Abstract: An electronic irritation device includes a plurality of electronic irritation signal modules. Each of the modules has at least one emitter for emitting optical or acoustic irritation signals, and additionally a connection device for coupling the plurality of irritation signal modules to one another and an unlocking device for automatically unlocking the connection device in order to decouple the plurality of irritation signal modules from one another and thereby distribute them spatially. Distributing a plurality of irritation signal modules makes it possible to increase the probability of an irritation effect upon deployment of a single irritation device.

Abstract: A room region (1) for an aircraft is provided, which room region comprises a disinfecting device (3) for disinfecting at least one surface (4) of the room region (1), wherein the disinfecting device (3) is designed to disinfect the surface (4) of the room region (1) by means of UVC radiation (5). The disinfecting device (3) comprises a lighting apparatus (6) for generating and emitting the UVC radiation (5). The lighting apparatus (6) is portable, and, in an active state, the lighting apparatus (6) is stationary and arranged.

Abstract: An electronic dazzling element has at least one optical emitter for emitting light pulses, which contains an electronic light-emitting device for generating light pulses, and a control device for controlling the light-emitting device of the optical emitter. In order to reduce the brightness reduction of the light pulses as a distance from the dazzling element increases, the optical emitter is configured to emit a collimated light beam. In order to simultaneously achieve the dazzling effect in as large a spatial region as possible, a beam direction of the collimated light beam may be changed.

Abstract: In an electronic dazzling element having at least one optical emitter with at least one electronic light-emitter for emitting light pulses, the light-emitter of the at least one optical emitter is controlled in such a way that a light pulse sequence emitted by the light-emitter is adapted to the physiology of the human eye.

Abstract: An electronic irritation device includes a plurality of electronic irritation signal modules. Each of the modules has at least one emitter for emitting optical or acoustic irritation signals, and additionally a connection device for coupling the plurality of irritation signal modules to one another and an unlocking device for automatically unlocking the connection device in order to decouple the plurality of irritation signal modules from one another and thereby distribute them spatially. Distributing a plurality of irritation signal modules makes it possible to increase the probability of an irritation effect upon deployment of a single irritation device.

Abstract: An electronic dazzling element has at least one optical emitter for emitting light pulses, which contains an electronic light-emitting device for generating light pulses, and a control device for controlling the light-emitting device of the optical emitter. In order to reduce the brightness reduction of the light pulses as a distance from the dazzling element increases, the optical emitter is configured to emit a collimated light beam. In order to simultaneously achieve the dazzling effect in as large a spatial region as possible, a beam direction of the collimated light beam may be changed.

Abstract: The present invention is directed to a luminous means comprising at least one light-emitting diode which is at least partly accommodated in a connection block, wherein electrical connections of the at least one light-emitting diode exit from the connection block in an angled fashion relative to the preferred light emission direction (M). The invention is further directed to a cable harness comprising at least one of said luminous means, as well as to an interior trim element comprising said luminous means.

Abstract: The temperature dependence of the most important characteristics of OLEDs (11) can be effectively counteractively controlled by the power supply (18) thereof if the actual instantaneous operating temperature is detected metrologically by at least one temperature sensor (19) incorporated into the hermetically encapsulated OLED (11). For this purpose, a line section (20) composed of a material having a high temperature coefficient of its electrical resistance is applied in electrically insulated fashion to one of the electrodes (areal transparent anode 13 or geometrically structured cathode 16), in a manner facing or averted from the polymer (14). If the temperature sensor (19) is arranged before the cathode on the emission side, that is to say even if it is arranged at the anode (13), its line section (20) preferably runs outside the projection of those geometrically structured regions of the cathode (16) which govern the cross-sectional geometries of the polymer excitation and thus of the emissions (15).

Abstract: A lighting arrangement (1) of a space-saving configuration, including a fluorescent lamp (2) and at least one light emitting diode (6), which is suitable in particular for use for interior lighting of an aircraft. In this case the light emitting diode (6), viewed in the direction of a main lighting direction (13), is arranged behind the fluorescent lamp (2). The lighting arrangement (1) further includes a light guide element (10) which is adapted to guide light (L2) emitted by the light emitting diode (6) past the fluorescent lamp (2) and emit it substantially in the main lighting direction (13).

Abstract: A lighting arrangement (1) which is advantageous in particular for the interior lighting of a vehicle or aircraft. The lighting arrangement (1) includes a plurality of light emitting diodes (2a-2e, 3a-3d, 4a-4c) of at least two groups (9, 10, 11), the light emitting diodes being arranged on a surface element (5, 5?, 5?), wherein each group (9, 10, 11) includes a light emitting diode or a plurality of light emitting diodes (2a-2e; 3a-3d; 4a-4c) of the same kind and light emitting diodes (2a-2e, 3a-3d, 4a-4c) of different groups (9, 10, 11) are of different kinds. The light emitting diodes (2a-2e, 3a-3d, 4a-4c) are distributed in a two-dimensional geometrical overall pattern (13) on the surface element (5, 5?, 5?).

Abstract: A lighting arrangement (1) which is advantageous in particular for the interior lighting of a vehicle or aircraft. The lighting arrangement (1) includes a plurality of light emitting diodes (2a-2e, 3a-3d, 4a-4c) of at least two groups (9, 10, 11), the light emitting diodes being arranged on a surface element (5, 5?, 5?), wherein each group (9, 10, 11) includes a light emitting diode or a plurality of light emitting diodes (2a-2e; 3a-3d; 4a-4c) of the same kind and light emitting diodes (2a-2e, 3a-3d, 4a-4c) of different groups (9, 10, 11) are of different kinds. The light emitting diodes (2a-2e, 3a-3d, 4a-4c) are distributed in a two-dimensional geometrical overall pattern (13) on the surface element (5, 5?, 5?).

Abstract: A lighting arrangement (1) of a space-saving configuration, including a fluorescent lamp (2) and at least one light emitting diode (6), which is suitable in particular for use for interior lighting of an aircraft. In this case the light emitting diode (6), viewed in the direction of a main lighting direction (13), is arranged behind the fluorescent lamp (2). The lighting arrangement (1) further includes a light guide element (10) which is adapted to guide light (L2) emitted by the light emitting diode (6) past the fluorescent lamp (2) and emit it substantially in the main lighting direction (13).