Example torque tube assemblies for use with aircraft high lift devices are described herein. An example apparatus includes a spline coupling (404) having a first yoke, a sliding splined shaft (804) having a second yoke and a torque tube (304) having a first end (302) and a second end (308) opposite the first end. A first fitting with a third yoke is coupled to the first end of the torque tube, and a second fitting with a fourth yoke is coupled to the second end of the torque tube. The third yoke is coupled to the first yoke to form a first U-joint (300), and the fourth yoke is coupled to the second yoke to form a second U-joint (306). The spline coupling is to be coupled to a first high lift device drive shaft and the sliding splined shaft is to be coupled to a second high lift device drive shaft.


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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 :

    15.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge / F16C SHAFTS , Wellen



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