{
"$type": "site.standard.document",
"coverImage": {
"$type": "blob",
"ref": {
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"size": 80760
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"description": "Provided is an aircraft tire which has both satisfactory light weight and satisfactory separation durability of carcass ply ends. An aircraft tire () includes a pair of bead cores (), and a carcass () extending between the pair of the bead cores (). In this aircraft tire (), the carcass () includes…",
"path": "/patents/1285743",
"publishedAt": "2021-03-18T00:00:00.000Z",
"site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
"tags": [
"B60C9/08",
"BRIDGESTONE CORPORATION"
],
"textContent": "Provided is an aircraft tire which has both satisfactory light weight and satisfactory separation durability of carcass ply ends. An aircraft tire () includes a pair of bead cores (), and a carcass () extending between the pair of the bead cores (). In this aircraft tire (), the carcass () includes at least one layer of a turn-up ply () which is composed of a main body () and folded portions (), and at least one layer of a down ply () which covers a tire width-direction outer side of the respective folded portions () of the turn-up ply () and extends to at least a tire radial-direction inner side of the respective bead cores (); rubber-cord reinforcing members () are each arranged between the main body () of an outermost turn-up ply () and the folded portion () of the turn-up ply () extending to a tire radial-direction outermost side, and between the folded portion () of the turn-up ply () extending to the tire radial-direction outermost side and an innermost down ply (); and cords of the rubber-cord reinforcing members () have an elongation at break of not less than 30%.",
"title": "AIRCRAFT TIRE"
}