{
  "$type": "site.standard.document",
  "description": "Aircraft wheel rim in two parts, one main part (1) comprising a hub (2), a web (4) extending between the hub and an annular external portion (3) intended to receive a tire and shaped to present a bead (5) at one of its ends, the other of its ends being shaped to receive a removable part (10)…",
  "path": "/patents/959424",
  "publishedAt": "2015-07-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60B21/104",
    "MESSIER BUGATTI DOWTY [FR]"
  ],
  "textContent": "Aircraft wheel rim in two parts, one main part (1) comprising a hub (2), a web (4) extending between the hub and an annular external portion (3) intended to receive a tire and shaped to present a bead (5) at one of its ends, the other of its ends being shaped to receive a removable part (10) forming a bead (12) which is fitted onto the annular external portion after placement of the tire, the rim comprising means for blocking rotation of the removable bead relative to the rim comprising at least one link rod (20) having ends whose centers define an axis which extends in a plane perpendicular to an axis of rotation of the rim while extending obliquely to make an angle (α) with respect to a radial direction, one of the ends being coupled to the main part, and the other of its ends being coupled to the removable part.",
  "title": "Aircraft wheel rim with removable flange"
}