A cable cutter assembly (200) for an aircraft (102) hoist is disclosed, and includes an actuator assembly (210) (e.g., at least one pressurized fluid cavity (248), a first outlet port (228), and a solenoid (240) that includes a coil (270) and an armature (290)). The armature (290) is movable between closed and open positions relative to the first outlet port (e.g., via an actuation force), with the armature (290) engaging the first outlet port (228) for the closed position (e.g., a valve seal (304) incorporated by the armature) and being spaced from the first outlet port (228) for the open position. A cutter (326) body (322) includes a cutter body (322) cavity (324) that is fluidly connected with the first outlet port (228). A cutter (326) is movably disposed within the cutter body cavity (324). Disposing the armature (290) in the open position (e.g., via energizing the coil) fluidly connects the pressurized fluid cavity (248) with the cutter body cavity (324) to move the cutter (326) in a cable (106, 360) cutting direction.


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    Titel :

    ELECTRO-PNEUMATIC CABLE CUTTER ASSEMBLY FOR AIRCRAFT HOIST


    Weitere Titelangaben:

    ELEKTROPNEUMATISCHE KABELSCHNEIDANORDNUNG FÜR FLUGZEUGHEBEZEUG
    ENSEMBLE COUPE-CÂBLE ÉLECTRO-PNEUMATIQUE POUR TREUIL D'AÉRONEF


    Beteiligte:
    MAHESHWARAPPA RAMESH (Autor:in) / JOHN POLY (Autor:in)

    Erscheinungsdatum :

    23.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B23D Hobeln , PLANING / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B66C Krane , CRANES / B66D Haspeln , CAPSTANS



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