{
  "$type": "site.standard.document",
  "description": "The device has a first annular flange (50) connected to an air intake (42). A second annular flange (46) is connected to a motorization pipe (44) plated against the first flange. A connection element (56) comprises a wall arranged on a plane perpendicular to an axis of a nacelle comprising a…",
  "path": "/patents/992996",
  "publishedAt": "2013-02-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The device has a first annular flange (50) connected to an air intake (42). A second annular flange (46) is connected to a motorization pipe (44) plated against the first flange. A connection element (56) comprises a wall arranged on a plane perpendicular to an axis of a nacelle comprising a reduction thickness part (72) with respect to rest of the wall. The thickness part is placed with respect to the element to allow relative movement between the element and the air intake and/or the motorization pipe by deformation. A sleeve (64) is inserted between the second flange and a support (62).",
  "title": "Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle"
}