Method for isolating a cabin wall of an aircraft or for cooling or heating of cabin air and a cabin wall suitable therefore
View Patent ↗The present invention relates to a method for insulating an aircraft cabin 6 and for the cooling or heating of cabin air in an aircraft, respectively with the method comprising the steps of: introducing aircraft cabin air into an aircraft cabin wall 6 ; guiding this aircraft cabin air along a section of this aircraft cabin wall 6 ; and leading this aircraft cabin air away from the aircraft cabin wall 6.
1. An aircraft cabin wall comprising an outer skin and a sidewall panel, wherein between the outer skin and the sidewall panel a defined air gap is provided for a controlled through-conveyance of aircraft cabin air; wherein on the inside of the outer skin a layer of primary insulation is provided; wherein on a side of the sidewall panel which side faces the outer skin a layer of secondary insulation is provided; and wherein the defined gap is formed between the primary insulation and the secondary insulation; and
wherein a ventilation device is provided for an active ventilation of the aircraft cabin through the gap.
2. The aircraft cabin wall of claim 1 , wherein the gap comprises a width (b) that is essentially uniform.
3. An aircraft comprising an aircraft cabin wall of claim 1 .
4. The aircraft cabin wall of claim 1 , wherein the defined gap comprises a drainage device for draining condensation water that forms in the gap and/or on the secondary insulation and/or on the primary insulation.
5. The aircraft cabin wall of claim 4 , wherein a collection device for a collection of condensation water is provided, wherein the collection device is optionally connectable to an air conditioning system of the aircraft, for re-supplying the condensation water to the cabin interior air.
6. An aircraft comprising an aircraft cabin wall of claim 5 , wherein the collection device is connected to the air conditioning system by a line.