Air conditioning arrangement for an aircraft with a plurality of climate zones that may be individually temperature-controlled
View Patent ↗An air conditioning arrangement for an aircraft with a plurality of climate zones that may be individually temperature-controlled includes a main branching system having an air supply feed path system with a mixing chamber and a plurality of sub-branching systems branching from the mixing chamber and leading to one of the climate zones in each case. Basic temperature control means are used for controlling the temperature of the air supply in the mixing chamber. Individual temperature-control means are used on the other hand for individually controlling the temperature of the air supply in each of the sub-branching systems as a function of a desired temperature value of the respective climate zone. Basic temperature control of the air supply in the mixing chamber preferably takes place independently of a temperature requirement of the climate zone with associated combined heat and power engine.
1. An air conditioning arrangement for an aircraft or other premises with a plurality of climate zones that may be individually temperature-controlled, comprising:
an air supply feed path system with a mixing chamber and a plurality of sub-branching systems branching off from the mixing chamber and leading to one of the climate zones in each case,
basic temperature control means for controlling the temperature of the air supply in the mixing chamber as a function of at least one desired temperature value, and
individual temperature-control means for individually controlling the temperature of the air supply in each of the sub-branching systems as a function of a desired temperature value of the respective climate zone, wherein the individual temperature-control means, in allocation to only a partial number of the climate zones, comprise at least one combined heat and power engine operating according to a thermodynamic cyclic process,
wherein the basic temperature-control means control the temperature of the air supply in the mixing chamber (i) as a function of a desired temperature value of at least one climate zone that is not associated with a combined heat and power engine, but (ii) independently and not as a function of a desired temperature value of at least one climate zone that is associated with a combined heat and power engine.
2. The air conditioning arrangement according to claim 1 , wherein the combined heat and power engine is a Stirling engine.
3. The air conditioning arrangement according to claim 1 , wherein the combined heat and power engine is in driving connection or can be brought into driving connection with a drive motor configured for operation in opposed directions of rotation and which is controlled by a control arrangement set up to reverse the direction of rotation of the drive motor, wherein the combined heat and power engine with a useful heat exchange surface is arranged in an air conduit system which in opposed directions of flow allows a moderating air flow via the useful heat exchange surface toward the sub-branching system of the relevant climate zone.
4. The air conditioning arrangement according to claim 1 , wherein a moderating air stream conveyed via a useful heat exchange surface of the combined heat and power engine and which is to be introduced into the associated sub-branching system of the relevant climate zone is fed from the air supply conveyed in this sub-branching.
5. The air conditioning arrangement according claim 1 , wherein a moderating air stream conveyed via a useful heat exchange surface of the combined heat and power engine and which is to be introduced into the associated sub-branching system of the relevant climate zone, or the thermal energy thereof, is taken from an outgoing air region of the aircraft.
6. The air conditioning arrangement according to claim 1 , wherein the basic temperature-control means control the temperature of the air supply in the mixing chamber (i) as a function of a desired temperature value of each climate zone that is not associated with a combined heat and power engine, but (ii) independently and not as a function of a desired temperature value of each climate zone that is associated with a combined heat and power engine.
7. The air conditioning arrangement according to claim 1 , wherein associated with the combined heat and power engine is a fan arrangement which generates or boosts a moderating air flow conveyed via a useful heat exchange surface of the engine and which is to be introduced into the associated sub-branching system of the relevant climate zone.
8. The air conditioning arrangement according to claim 7 , wherein, in the flow direction of the moderating air flow on either side of the combined heat and power engine, the fan arrangement comprises at least one respective fan.
9. The air conditioning arrangement according to claim 7 , wherein, in the flow direction of the moderating air flow on just one side of the combined heat and power engine, the fan arrangement comprises a fan.
10. The air conditioning arrangement according to claim 7 , wherein at least one fan of the fan arrangement is in driving connection or can be brought into driving connection with a drive motor configured for operation in opposed directions of rotation and which is controlled by a control arrangement set up to reverse the direction of rotation of the drive motor.