| 摘要 |
The invention relates to an escape path marking for an aircraft, having a plurality of photoluminescent elements (12, 30, 36, 44, 84, 88, 100, 102, 54, 56, 70, 72, 80, 104, 106), which glow in the dark and of which each has a carrier element that is provided for attaching to a subsurface, characterized in that the carrier element has connecting edges (14, 16, 31, 33, 38, 40, 46, 50, 108, 110) on one or both end sides, the edges having an arc-shaped progression or having at least two sections not extending perpendicular to an orientation axis (A) of the carrier element disposed perpendicularly on a cross-section in the region of the connecting edge, wherein the orientation axes (A) of two carrier elements disposed successively enclose an angle with each other. |
