Passenger light cooling
The invention relates to a passenger service unit for an aircraft, comprising at least one light source and at least one passenger air supply device. According to the invention the passenger air supply device is adapted for applying a flow of air to the light source. Furthermore it relates to a method for providing light and fresh air to passenger of an aircraft by providing an air flow from an air supply device and light from a light source to the passenger. The method comprises applying an air flow from said passenger air supply device to said light source for cooling the light source by means of convection. Furthermore the invention relates to a method for assembling a passenger service unit and to an aircraft.
1. A passenger service unit for an aircraft, comprising at least one light source and at least one passenger air supply device, wherein the passenger air supply device is adapted for applying a flow of air to the light source, wherein a direction of the air flow provided to at least one passenger and a direction of a radiation of light from the light source may be adjusted independently from each other, and
wherein the passenger air supply device comprises an air duct with an outlet for directing the air flow to the at least one passenger and the light source is at least partially integrated into the air duct.
2. The passenger service unit according claim 1 , wherein the light source is arranged in an outlet of an air duct of the passenger air supply device.
3. The passenger service unit according to claim 1 wherein the outlet comprises an orifice mounted in a first mounting component and being movable with regard to this first mounting component for directing the flow of air exiting the orifice into at least two, preferably a plurality of alternative directions and that the light source is mounted in a second mounting component and being movable with regard to this second mounting component for directing the light beam into at least two, preferably a plurality of alternative directions and preferably the second mounting component being movable with regard to the first mounting component.
4. The passenger service unit according to claim 3 , wherein the orifice is closable by means of closing means.
5. The passenger service unit according to claim 4 , wherein the light source is arranged upstream of the closing means and at least one of the orifice and the closing means is at least partially transparent.
6. The passenger service unit according to claim 5 , wherein the light source receiving an air flow in case the closing means are in a closed position in that:
the closing means cannot be fully closed, and/or
a bypass duct for directing an air flow to the light source is present.
7. The passenger service unit according to claim 1 , wherein the outlet is closable by means of closing means.
8. The passenger service unit according to claim 1 , wherein the light source is mounted in a frame element inside the air duct.
9. An aircraft comprising at least one passenger service unit according to claim 1 .
10. A passenger service unit for an aircraft comprising at least one light source and at least one passenger air supply device, wherein:
the passenger air supply device is adapted for applying a flow of air to the light source, wherein a direction of the air flow and a direction of a radiation of light from the light source may be adjusted independently from each other, and
the passenger air supply device comprises an air duct with a first outlet for directing a first air flow to a passenger and a second outlet comprising a nozzle for directing a second air flow to the light source.
11. The passenger service unit according to claim 10 , wherein the light source is arranged in an outlet of an air duct of the passenger air supply device.
12. The passenger service unit according to claim 10 , wherein the outlet is closable by means of closing means.
13. The passenger service unit according to claim 12 , wherein the orifice is closable by the closing means.
14. The passenger service unit according to claim 12 , wherein the light source is arranged upstream of the closing means and at least one of the orifice and the closing means is at least partially transparent.
15. The passenger service unit according to claim 14 , wherein the light source receiving an air flow in case the closing means are in a closed position in that:
the closing means cannot be fully closed, and/or
a bypass duct for directing an air flow to the light source is present.
16. The passenger service unit according to claim 10 , wherein the light source is mounted in a side wall of the air duct and extending into the air duct.
17. An aircraft comprising at least one passenger service unit according to claim 10 .