A door for an aircraft is configured to be selectively closed on a frame. The door includes a safety system for an anchoring element. The safety system includes a source of light radiations and a receptor of said radiations, the source being integral with the door and the receptor being integral with the anchoring element. The receptor is optically connected to signalling apparatus that signals the positioning of the anchoring element in the second operating condition when the receptor receives the light radiation from the source.
Door for a vehicle provided with an improved security system
26.11.2024
Patent
Elektronische Ressource
Englisch
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