An assembly (26) is provided for an aircraft. This assembly (26) includes a keeper (44), a latch (46), a lock (50) and an electric sensor (102). The latch (46) includes a handle (51) and a hook structure (62) operatively coupled to the handle (51). The hook structure (62) is engaged with the keeper (44) when the handle (51) is in a closed position. The hook structure (62) is disengaged from the keeper (44) when the handle (51) is in an open position. The lock (50) includes a lock element (84) configured to move between a locked position and an unlocked position. The lock (50) is configured to lock the handle (51) in the closed position when the lock element (84) is in the locked position. The lock (50) is configured to unlock the handle (51) from the closed position when the lock element (84) is in the unlocked position. The electronic sensor (102) is configured to provide a signal when the lock element (84) is in one of the locked position or the unlocked position.
AIRCRAFT LATCH ASSEMBLY WITH LOCK SENSOR(S)
FLUGZEUGVERRIEGELUNGSANORDNUNG MIT VERRIEGELUNGSSENSOR(EN)
ENSEMBLE VERROU D'AÉRONEF AVEC CAPTEUR(S) DE VERROUILLAGE
2024-07-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |