An aeroplane includes an external skin and an internal bulkhead delimiting a cabin, and an escape opening passing through the external skin and the internal bulkhead. The escape opening is closed off by an external escape hatch disposed flush with the external skin. The aeroplane also includes an internal escape hatch that closes off the escape opening disposed flush with the internal bulkhead, and pressure regulating means capable of automatically triggering an opening of the internal escape hatch or a part of the internal escape hatch when a pressure differential on both sides of the internal escape hatch exceeds a determined value.
AVION EQUIPE D'UNE TRAPPE INTERIEURE D'EVACUATION INTEGRANT UN SYSTEME DE REGULATION DE PRESSION
2016-07-01
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
AVION EQUIPE D'UNE TRAPPE INTERIEURE D'EVACUATION AVEC UNE DOUBLE COMMANDE D'OUVERTURE
European Patent Office | 2016
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