{
  "$type": "site.standard.document",
  "description": "A turbofan engine (10) includes a fan variable area nozzle (42) axially movable relative to the fan nacelle (34) to vary a fan nozzle exit area (44) and adjust a pressure ratio of the fan bypass airflow (B) during engine operation.",
  "path": "/patents/1422806",
  "publishedAt": "2024-02-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "RTX CORP [US]"
  ],
  "textContent": "A turbofan engine (10) includes a fan variable area nozzle (42) axially movable relative to the fan nacelle (34) to vary a fan nozzle exit area (44) and adjust a pressure ratio of the fan bypass airflow (B) during engine operation.",
  "title": "GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO"
}