A hook system (200) has a mount (202) and a sacrificial connector (204) that is selectively attached to the mount (202) and is configured for attachment to a hook (206). The mount (202) includes a first sidewall (210) comprising a first concave profile (216) on a side of the first sidewall (210), a second sidewall (212) laterally offset in a fixed location relative to the first sidewall (210) and defining a channel (214) therebetween, the second sidewall (212) having a second concave profile (216) on a side of the second sidewall (212). The hook system (200) also has a first pin structure (222), such as a bolt having a head (224), extending between the first sidewall (210) and the second sidewall (212). The connector (204) has a third concave profile (228), the third concave profile (228) being configured to receive the first pin structure (222) therein. The hook system (200) also includes a second pin structure (234), such as a bolt having a head (236), extending through the connector (204), wherein each of the first concave profile (216) and the second concave profile (216) are configured to receive the second pin structure (234) therein. The connector (204) is configured to be at least partially received within the channel (214).


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    Titel :

    HOOK SYSTEM


    Weitere Titelangaben:

    HAKENSYSTEM
    SYSTÈME DE CROCHET


    Beteiligte:
    DUVAL SEBASTIEN (Autor:in) / OUELLET MARC (Autor:in)

    Erscheinungsdatum :

    17.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B66C Krane , CRANES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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