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 element with a light emitting device preferably in the form of a light emitting diode, can be fitted in a light carrier. The lighting element has a light-transmissive lens body with a lens-shaped light entry surface and a light exit surface and the light exit surface is smaller than the light entry surface. A starry sky lighting configuration for example in an aircraft cabin, can be implemented with a plurality of such lighting elements.

Abstract: A lighting element has a light emitting diode that is installed in a light carrier. The lighting element has a light guide element that is optically coupled to the light emitting diode and the light guide element has a smaller light exit surface than the light emitting diode. With a plurality of such lighting elements it is possible to embody an effect lighting configuration for example in an aircraft cabin.

Abstract: A method for monitoring and controlling a plurality of series-connected capacitance, wherein at least during the discharge of the capacitances, there is determined a voltage of every capacitance, and in the instance of a drop-off of a voltage of one of the capacitances below a first threshold voltage of this capacitance, the capacitance is bridged over to at least the end of the discharge. Also provided are devices for determining every voltage of every capacitance, devices for symmetrizing voltages among the capacitances, and devices for the deactivation of at least one of the capacitances.

Abstract: An emergency power supply apparatus (1), in particular in an aircraft, having an appliance chassis (2) and having a battery housing (3) which can be fitted to it for holding a number of batteries or rechargeable batteries, with first latching elements (14, 16) being provided at the side on the battery housing (3) and interacting detachably with corresponding second latching elements (15), which are provided on the appliance chassis (2), in the form of a snap-action connection.

Abstract: A control device for the actuation of lamps in particular for internal aircraft lighting, wherein the control device (1) has an input (18) for the supply of an input signal and a plurality of outputs (21–28) for passing output signals to connected lamps (L1–L8). In the control device (1) a signal processing module (8–12) is preferably formed by a microprocessor and a preferably freely programmable electronic memory (13–17). The signal processing module (8–12) produces the output signals from the input signal in accordance with a conversion instruction deposited in the memory (13–17), wherein different conversion instructions can be stored in the memory (13–17) for output signals belonging to different outputs (21–28).

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).

Abstract: A control device for the actuation of lamps in particular for internal aircraft lighting, wherein the control device (1) has an input (18) for the supply of an input signal and a plurality of outputs (21-28) for passing output signals to connected lamps (L1-L8). In the control device (1) a signal processing module (8-12) is preferably formed by a microprocessor and a preferably freely programmable electronic memory (13-17). The signal processing module (8-12) produces the output signals from the input signal in accordance with a conversion instruction deposited in the memory (13-17), wherein different conversion instructions can be stored in the memory (13-17) for output signals belonging to different outputs (21-28).

Abstract: An apparatus for lighting or illuminating spaces, bodies or surfaces, which is formed from a plurality of light emitting diodes (1). The light emitting diodes (1) are radially enclosed by a casing body (14) which is adjoined at the end by a tubular element (15) which bears against a lens (4). A set spacing is thereby established between the light emitting diode (1) and the lens (4). All light spots issuing from the light emitting diode (1) are projected to form a single light spot of a high level of brightness by virtue of the superimposed relationship at a spacing in front of the lens (4).