{
  "$type": "site.standard.document",
  "description": "A thermal management system (100) for a gas turbine engine (20) includes a first heat exchanger (66) that provides a first conditioned fluid (83), a second heat exchanger (68) in series flow communication with the first heat exchanger (66) and that exchanges heat with the first conditioned fluid…",
  "path": "/patents/991185",
  "publishedAt": "2013-05-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/08",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A thermal management system (100) for a gas turbine engine (20) includes a first heat exchanger (66) that provides a first conditioned fluid (83), a second heat exchanger (68) in series flow communication with the first heat exchanger (66) and that exchanges heat with the first conditioned fluid (83) to provide a second conditioned fluid (89), and a third heat exchanger (70) in parallel flow communication with the second heat exchanger (68) and that selectively exchanges heat with the first conditioned fluid (83) to provide a third conditioned fluid (93). The second conditioned fluid (89) and the third conditioned fluid (93) combine to provide a mixed conditioned fluid (95). A first portion (97) of the mixed conditioned fluid (95) having a first temperature is communicated to a first engine system (110). A second portion (99) of the mixed conditioned fluid (95) having a second temperature is communicated to a second engine system (118). The second temperature includes a greater temperature than the first temperature.",
  "title": "Gas turbine engine thermal management system"
}