Conditioned air supply method and supply system for aircraft
View Patent ↗When conditioned air is supplied in an aircraft, the conditioned air in which at least one of oxygen concentration and humidity is adjusted is generated in the aircraft. The generated conditioned air is blown via a plurality of air blow-off ports 40 a disposed inside the aircraft cabin so that the conditioned air reaches face disposition regions of passengers H in a plurality of seat locations inside the cabin.
1. A conditioned air supply system for an aircraft, comprising:
an oxygen-enriched air generator that generates oxygen-enriched air as conditioned air in said aircraft;
a measurement device that measures a pressure inside a cabin of said aircraft; a storage device that stores a preset relationship between a pressure inside said cabin and a target partial pressure; said relationship being set so that said target partial pressure exceeds a value obtained by multiplying the pressure inside said cabin by an oxygen concentration ratio in the air on the earth's surface and is equal to or less than an oxygen partial pressure in the air on the earth's surface;
a target partial pressure determination device that finds said target partial pressure on the basis of said relationship and the measured pressure inside said cabin;
a control device that controls said oxygen-enriched air generator so that an oxygen partial pressure of the generated conditioned air becomes said target partial pressure;
a piping having a plurality of air blow-off ports connected to said oxygen-enriched air generator; said air blow-off ports being disposed in locations in which said conditioned air can be blown so as to reach respective face disposition regions of passengers in a plurality of seat locations inside said cabin; and
a mixing chamber that introduces a flow of air having oxygen concentration lower than the oxygen concentration of the conditioned air to areas of the cabin other than the face disposition regions of the cabin where the conditioned air is blown.
2. The conditioned air supply system for an aircraft according to claim 1 , wherein said piping has a plurality of branching ends, and said branching ends are configured by a plurality of ducts, each duct being attached to each of a plurality of seats or to a fuselage of said aircraft, said air blow-off port is provided in each duct, and each duct can change a posture thereof between a usage posture in which said conditioned air is blown from said air blow-off port so as to reach said face disposition region and a withdrawal posture in which it is disposed in a region that does not interfere with a movement region of a passenger inside said cabin.
3. The conditioned air supply system for an aircraft according to claim 1 , further comprising: a mask that is attachable to a passenger face; a flexible tube connected to said mask; and said tube being detachably attached to said piping, wherein said conditioned air introduced from said air blow-off port into said tube attached to said piping is supplied to the passenger via said mask.
4. The conditioned air supply system for an aircraft according to claim 1 , wherein said piping has a plurality of nozzles, each nozzle being attached to each of a plurality of seats or to a fuselage of said aircraft, said air blow-off port and an auxiliary air blow-off port are provided in each nozzle, in each nozzle, said auxiliary air blow-off port is disposed in a location in which said conditioned air is blown toward a region separated from said face disposition region, and each nozzle is provided with a mechanism for adjusting a blow-off flow rate of said conditioned air so that the blow-off flow rate of said conditioned air from said auxiliary air blow-off port decreases when the blow-off flow rate of said conditioned air from said air blow-off port increases, and the blow-off flow rate of said conditioned air from said auxiliary air blow-off port increases when the blow-off flow rate of said conditioned air from said air blow-off port decreases.
5. The conditioned air supply system for an aircraft according to claim 1 , wherein said oxygen-enriched air generator comprises a selectively permeable membrane that separates high-pressure air supplied from a high-pressure air supply source into oxygen-enriched air and nitrogen-enriched air, a conditioning chamber into which the oxygen-enriched air separated by said selectively permeable membrane and air whose oxygen concentration is lower than that of the oxygen-enriched air separated by said selectively permeable membrane are introduced, and a flow rate control valve for the oxygen-enriched air introduced into said conditioning chamber, and a moisture regenerator that recovers moisture contained in the air discharged from said cabin and humidifies the air inside said conditioning chamber with the recovered moisture is provided.
6. The conditioned air supply system for an aircraft according to claim 5 , wherein an oxygen partial pressure determination device that finds an oxygen partial pressure of the oxygen-enriched air introduced from said conditioning chamber into said piping is provided, and an opening degree of said flow rate control valve is adjusted by said control device so as to reduce a difference between said found target partial pressure and said found oxygen partial pressure.
7. The conditioned air supply system for an aircraft according to claim 6 , wherein:
a part of the air supplied from said high-pressure air supply source is introduced into said mixing chamber, and
a part of the air flowed out from said cabin returns into said cabin via said mixing chamber.
8. The conditioned air supply system for an aircraft according to claim 5 , wherein:
a part of the air supplied from said high-pressure air supply source is introduced into said mixing chamber, and
a part of the air flowed out from said cabin returns into said cabin via said mixing chamber.