{
  "$type": "site.standard.document",
  "description": "A nacelle assembly (N) for a bypass gas turbine engine includes a variable area fan nozzle (42) having a first fan nacelle section (52) and a second fan nacelle section (54). The variable area fan nozzle (42) is in communication with a fan bypass flow path (40). The first fan nacelle section (52)…",
  "path": "/patents/1003010",
  "publishedAt": "2012-04-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K1/06",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A nacelle assembly (N) for a bypass gas turbine engine includes a variable area fan nozzle (42) having a first fan nacelle section (52) and a second fan nacelle section (54). The variable area fan nozzle (42) is in communication with a fan bypass flow path (40). The first fan nacelle section (52) defines an intermittent trailing edge (60) which defines a multiple of ports (62) and the second fan nacelle section (54) defines a multiple of doors (66). Each of the multiple of doors (66) matches each of the multiple of ports (62) such that a fan nacelle trailing edge (34S) is continuous when the second fan nacelle section (54) is selectively translated to a closed position relative to the first fan nacelle section (52).",
  "title": "Gas turbine engine with variable area fan nozzle and method of operating a variable area fan nozzle"
}