Crown Reinforcement For An Airplane Tire

摘要

Working reinforcement (2) of airplane tire (1) is radially inside tread (3) and radially outside carcass reinforcement (4), comprising carcass layer (41). Working reinforcement (2) comprises working biply (21) of greatest axial width (LT) and two axial ends (E). Hoop reinforcement (7) comprises hooping layer (71) radially inside working biply (21), and having axial width (LF) at least equal to 0.8 times LT. Distance D between axial end (E) of greatest axial width (LT) and its orthogonal projection (I) onto the radially outermost carcass layer (41) is at least equal to 7 mm and the distance D′ between point (F) of working biply (21) of greatest axial width (LT), axially inside axial end (E) at a distance L equal to 25 mm, and its orthogonal projection (J) onto the radially outermost carcass layer (41) is at least equal to 4 mm and at most equal to the distance D.

主权项

1. An airplane 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 biply consisting at least in part of two radially superposed working layers; each working layer comprising reinforcers coated in an elastomeric material, positioned circumferentially along a periodic curve and forming, with the circumferential direction of the tire and in the equatorial plane of the tire (XZ), an angle at least equal to 8° and at most equal to 30°; the working biply of greatest axial width (LT) comprising two axial ends (E) each one corresponding to the axially outermost and radially innermost point of the working biply; the carcass reinforcement comprising at least one carcass layer comprising reinforcers which are coated in an elastomeric material, forming, with the circumferential direction of the tire, an angle at least equal to 80° and at most equal to 100°; a hoop reinforcement comprising at least one hooping layer comprising reinforcers which are coated in an elastomeric material, forming, with the circumferential direction of the tire, an angle at most equal to 5°; at least one hooping layer being radially on the inside of the working biply of greatest axial width (LT), and having an axial width (LF) at least equal to 0.8 times the axial width (LT) of the working biply of greatest axial width (LT); wherein the distance D between an axial end of the working biply of greatest axial width (LT) and its orthogonal projection (I) onto the radially outermost carcass layer is at least equal to 7 mm and wherein the distance D′ between the point of the working biply of greatest axial width (LT), axially on the inside of the axial end at a distance L equal to 25 mm, and its orthogonal projection (J) onto the radially outermost carcass layer is at least equal to 4 mm and at most equal to the distance D.