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


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    Title :

    Aircraft safety latch


    Contributors:

    Publication date :

    2025-07-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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