{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) includes a spool (14) along an engine centerline axis (A) which drives a gear train (25), said spool (14) includes a low pressure compressor (16) with four to eight (4-8) stages.",
  "path": "/patents/984693",
  "publishedAt": "2013-07-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/28",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine (10) includes a spool (14) along an engine centerline axis (A) which drives a gear train (25), said spool (14) includes a low pressure compressor (16) with four to eight (4-8) stages.",
  "title": "Gas turbine engine"
}