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.
TORQUE TUBE ASSEMBLIES FOR USE WITH AIRCRAFT HIGH LIFT DEVICES
DREHMOMENTROHRANORDNUNGEN ZUR VERWENDUNG MIT FLUGZEUGHOCHAUFTRIEBSVORRICHTUNGEN
ENSEMBLES DE TUBE DE TORSION DESTINÉS À ÊTRE UTILISÉS AVEC DES DISPOSITIFS HYPERSUSTENTATEURS D'AÉRONEF
08.12.2021
Patent
Elektronische Ressource
Englisch
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