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A latching mechanism for an aircraft galley, the aircraft galley comprising a door and a frame, the latching mechanism comprising: a latch bolt movable between a retracted position and an extended position; and an actuator configured to maintain the latch bolt in the retracted position, the actuator configured to move the latch bolt to the extended position on closing the door in the frame, wherein the latch bolt is receivable by a latch striker to latch the aircraft galley door when the door is closed and the latch bolt is in the extended position.
A latching mechanism for an aircraft galley, the aircraft galley comprising a door and a frame, the latching mechanism comprising: a latch bolt movable between a retracted position and an extended position; and an actuator configured to maintain the latch bolt in the retracted position, the actuator configured to move the latch bolt to the extended position on closing the door in the frame, wherein the latch bolt is receivable by a latch striker to latch the aircraft galley door when the door is closed and the latch bolt is in the extended position.
LATCHING MECHANISM
VERRIEGELUNGSMECHANISMUS
MÉCANISME DE VERROUILLAGE
KESKIN VOLKAN (author)
2025-02-26
Patent
Electronic Resource
English