An apparatus is provided for an aircraft. This apparatus includes a latch (46). The latch (46) includes a handle (58), a hook structure (60) and a linkage system (62) operatively coupling the handle (58) to the hook structure (60). The linkage system (62) includes a back link (108), a center link (110), a back link pivot member (114) and a center link pivot member (116). The hook structure (60) includes a hook (72), a structure aperture (100) and a structure slot (102) located longitudinally between the hook (72) and the structure aperture (100). The back link (108) is pivotally coupled to the center link (110). The back link pivot member (114) is received within the structure aperture (100) and pivotally couples the back link (108) to the hook structure (60). The center link pivot member (116) is received within the structure slot (102) and pivotally couples the handle (58) and the center link (110) together and to the hook structure (60).
LONG THROW LATCH FOR AIRCRAFT SYSTEM
VERRIEGELUNG FÜR LANGE WURFWINKEL EINES FLUGZEUGSYSTEMS
VERROU À LONGUE PORTÉE POUR SYSTÈME D'AÉRONEF
2025-03-19
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |