{
  "$type": "site.standard.document",
  "description": "A bearing support for a rotor (12) of an aircraft turbine engine (10) includes a front bearing and a front bearing support (118) and bearing strut (120) for securely attaching the front bearing to the aircraft turbine engine support structure (122). The front bearing support (118) and bearing strut…",
  "path": "/patents/1084765",
  "publishedAt": "2004-08-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/162",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A bearing support for a rotor (12) of an aircraft turbine engine (10) includes a front bearing and a front bearing support (118) and bearing strut (120) for securely attaching the front bearing to the aircraft turbine engine support structure (122). The front bearing support (118) and bearing strut (120) are integral with the aircraft turbine engine support structure (122).",
  "title": "Gas turbine engine bearing support"
}