Overhead flow distribution assembly for aircraft cabin

An overhead flow distribution assembly for an aircraft cabin, the assembly comprising:

• a first conduit defining a first plenum having:
• first upper outlets spaced apart from each other along a longitudinal direction of the aircraft;
• first lower outlets spaced apart from each other along the longitudinal direction;
• and
• a first inlet between the first upper outlets and the first lower outlets, wherein the first inlet is defined by at least one opening though a wall of the first conduit extending along the longitudinal direction;
• a first baffle:
• that extends within the first plenum along the longitudinal direction,
• that is disposed between the first upper outlets and the first inlet along a transverse direction normal to the longitudinal direction,
• that has openings defined therethrough, and
• that is configured to restrict airflow from the first inlet toward the first upper outlets;
• a second conduit:
• that is disposed adjacent the first conduit in the longitudinal direction and extends along the longitudinal direction, and
• that defines a second plenum having:
• second upper outlets spaced apart from each other along the longitudinal direction;
• second lower outlets spaced apart from each other along the longitudinal direction;
• and
• a second inlet disposed between the second upper outlets and the second lower outlets and in an end of the second conduit adjacent the first conduit and that defines a fluid communication between the first plenum and the second plenum;
• and
• a second baffle:
• that extends along the longitudinal direction within the second plenum,
• that is disposed between the second upper outlets and at least part of the second inlet along the transverse direction,
• that has openings defined therethrough, and
• that is configured to restrict airflow from the second inlet toward the second upper outlets.