{
  "$type": "site.standard.document",
  "description": "A method for servicing a gas turbine engine (120) includes providing access from a forward section of the gas turbine engine (120) to a gearbox (148) contained within a bearing compartment (B).",
  "path": "/patents/990256",
  "publishedAt": "2013-05-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/164",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A method for servicing a gas turbine engine (120) includes providing access from a forward section of the gas turbine engine (120) to a gearbox (148) contained within a bearing compartment (B).",
  "title": "Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings"
}