{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) includes a first (86) and second (90) pump driven by a spool (30). An air-oil cooler (88) is located downstream of the first pump (86). An air-air precooler (92) is located downstream of the second pump (90) and the air-oil cooler (88).",
  "path": "/patents/984937",
  "publishedAt": "2013-04-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D13/06",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) includes a first (86) and second (90) pump driven by a spool (30). An air-oil cooler (88) is located downstream of the first pump (86). An air-air precooler (92) is located downstream of the second pump (90) and the air-oil cooler (88).",
  "title": "Gas turbine engine with integrated thermal management system"
}