{
  "$type": "site.standard.document",
  "description": "Oil recovery gutter (100) for lubrication oil, in particular for a mechanical reducer of an aircraft turbomachine, annular around a central axis (X), and comprising a first radial wall (110) extending radially with respect to the central axis, an inclined wall (120) extending from an external…",
  "path": "/patents/1391875",
  "publishedAt": "2025-07-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/06",
    "SAFRAN TRANS SYSTEMS [FR]"
  ],
  "textContent": "Oil recovery gutter (100) for lubrication oil, in particular for a mechanical reducer of an aircraft turbomachine, annular around a central axis (X), and comprising a first radial wall (110) extending radially with respect to the central axis, an inclined wall (120) extending from an external radial end of the first radial wall (110), a guide portion (130) having a generally U-shaped form extending from an end of the inclined wall (120), and a second radial wall (140) extending radially outward with respect to the central axis (X) from an end of the guide portion (130), a space delimited by the first radial wall (110), the second radial wall (140) and the inclined wall (120) forming an oil intake chamber (150), and a space delimited by the guide portion (130) and the second radial wall (140) forming an oil evacuation cavity (160).",
  "title": "LUBRICATING OIL RECOVERY GUTTER FOR REDUCTION GEAR",
  "updatedAt": "2026-06-19T07:41:22.812Z"
}