Systems, devices, and methods are provided for a locking apparatus. A locking apparatus can be configured to operably attach a fixed-wing of an aircraft to a body of the aircraft. The locking apparatus can include a first connector configured to releasably receive a first tube, a second connector having a first side and second side, the first side configured to receive a second tube and the second side configured to releasably receive the first connector, and an end coupling cap configured to releasably lock the first connector and second connector together.


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    Title :

    Aircraft tail lock


    Contributors:

    Publication date :

    2024-09-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16L PIPES , Rohre / B64C AEROPLANES , Flugzeuge



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