{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) includes a fan section (22) and an intercooling turbine section (24) along an engine axis aft of the fan section (22) and forward of a combustor section (30).",
  "path": "/patents/991234",
  "publishedAt": "2013-05-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/143",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine (10) includes a fan section (22) and an intercooling turbine section (24) along an engine axis aft of the fan section (22) and forward of a combustor section (30).",
  "title": "Gas turbine engine with intercooling turbine section"
}