{
  "$type": "site.standard.document",
  "description": "The device has a coupling unit (10) with a front trunnion (14) having triangular shackles placed in a vertical plane oriented along a direction inclined with respect to longitudinal and transversal directions of an aircraft. The shackles are situated in a horizontal plane defined along the…",
  "path": "/patents/1077375",
  "publishedAt": "2005-06-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/12",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The device has a coupling unit (10) with a front trunnion (14) having triangular shackles placed in a vertical plane oriented along a direction inclined with respect to longitudinal and transversal directions of an aircraft. The shackles are situated in a horizontal plane defined along the transversal and longitudinal directions. A rear trunnion (16) has shackles oriented along vertical direction of the aircraft.",
  "title": "Underwing aircraft engine mounting structure"
}