Individual temperature-control of aircraft cabin regions by heating and evaporative cooling

Patent metadata

Field	Value
Publication number	US-9540111-B2
Application number	US-81283109-A
Country	US
Kind code	B2
Filing date	Jan 12, 2009
Priority date	Jan 16, 2008
Publication date	Jan 10, 2017
Grant date	Jan 10, 2017

Abstract

An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of an aircraft includes a central air conditioning device, which provides a pressurized and temperature-controlled central air flow. A part of the central air flow is supplied to a first cabin region. Another part of the central air flow is heated in a heating device or cooled in a cooling device and supplied to another cabin region. Water evaporates in the cooling device, in order to cool the air flow to be supplied to the cabin region.

First claim

What is claimed is:

1. An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of the aircraft, comprising:
a central air conditioning device which is designed to provide a central air flow having, in flight, a pressure lying above the air pressure outside the cabin and an actual temperature, wherein the central air conditioning device is supplied with an air flow comprising engine bleed air and/or air recirculated from the cabin of the aircraft;
a first supply line, which is designed to supply a part of the central air flow into the cabin, wherein the cabin includes a first temperature sensor for measuring the temperature in the cabin;
at least one branch line, which is designed to supply another part of the central air flow to further cabin regions, each of which is to be individually air conditioned and constitutes the environment of a respective seat in the cabin, wherein each environment of a seat is provided with a temperature sensor for measuring the actual temperature of the environment of the seat;
a cooling device which is connected to the central air conditioning device via the branch line, wherein the cooling device cools the air flow in the at least one branch line if the actual temperature of the air flow in the branch line is higher than a desired temperature of an air flow to be supplied to the respective environment of a seat, the cooling device being designed, for the cooling, to evaporate water into the air flow to be supplied to the respective further environment of a seat; and
a plurality of heating devices which heat the air flow in the at least one branch line if the actual temperature of the air flow is lower than the desired temperature of the air flow to be supplied to the respective environment of a seat,
wherein the at least one branch line supplies a part of the central air flow provided by the central air conditioning device to the cooling device,
wherein the cooling device is connected to a plurality of distributing lines which divide the air flow leaving the cooling device,
wherein each of the distributing lines is connected to a respective one of the plurality of heating devices, to supply a respective divided air flow to the heating device,
wherein at least one supply line is connected to the heating device, which supply line supplies the air flow to a respective environment of a seat, and
wherein a control device is configured to control the central air conditioning device, the cooling device, and at least one of the plurality of heating devices in such a manner that the total energy consumption of the air conditioning system is minimal, wherein the control device compares the actual temperatures of the environments of the seats with the desired temperatures of the environments of the seats and calculates therefrom the desired temperature of the air flow to be supplied to the environment of the respective seat.

2. The air conditioning system according to claim 1 , further comprising a control device which is designed to control the cooling device, based on a measured actual temperature, in such a manner that the air flow in the at least one branch line is cooled to the desired temperature of the air flow to be supplied to the respective region.

3. The air conditioning system according to claim 1 , wherein a control device controls the central air conditioning device in such a manner that the air delivered by the control device has an actual temperature which corresponds to the desired temperature of the cabin region requiring the greatest air volume flow.

4. The air conditioning system according to claim 1 , wherein the cooling device sprays water into the air flow, nebulizes water into the air flow by ultrasound and/or atomizes water into the air flow by compressed air.

5. The air conditioning system according to claim 1 , wherein the cooling device is designed in such a manner that the air flow to be supplied to the cabin region passes through a bubble column.

6. The air conditioning system according to claim 1 , wherein the cooling device is designed in such a manner that water contained in a porous material evaporates into the air flow and/or water on a body with a large surface.

7. The air conditioning system according to claim 1 , wherein the cooling device is designed in such a manner that water evaporates into the air flow on a membrane.

8. A method for the individual air conditioning of a region of a cabin of an aircraft, comprising:
providing an air flow by means of a central air conditioning device which, in flight, is pressurized to a pressure which is higher than the air pressure outside the cabin;
temperature-controlling the pressurized air flow to an actual temperature;
supplying the temperature-controlled air flow at the actual temperature to the cabin;
providing the temperature-controlled air flow at the actual temperature to further cabin regions, each of which is to be individually air conditioned and constitutes the environment of a respective seat in the cabin, wherein each environment of a seat is provided with a temperature sensor for measuring the actual temperature of the environment of a seat;
providing at least one cooling device with the temperature-controlled air flow of the central air conditioning device via a branch line;
cooling the temperature-controlled air flow provided to the further environments of a seat, via a cooling device, by evaporating water before an air flow is supplied to the respective environment of a seat if a desired temperature of the air flow to be supplied to the respective environment of a seat is lower than the actual temperature;
heating, via at least one heating device, the air flow provided to the further environments of a seat before the air flow is supplied to the respective environments of seats if the desired temperature of the air flow to be supplied to the respective environment of a seat is higher than the actual temperature;
cooling the temperature-controlled air flow at the actual temperature, which is supplied to the environments of seats, to the lowest desired temperature of all the desired temperatures of the further environments of seats;
dividing the air flow at the desired temperature into a plurality of air flows which are assigned to a respective environment of a seat;
heating the divided air flows to be supplied to the respective environments of seats to the respective desired temperature if the desired temperature of the air flow to be supplied to the respective environment of a seat is higher than the lowest desired temperature of all the desired temperatures of the further zones; and
controlling, by means of a control device, the central air conditioning device, the cooling device, and the at least one heating device in such a manner that the total energy consumption of the air conditioning system is minimal.

9. The method according to claim 8 , further comprising:
controlling the cooling of the air flow supplied to the respective environment of a seat, based on a measured actual temperature, in such a manner that this air flow enters this environment of a sea at the desired temperature of the air flow to be supplied to this environment of a seat.

10. The method according to claim 8 , further comprising:
removing air from the cabin to which the air flow is to be supplied, the removed air flow being cooled before it is supplied to the cabin again.

11. An air conditioning system for an aircraft for the individual air conditioning of regions of a cabin of the aircraft, comprising:
a central air conditioning device which is designed to provide a central air flow having, in flight, a pressure lying above the air pressure outsid

Assignees

• Dittmar Jan
• Schumacher Christian
• Airbus Operations Gmbh

Inventors

• Dittmar Jan
• Schumacher Christian

Classifications

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• B64D2013/0662

  with humidity control · CPC title

• B64D2013/0674

  comprising liquid subsystems · CPC title

• B64D11/0626

  with individual temperature or ventilation control · CPC title

• Y02T50/56

  Cross-Sectional Technologies · mapped topic