Patent ID: 8539787

Claim:
An aircraft with an air-conditioning system, comprising: an aircraft cabin having a plurality of regions and a plurality of seats, including a first region that surrounds a first seat, the first seat sized to accommodate a seated passenger; at least one heat transfer device configured as a heat exchanger, which is associated with and cools the first region, and to which is fed a coolant circulating in a cooling circuit of a cooling system, wherein the coolant of the cooling system is always in a liquid state in the cooling circuit; a central air-conditioning system operatively connected to the heat exchanger and supplying air to the heat exchanger, wherein the coolant in heat exchanger cools the air, and the air leaving the heat exchanger flows into the aircraft cabin; a first seat feed line located within the first seat and connected to the central air-conditioning system, the first seat feed line discharging air from the central air-conditioning system into the first region; and a heating device that heats the air flowing into the first region, the heating device and the heat exchanger each being located within the first seat feed line, wherein a temperature of the discharged air and or an amount of discharged air is configured to be individually adjusted for the first region.