A latch (12) is for connecting a panel to a structure, comprising: a bracket (30); a sliding body (32), translationally movable within the bracket; and a hooking arm (34) comprising a hook (74) and connected to the sliding body. The hooking arm is movable relative to the sliding body between an inclined and a parallel conformation. The sliding body can be moved between an unlocking position and a locking position. In the unlocking position, the hooking arm (34) is in an inclined conformation and in a first axial position relative to the bracket. In the locking position, the hooking arm is in the parallel conformation and in a second axial position. In an intermediate position, the hooking arm is in the parallel conformation and in the first axial position.
VERROU À CROCHET POUR PANNEAU D'AÉRONEF
AIRCRAFT PANEL HOOK LATCH
HAKENSCHLOSS FÜR EINE FLUGZEUGPLATTE
2025-01-01
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |