Escape path marking for an aircraft

A - Human Necessities – 62 – B

Patent

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Details

A62B 3/00 (2006.01) B60Q 3/02 (2006.01) B64D 25/08 (2006.01) F21S 4/00 (2006.01) G09F 13/20 (2006.01) G09F 19/22 (2006.01)

Patent

CA 2679653

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.

L'invention concerne un marquage d'issues de secours destiné à un avion et comprenant plusieurs éléments photoluminescents (12, 30, 36, 44, 84, 88, 100, 102, 54, 56, 70, 72, 80, 104, 106) qui brillent dans le noir et dont chacun présente un élément support permettant la fixation au sol. Le marquage selon l'invention est caractérisé en ce que l'élément support présente à une ou au deux extrémités des arêtes de raccord (14, 16, 31, 33, 38, 40, 46, 50, 108, 110) ayant une allure arquée ou présentant au moins deux segments qui ne s'étendent pas perpendiculairement à un axe d'orientation (A) de l'élément support, cet axe d'orientation étant perpendiculaire à une section transversale dans la zone de l'arête de raccord. Les axes d'orientation (A) de deux éléments supports successifs forment un angle entre eux.

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