Aircraft arrestor system and method of decelerating an aircraft

E - Fixed Constructions – 01 – C

Patent

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E01C 9/00 (2006.01) B64F 1/02 (2006.01) E01C 3/00 (2006.01)

Patent

CA 2667360

An arrestor system and method of decelerating an aircraft. The arrestor system has a base with at least one tile made of a plurality of particles being arranged such that the particles form a plurality of water drainage passageways and wherein the at least one tile has a compressive strength which will fatigue upon a force being imparted thereto which is greater than the compressive strength of the tile.

La présente invention se rapporte à un système d'arrêt d'un aéronef, et à un procédé de décélération d'un aéronef. Le système d'arrêt comprend une base comprenant au moins un carreau constitué d'une pluralité de particules qui sont agencées de telle sorte que les particules forment une pluralité de voies de passage d'évacuation d'eau et, le(s) carreau(x) présentant une résistance à la compression qui se fatigue à mesure qu'une force est exercée sur lui et qui est supérieure à la résistance à la compression du carreau.

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