{
  "$type": "site.standard.document",
  "description": "A nacelle assembly for a high-bypass gas turbine engine (10) includes a variable area fan nozzle (42) in communication with a fan bypass flow path (40). An actuator assembly (56) is operable to move a second fan nacelle section (54) relative to a first fan nacelle section (52) to vary a fan nozzle…",
  "path": "/patents/1005076",
  "publishedAt": "2012-02-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/06",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A nacelle assembly for a high-bypass gas turbine engine (10) includes a variable area fan nozzle (42) in communication with a fan bypass flow path (40). An actuator assembly (56) is operable to move a second fan nacelle section (54) relative to a first fan nacelle section (52) to vary a fan nozzle exit area and adjust fan bypass airflow. The actuator assembly (56) extends at least partially into the fan bypass flow path (40).",
  "title": "Variable area fan nozzle"
}