CROWN FOR AN AIRCRAFT TIRE

摘要

The invention relates to a tire for an aircraft, including a tread (2) including at least two circumferential ribs (4) adjacent to at least one circumferential groove (5), each circumferential rib (4) extending axially between the two side surfaces (7) and circumferentially over the entire periphery of the tire. The tread (2) includes lines (8) of recess (9) formed in at least one circumferential groove (4) and opening onto the rolling surface (3). Said lines are mutually parallel, angled relative to the circumferential direction (XX') of the tire at an angle (i) >= 45°, and distributed over at least a portion of the periphery of the tire according to a circumferential pitch (p) >= 0.02 times and <= 0.12 times the circumferential length of the periphery of the tire (1).