A door for an aircraft configured to be selectively closed on a frame, the door comprising a safety system for an anchoring element, the safety system comprising 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, said receptor being optically connected to signalling means, signalling 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
2024-04-04
Patent
Electronic Resource
English
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