An aircraft (1) cabin (10) air distribution system with a fuselage (2), a cabin (10) in the fuselage (2), a supply duct (130, 30C, 30, 40), and a plurality of outlets (62) configured to feed air into the cabin (10). The outlets (62) include upper outlets (62) positioned at a higher level than the supply duct (130, 30C, 30, 40), and lower outlets (64) positioned at a lower level than the supply duct (130, 30C, 30, 40). The aircraft (1) cabin (10) air distribution system also includes a plurality of branch ducts (52) configured to feed air from the supply duct (130, 30C, 30, 40) to the outlets (62), wherein each branch duct (52) meets the supply duct (130, 30C, 30, 40) at a respective junction. The branch ducts (52) include upper branch ducts (52) which each feed air to one or more of the upper outlets (62) and lower branch ducts (54) which each feed air to one or more of the lower outlets (64).


    Access

    Download


    Export, share and cite



    Title :

    Aircraft cabin air distribution system


    Publication date :

    2023-12-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    AIRCRAFT CABIN AIR DISTRIBUTION SYSTEM

    KOMARLA SASANK | European Patent Office | 2025

    Free access

    Aircraft cabin air distribution system

    SASANK KOMARLA | European Patent Office | 2025

    Free access

    AIRCRAFT CABIN AIR DISTRIBUTION SYSTEM

    KOMARLA SASANK | European Patent Office | 2025

    Free access


    SYSTEM, AIRCRAFT CABIN AND METHOD FOR MONITORING AN AIRCRAFT CABIN

    VOSS JENS / ROTH FRANZISKA | European Patent Office | 2025

    Free access