Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft

1. A method for controlling a temperature of feed air to be injected into at least one cabin zone of a cabin of a passenger aircraft, the method comprising:

independently controlling the temperature of the feed air injected into the at least one cabin zone dependent upon a deviation of an injection temperature actual value of the feed air, measured by an injection temperature sensor, from an injection temperature target value; and

establishing the injection temperature target value required to maintain a set ambient temperature in the at least one cabin zone on the basis of the following conditions operated simultaneously by a control unit:

using an external ambient temperature actual value of an external surrounds outside of the passenger aircraft, measured by an external ambient temperature sensor,

without using a cabin zone ambient temperature actual value of the at least one cabin zone, thereby not requiring any output from an ambient temperature sensor in the at least one cabin zone; wherein the injection temperature target value for the at least one cabin zone is also established on the basis of a first correction value for the at least one cabin zone, and wherein the first correction value for the at least one cabin zone is constant and based on the physical zone-specific factors of the at least one cabin zone affecting heat transfer.

2. The method of claim 1 , wherein the injection temperature target value for the at least one cabin zone is also established on the basis of a second correction value for the at least one cabin zone, the second correction value being based on an ambient temperature target value for the at least one cabin zone, wherein the ambient temperature target value can be entered manually.

3. The method of claim 1 , wherein the cabin is divided into a plurality of cabin zones each receiving feed air, and the method further comprises:

independently controlling the temperature of the feed air injected into each of the plurality of cabin zones dependent upon a deviation of an injection temperature actual value of the feed air for each cabin zone, measured by an injection temperature sensor, from an injection temperature target value for each cabin zone; and

establishing the injection temperature target value for each of the plurality of cabin zones on the basis of an external ambient temperature actual value of an external surrounds outside of the passenger aircraft, measured by an external ambient temperature sensor, and without using a cabin zone ambient temperature actual value of any of the plurality of cabin zones.

4. The method of claim 1 , wherein the at least one cabin zone does not include an operating ambient temperature sensor such that the injection temperature target value for the at least one cabin zone cannot be established based on output from an ambient temperature sensor in the at least one cabin zone.

5. A passenger aircraft, comprising:

a cabin including at least one cabin zone configured to be supplied with injected temperature regulated feed air; and

an electronic control unit arranged to independently control, for the at least one cabin zone, a temperature of the injected feed air that is injected into the at least one cabin zone dependent upon a deviation of an injection temperature actual value, measured by an injection temperature sensor, in relation to an injection temperature target value for the at least one cabin zone,

wherein the electronic control unit establishes the injection temperature target value required to maintain a set ambient temperature in the at least one cabin zone on the basis of the following conditions operated simultaneously by the control unit:

using an external ambient temperature actual value of an external surrounds outside of the passenger aircraft, measured by an external ambient temperature sensor,

without using a cabin zone ambient temperature actual value of the at least one cabin zone, thereby not requiring any output from an ambient temperature sensor in the at least one cabin zone, wherein the injection temperature target value for the at least one cabin zone is also established on the basis of a first correction value for the at least one cabin zone; and wherein the first correction value for the at least one cabin zone is constant and based on the physical zone-specific factors of the at least one cabin zone affecting heat transfer.

6. The passenger aircraft of claim 5 , wherein the injection temperature target value for the at least one cabin zone is also established on the basis of a second correction value for the at least one cabin zone, the second correction value being based on an ambient temperature target value for the at least one cabin zone, wherein the ambient temperature target value can be entered manually.

7. The passenger aircraft of claim 5 , wherein the cabin is divided into a plurality of cabin zones each receiving injected feed air, and the electronic control unit is arranged to independently control the temperature of the feed air injected into each of the plurality of cabin zones dependent upon a deviation of an injection temperature actual value of the feed air for each cabin zone, measured by an injection temperature sensor, from an injection temperature target value for each cabin zone, and

wherein the electronic control unit establishes the injection temperature target value for each of the plurality of cabin zones on the basis of an external ambient temperature actual value of an external surrounds outside of the passenger aircraft, measured by an external ambient temperature sensor, and without using a cabin zone ambient temperature actual value of any of the plurality of cabin zones.

8. The passenger aircraft of claim 5 , wherein the at least one cabin zone does not include an operating ambient temperature sensor such that the injection temperature target value for the at least one cabin zone cannot be established based on output from an ambient temperature sensor in the at least one cabin zone.