{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) includes a bypass duct (16) for a bypass airflow and a diffuser case (66) including an inlet (92) in communication with the bypass duct (16) for communicating a bypass flow (76) to a heat exchanger portion (68). An outlet passage (94) extends through the bypass duct (16)…",
  "path": "/patents/1424736",
  "publishedAt": "2024-02-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) includes a bypass duct (16) for a bypass airflow and a diffuser case (66) including an inlet (92) in communication with the bypass duct (16) for communicating a bypass flow (76) to a heat exchanger portion (68). An outlet passage (94) extends through the bypass duct (16) to exhaust airflow exiting the heat exchanger portion (68) outside of the bypass duct (16).",
  "title": "DIFFUSER CASE HEAT EXCHANGER"
}