{
  "$type": "site.standard.document",
  "description": "A gas turbine engine includes a first pump (86) driven by a spool (30), an air-oil cooler (88) downstream of the first pump (86), a second pump (90) driven by the spool (30) and an air-air precooler (92) downstream of the second pump (90). The air-air precooler (92) is downstream of the air-oil…",
  "path": "/patents/984968",
  "publishedAt": "2013-04-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/08",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine includes a first pump (86) driven by a spool (30), an air-oil cooler (88) downstream of the first pump (86), a second pump (90) driven by the spool (30) and an air-air precooler (92) downstream of the second pump (90). The air-air precooler (92) is downstream of the air-oil cooler (88). A compartment is downstream of the precooler (92) to receive a cooling air from the precooler (92).",
  "title": "Compartment cooling for a gas turbine engine"
}