{
  "$type": "site.standard.document",
  "description": "An aircraft system includes a turbine engine case and an attachment that is configured to mount the turbine engine case (64) to a pylon structure (88) and transfer one or more loads between the turbine engine case (64) and the pylon structure (88). The attachment includes a bracket (100), a first…",
  "path": "/patents/1416596",
  "publishedAt": "2026-06-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/402",
    "RTX CORP [US]"
  ],
  "textContent": "An aircraft system includes a turbine engine case and an attachment that is configured to mount the turbine engine case (64) to a pylon structure (88) and transfer one or more loads between the turbine engine case (64) and the pylon structure (88). The attachment includes a bracket (100), a first link (102A) and a second link (102B). The bracket is configured to mount to the pylon structure (88) through a bracket-pylon pin connection (160) such that the attachment (98) is operable to pivot about the bracket-pylon pin connection (160) and move relative to the pylon structure (88). The bracket is mounted to the first link (102A) through a bracket-first link pin connection (144A). The bracket is mounted to the second link (102B) through a bracket-second link pin connection (144B). The first link (102A) is mounted to the turbine engine case (64) through a first link-case pin connection (146A). The second link (102B) is mounted to the turbine engine case (64) through a second link-case pin connection (146B).",
  "title": "ATTACHMENT FOR MOUNTING AIRCRAFT PROPULSION SYSTEM TO PYLON STRUCTURE"
}