{
  "$type": "site.standard.document",
  "description": "The device has connection elements (46) e.g. bolts or rivets, housed in passage holes (38, 44) formed in cylindrical parts to be connected, respectively. Each element comprises a rod (48) having ends provided with supports (50, 52) for holding the parts in a plated manner. Each hole includes a…",
  "path": "/patents/999795",
  "publishedAt": "2012-08-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D29/00",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The device has connection elements (46) e.g. bolts or rivets, housed in passage holes (38, 44) formed in cylindrical parts to be connected, respectively. Each element comprises a rod (48) having ends provided with supports (50, 52) for holding the parts in a plated manner. Each hole includes a reduced section adjusted to a section of the rod near the corresponding support, and another section with a large clearance at a junction plane (42), such that the rod is subjected to weak shearing forces at the junction plane during relative deformation of the connected parts.",
  "title": "Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle"
}