Example torque tube assemblies (200) for use with aircraft high lift devices (108, 110, 112, 114) are described herein. An example torque tube assembly (200) includes a torque tube (304) having a first end (302) and a second end (208) opposite the first end. A first fitting (400) is coupled to the first end (302) and a second fitting (800) is coupled to the second end (308). The first fitting (400) is to be coupled to a first high lift device of an aircraft. The second fitting (800) has a spline section (910, 912). The torque tube assembly (200) also includes a sliding spline shaft (894) having a channel (902) and a first yoke (810). The second fitting (800) is slidably received within the channel (902). The torque tube assembly (200) further includes a spline coupling (802) having a second yoke (812), which is coupled to the first yoke (810) of the sliding spline (804) shaft to form a U-joint (806). The spline coupling (808) is to be coupled to a second high lift device of the aircraft. 00 0 CN CN 0 00 c)- 00 C'14 N -, C'14 C'14 C'14 (0 -*Z T oo (0 CN T- CN


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    Title :

    Torque tube assemblies for use with aircraft high lift devices


    Contributors:

    Publication date :

    2024-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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