Example torque tube assemblies for use with aircraft high lift devices are described herein. An example torque tube assembly (200) includes a torque tube (304) having a first end (302) and a second end (308) opposite the first end. A first fitting is coupled to the first end and a second fitting is coupled to the second end. The first fitting is to be coupled to a first high lift device of an aircraft. The second fitting (800) has a spline section (910). The torque tube assembly also includes a sliding spline shaft (804) having a channel (902) and a first yoke (810). The second fitting (800) is slidably received within the channel (902). The torque tube assembly further includes a spline coupling (808) having a second yoke (812), which is coupled to the first yoke (810) of the sliding spline shaft (804) to form a U-joint (806). The spline coupling (808) is to be coupled to a second high lift device of the aircraft.


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    Titel :

    TORQUE TUBE ASSEMBLIES FOR USE WITH AIRCRAFT HIGH LIFT DEVICES


    Weitere Titelangaben:

    DREHMOMENTROHRANORDNUNGEN ZUR VERWENDUNG MIT FLUGZEUGHOCHAUFTRIEBSVORRICHTUNGEN
    ENSEMBLES DE TUBE DE TORSION DESTINÉS À ÊTRE UTILISÉS AVEC DES DISPOSITIFS HYPERSUSTENTATEURS D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    08.12.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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