{
  "$type": "site.standard.document",
  "description": "A thermal management system (68) for a gas turbine engine (20) includes a first heat exchanger (HX1) and a second heat exchanger (HX2) in communication with a bypass flow through an inlet (70). A valve (72) is operable to selectively communicate the bypass flow to either the first heat exchanger or…",
  "path": "/patents/993830",
  "publishedAt": "2013-01-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/085",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A thermal management system (68) for a gas turbine engine (20) includes a first heat exchanger (HX1) and a second heat exchanger (HX2) in communication with a bypass flow through an inlet (70). A valve (72) is operable to selectively communicate the bypass flow to either the first heat exchanger or the second heat exchanger through the inlet.",
  "title": "Thermal management system for gas turbine engine"
}