{
  "$type": "site.standard.document",
  "description": "The invention relates to a forward engine attachment system (150) for an engine (102) comprising a reactor mast (104) with a nose (110) presenting a main female clevis (111) and a cylindrical housing, a main rod (162) fixed to the engine (102) by a secondary ball joint connection around a secondary…",
  "path": "/patents/1387586",
  "publishedAt": "2026-03-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/12",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to a forward engine attachment system (150) for an engine (102) comprising a reactor mast (104) with a nose (110) presenting a main female clevis (111) and a cylindrical housing, a main rod (162) fixed to the engine (102) by a secondary ball joint connection around a secondary axis (12), a main shaft (165) providing a main ball joint connection of the main rod (162) in the main female clevis (111) around a main axis (10), where the main axis (10) and the secondary axis (12) are in the same vertical plane, a hollow outer cylinder with vertical axis, of which a first end is fixed in the cylindrical housing and of which a second end is mounted movably through an annular linear connection with respect to the front casing (103) and an inner cylinder threaded and fixed in the outer cylinder. [0002] Such a forward engine attachment system has reduced vertical bulk because the forward engine attachment is integrated into the reactor mast.",
  "title": "FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE HAVING A COMPACT STRUCTURE",
  "updatedAt": "2026-06-14T13:21:27.163Z"
}