{
  "$type": "site.standard.document",
  "description": "The nacelle has a connecting device comprising an annular flange (46) that is connected to an air inlet (42), and another annular flange (50) connected to a motor (44) that is pressed against the former flange. The flanges extend in a plane perpendicular to a longitudinal axis of the nacelle…",
  "path": "/patents/992997",
  "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 nacelle has a connecting device comprising an annular flange (46) that is connected to an air inlet (42), and another annular flange (50) connected to a motor (44) that is pressed against the former flange. The flanges extend in a plane perpendicular to a longitudinal axis of the nacelle. Connecting elements i.e. bolts, are placed in respective bolt holes (48, 54) for connecting the flanges. One of the flanges comprises a U- or V-shaped opening (72) located between the bolt hole and a junction zone (68) of the flange and/or between the bolt hole and an outer edge (74) of the flange.",
  "title": "Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle"
}