| 摘要 |
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. The reflector arrangement comprises a first and a second reflection surface allocated to the first and second light source, respectively, said reflection surfaces also being symmetrically arranged to the preferential axis and respectively provided with a light propagation limiting edge for limiting the light propagation range, within which light emitted directly by the respectively allocated light source emerges from the receiving room of the housing. 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. The two reflection surfaces are oriented and/or configured such that light emitted by the one light source is reflected by the reflection surface allocated thereto past the light propagation limiting edge of the other reflection surface to increase the luminous intensity within the light propagation range of the other light source near the partial range defined by the light propagation limiting edge of the one reflection surface.
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