{
  "$type": "site.standard.document",
  "description": "Plain bearing (50) for a mechanical reducer (6) of a turbomachine, in particular of an aircraft, the plain bearing (50) being formed from a single piece and comprising: - a cylindrical body (52) comprising: + an external cylindrical surface (56) for guiding, + a first axial mounting extension (64)…",
  "path": "/patents/1393499",
  "publishedAt": "2026-02-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D15/12",
    "SAFRAN TRANS SYSTEMS [FR]"
  ],
  "textContent": "Plain bearing (50) for a mechanical reducer (6) of a turbomachine, in particular of an aircraft, the plain bearing (50) being formed from a single piece and comprising: - a cylindrical body (52) comprising: + an external cylindrical surface (56) for guiding, + a first axial mounting extension (64), + a first circumferential flange (66) extending around the first extension (64), + a second axial mounting extension (68), and + a second circumferential flange (70) extending around the second extension (68), characterized in that it further comprises: - a fixing cover (54) which is connected to said first axial extension (64) and which extends axially facing said first flange (66).",
  "title": "PLAIN BEARING FOR A MECHANICAL GEAR OF AN AIRCRAFT TURBINE ENGINE",
  "updatedAt": "2026-06-19T12:30:58.894Z"
}