{
  "$type": "site.standard.document",
  "description": "To provide an aircraft tire capable of suppressing rubber tire wear during landing and shocks which accelerate or decelerate an aircraft at touchdown. An aircraft tire 3 includes, on a side of a tire body 4 constituting an outer peripheral part of an aircraft wheel 1, a protrusion 5 for receiving…",
  "path": "/patents/952877",
  "publishedAt": "2016-03-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60C13/02",
    "DAITO PRESS MFG CO LTD [JP]"
  ],
  "textContent": "To provide an aircraft tire capable of suppressing rubber tire wear during landing and shocks which accelerate or decelerate an aircraft at touchdown. An aircraft tire 3 includes, on a side of a tire body 4 constituting an outer peripheral part of an aircraft wheel 1, a protrusion 5 for receiving flight wind pressure. The wheel 1 is rotated ahead of the touchdown by the action of the wind pressure received by the protrusion 5 in a direction in which the wheel 1 rotates during a landing roll. Weight 15 is inserted into a hollow part 11 of the protrusion 5. Through use of centrifugal force on the weight 15 in association with a rotational motion of the wheel 1, the protrusion 5 is deformed to change its wind pressure receiving area for bringing rotational speed of the wheel 1 ahead of the touchdown close to a rotating speed of the wheel that is consistent with a flying speed of the aircraft making the touchdown.",
  "title": "AIRCRAFT TIRE"
}