An air duct system comprising an air duct having a main body, a visible light source, and one or more photovoltaic devices. The main body of the air duct defines a passageway having a reflective inner surface. The visible light source is configured to generate visible light, where the visible light source directs the visible light along the reflective inner surface of the air duct. The one or more photovoltaic devices are disposed along the reflective inner surface of the air duct, where a portion of the visible light generated by the visible light source is converted into electrical power by the one or more photovoltaic devices.

A luminous laminated automotive glazing with diodes peripherally on a diode carrier facing the edge face of the interior glass equipped with a recess, a profiled bead and a protective adhesive strip between the diode carrier and the bead.

A luminous laminated automotive glazing with diodes peripherally on a diode carrier facing the edge face of the interior glass equipped with a recess, a profiled bead and a protective adhesive strip between the diode carrier and the bead.

An illumination system illuminates a periphery of a mirror that reflects a face of a user. A light is provided around the mirror. A sensor detects information on the face of the user and is located on a periphery of the mirror. A light control unit controls the lighting state of the light based on a detection result of the information on the face by the sensor.

An illumination system illuminates a periphery of a mirror that reflects a face of a user. A light is provided around the mirror. A sensor detects information on the face of the user and is located on a periphery of the mirror. A light control unit controls the lighting state of the light based on a detection result of the information on the face by the sensor.

A cabin interior arrangement 1 for an aircraft is proposed that comprises a first cabin interior object and a second cabin interior object 3a, b, comprising a power transmitting device 5 for transmitting power from an aircraft electrical system 7, wherein the power transmitting device 5 is arranged on the first cabin interior object 3a, comprising a power receiving device 6 for receiving the power from the power transmitting device 5, wherein the power receiving device 6 is arranged on the second cabin interior object 3b, wherein the power transmitting device 5 and the power receiving device 6 are embodied as a power transfer arrangement 2 for supplying the power to a mobile terminal 4, wherein the power transmitting device 5 and the power receiving device 6 are designed to transfer power over a distance of several centimetres, wherein the power transmitting device 5 and the power receiving device 6 are deigned to set up a wireless and/or cordless supply connection segment 10 between the power transmitting device 5 and the power receiving device 6. In addition, an aircraft is proposed that comprises the cabin interior arrangement 1 comprising the power transfer arrangement 2 for supplying power to the terminal 4.

A cabin interior arrangement 1 for an aircraft is proposed that comprises a first cabin interior object and a second cabin interior object 3a, b, comprising a power transmitting device 5 for transmitting power from an aircraft electrical system 7, wherein the power transmitting device 5 is arranged on the first cabin interior object 3a, comprising a power receiving device 6 for receiving the power from the power transmitting device 5, wherein the power receiving device 6 is arranged on the second cabin interior object 3b, wherein the power transmitting device 5 and the power receiving device 6 are embodied as a power transfer arrangement 2 for supplying the power to a mobile terminal 4, wherein the power transmitting device 5 and the power receiving device 6 are designed to transfer power over a distance of several centimetres, wherein the power transmitting device 5 and the power receiving device 6 are deigned to set up a wireless and/or cordless supply connection segment 10 between the power transmitting device 5 and the power receiving device 6. In addition, an aircraft is proposed that comprises the cabin interior arrangement 1 comprising the power transfer arrangement 2 for supplying power to the terminal 4.

A luminous laminated automotive glazing with diodes peripherally on a diode carrier facing the edge face of the interior glass equipped with a recess, a profiled bead and a protective adhesive strip between the diode carrier and the bead.

A luminous laminated automotive glazing with diodes peripherally on a diode carrier facing the edge face of the interior glass equipped with a recess, a profiled bead and a protective adhesive strip between the diode carrier and the bead.

A reactive illuminated wireless charging surface incorporated into a seating module or worksurface aboard an aircraft or other mobile platform has a translucent exterior surface beneath which a wireless charging device may be positioned and over which a PED may be placed for charging. The illuminated wireless charging surface may incorporate arrays or strips of individually addressable light emitting diodes (LED) or other like luminous devices set into flexible printed control boards (PCB) beneath the exterior surface. The illuminated wireless charging surface may have a display controller for driving the LED arrays in practical or aesthetically appealing ways to provide dynamic visual indication of a charging status, e.g., by adjusting individual LEDs or groups thereof to shift in color or intensity according to predetermined or preprogrammed patterns.