Window unit for an aircraft with shading and lighting functions
View Patent ↗A window unit for an aircraft with which individual lighting scenarios can be produced. In addition, an aircraft is equipped with at least one window unit. The window unit includes a window pane, which is coated with an electrically actuatable shading device for reducing incidental light entering through the window page. In addition, the window unit includes a control unit for operating the shading device as well as a lighting device for producing a light effect in the region of the window unit. In this connection, the control unit has an interface via which the control unit is connected to a network system of the aircraft for operation of the shading device. Likewise, the lighting device is coupled with the control unit, so that the lighting device can be operated with the network system of the aircraft via the interface of the control unit.
1. A window unit in an aircraft, comprising:
a window pane is coated with an electrically actuatable shading device for reducing incidental light penetrating through the window pane;
a control unit for operating the shading device;
a lighting device for producing a light effect in the region of the window unit;
whereby the control unit has an interface, via which the control unit is connected to a network system of the aircraft for operation of the shading device;
wherein the lighting device likewise is coupled with the control unit, in order to operate the lighting device with the network system of the aircraft via the interface of the control unit.
2. A window unit according to claim 1 ,
wherein the lighting device is supplied with energy via the control unit of the shading device.
3. A window unit according to claim 1 ,
wherein the lighting device is controlled by the network system of the aircraft via the control unit of the shading device, which supplied the lighting device with the necessary control signals.
4. A window unit according to claim 1 , further comprising:
a window funnel, at whose smaller opening the window pane is located and which faces in the direction of the passenger cabin of the aircraft with its widening, so that it forms a section of the inner lining of the passenger cabin,
whereby the lighting device is arranged on the window funnel, such that the widening of the window funnel is illuminated at least partially by the lighting device upon operation of the lighting device.
5. A window unit according to claim 4 ,
wherein the lighting device includes a plurality of illumination means, which are arranged in the widening area of the window funnel.
6. A window unit according to claim 4 ,
wherein the lighting device includes a plurality of illumination means, which are arranged on the outer side of the window funnel in the region of the widening area.
7. A window unit according to claim 5 ,
wherein the illumination means are formed in order to produce light of different wavelengths.
8. A window unit according to claim 5 ,
wherein the illumination means are formed as RGB light diodes.
9. An aircraft comprising at least one window unit, the window unit comprising:
a window pane is coated with an electrically actuatable shading device for reducing incidental light penetrating through the window pane;
a control unit for operating the shading device;
a lighting device for producing a light effect in the region of the window unit;
whereby the control unit has an interface, via which the control unit is connected to a network system of the aircraft for operation of the shading device;
wherein the lighting device likewise is coupled with the control unit, in order to operate the lighting device with the network system of the aircraft via the interface of the control unit.