Patent ID: 6761337
Filing Date: 2004-07-13
Classification: B64D,Y10S

Abstract:
Fast aircraft evacuation device comprising a structure with one wall that delimits a passenger cabin, said wall comprising an inner wall portion and a fuselage wall portion, at least one opening formed in said fuselage wall portion and an access door that can close the said opening, the fast evacuation device comprising a housing provided in the said structure close to the door, an inflatable slide placed in the housing, a hatch closing the housing on the outside of the aircraft, means of arming-disarming the slide and means for controlling automatic opening of the hatch when the door is opened when the arming-disarming means are in the armed state, characterised in that the housing is located in a pressurised area inside the aircraft, said pressurized area being separated from the cabin by said inner wall portion.