The cabin includes a rear compartment including at least one luggage storage area and/or a lavatory, a main compartment including a plurality of seats, and an intermediate compartment. The intermediate compartment includes, on either side of the fuselage, isolation areas, and a central passageway, having a width greater than 50.8 cm. Each isolation area includes a seat and longitudinal partitions delimiting an access opening to the isolation area. Each seat is maneuverable between a retracted seating position for an occupant of the isolation area and an extended lying position of an occupant of the isolation area.
AIRCRAFT CABIN, EXTENDING INTO A FUSELAGE ALONG AN AIRCRAFT AXIS AND ASSOCIATED BUSINESS JET
2021-03-04
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft cabin air distribution system, aircraft and method of feeding air into cabin of fuselage
European Patent Office | 2025
|CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE
European Patent Office | 2025
|CABIN LINING ELEMENT FOR AN AIRCRAFT CABIN AND RIB FOR AN AIRCRAFT FUSELAGE STRUCTURE
European Patent Office | 2021
|Cabin lining element for an aircraft cabin and rib for an aircraft fuselage structure
European Patent Office | 2024
|Aircraft fuselage section, aircraft fuselage and aircraft
European Patent Office | 2023
|