Crown Reinforcement For Aircraft Tire

An aircraft tire comprising:

• a working reinforcement radially on the inside of a tread and radially on the outside of a carcass reinforcement;
• the working reinforcement comprising at least one working layer made up of a circumferential zigzag winding of a strip on a cylindrical surface having as its axis of revolution the axis of rotation of the tire, with a periodic curve, the peak-to-peak amplitude of which defines the axial width L of the working layer between a first and a second axial end;
• the working layer being made up, in any meridian plane containing the axis of rotation of the tire, of an arrangement of portions of strip R extending axially from the first axial end to the second axial end of the working layer,
• the strip of width W being made up of textile reinforcers coated in an elastomeric compound,
• wherein, in any meridian plane containing the axis of rotation of the tire, the arrangement of portions of the strip extending axially from the first axial end to the second axial end of the working layer is such that two consecutive portions of the strip overlap, at least in part, over a width of overlap e, and wherein the width of overlap e between two consecutive portions of the strip is constant over the entire axial width L of the working layer.