Abstract: The anticollision light for aircraft, particularly airplanes, is provided with a holding body (12) with an outer side and several LEDs (16) arranged at the outer side of the holding body (12) the light-radiating directions of which point away from the holding body (12). Further, the anticollision light is provided with a drive unit (18) for the pulse-like drive of at least some of the LEDs (16) and a refractive optical element (26) for generating a desired spatial distribution of the light of the LEDs (16), the refractive optical element (26) surrounding the holding body at least in the region of the LEDs (16).

Abstract: An aircraft position light for an aircraft is provided with a luminous device for emitting light and a reflector arrangement. The luminous device comprises a first and a second light source, which emit light within a light radiation solid angle, the two light sources being arranged symmetrically to the preferential axis and central axes of the light radiation solid angles being inclined so as to face each other. The reflector arrangement comprises a first and a second reflection surface allocated to the first and second light source, respectively. The first reflection surface is arranged opposite to the first light source and the second reflection surface is arranged opposite to the second light source.

Abstract: The anticollision light for aircraft, particularly airplanes, is provided with a holding body (12) with an outer side and several LEDs (16) arranged at the outer side of the holding body (12) the light-radiating directions of which point away from the holding body (12). Further, the anticollision light is provided with a drive unit (18) for the pulse-like drive of at least some of the LEDs (16) and a refractive optical element (26) for generating a desired spatial distribution of the light of the LEDs (16), the refractive optical element (26) surrounding the holding body at least in the region of the LEDs (16).

Abstract: The light particularly serves as position light for an aircraft, preferably for being mounted to the rear end of an aircraft, such as, e.g., an airplane, and is provided with a luminous means for emitting light and a reflector arrangement. The luminous means comprises a first and a second light source which are substantially identical and respectively emit light within a light radiation solid angle with a central axis, the two light sources being arranged symmetrically to the preferential axis and the central axes of the light radiation solid angles being inclined so as to face each other.

Abstract: An aircraft floodlight includes a lens placed in front of a housing thereof, a gas discharge lamp that is provided along with a reflector, and an electronic power supply unit. The housing has at least two reflectors that are aligned at different angles to one another and generate overlapping cones of light.