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..
AIRCRAFT SAFETY LATCH
FLUGZEUGSICHERHEITSVERRIEGELUNG
VERROU DE SÉCURITÉ POUR AÉRONEF
17.05.2023
Patent
Elektronische Ressource
Englisch
IPC: | E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES |