An aircraft catcher bracket comprises a mounting section (24, figure 2), a C-shaped bracket body 22, with first and second ends separated by a gap, and a first gate 26 mounted to the first end of the bracket body by a first pivot 28, which can rotate about the pivot between a closed position where the first gate bridges the gap to form a ring for retaining a shaft 6, and an open position where the first gate is displaced within the bracket body to form an opening for receiving a shaft into the catcher bracket. Preferably the shaft is a drive shaft for driving aircraft wing components such as leading edge slats.


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    Titel :

    Aircraft catcher bracket


    Beteiligte:

    Erscheinungsdatum :

    10.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16L PIPES , Rohre / B64C AEROPLANES , Flugzeuge



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