A hook body (330) for a latch mechanism includes a plurality of longitudinal members (331, 333), each of the plurality of longitudinal members extending in a longitudinal direction with respect to the hook body (330); and a load slot (340) at a proximal end (341) of the hook body (330), the load slot (340) having a loading portion (350) and a receiving portion (354), the receiving portion (354) configured to receive a transverse rod of a T-bolt and the loading portion (350) configured to apply a load to the transverse rod upon translation of the hook body (330) away from the transverse rod..


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    Title :

    AIRCRAFT SAFETY LATCH


    Additional title:

    FLUGZEUGSICHERHEITSVERRIEGELUNG
    VERROU DE SÉCURITÉ POUR AÉRONEF


    Contributors:

    Publication date :

    2023-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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