiligte:
    MORNACCHI ANDREA (Autor:in) / MOLINELLI DARIO (Autor:in) / SAVINO DARIO (Autor:in) / QUAGLIA ENRICO (Autor:in) / ROMBOLA' FEDERICO (Autor:in)

    Erscheinungsdatum :

    03.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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