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An interlock assembly for an aircraft door includes a shaft, an interlock first portion, and an auto-disarm second portion. The shaft is rotatable about the second rotational axis between an armed position and a disarmed position. The shaft includes an interlock cam and an auto-disarming cam. In a first interlock position, the interlock first portion permits rotation of the shaft between the armed position and the disarmed position. In a second interlock position, the interlock first portion prevents rotation of the shaft from the disarmed position to the armed position. In a first auto-disarm position, the auto-disarm second portion permits rotation of the shaft between the armed position and the disarmed position. In a second auto-disarm position, the auto-disarm second portion prevents rotation of the shaft from the disarmed position to the armed position.
An interlock assembly for an aircraft door includes a shaft, an interlock first portion, and an auto-disarm second portion. The shaft is rotatable about the second rotational axis between an armed position and a disarmed position. The shaft includes an interlock cam and an auto-disarming cam. In a first interlock position, the interlock first portion permits rotation of the shaft between the armed position and the disarmed position. In a second interlock position, the interlock first portion prevents rotation of the shaft from the disarmed position to the armed position. In a first auto-disarm position, the auto-disarm second portion permits rotation of the shaft between the armed position and the disarmed position. In a second auto-disarm position, the auto-disarm second portion prevents rotation of the shaft from the disarmed position to the armed position.
INTERLOCK ASSEMBLY FOR AN AIRCRAFT DOOR
BUCHET DAMIEN (author)
2024-07-25
Patent
Electronic Resource
English