{
  "$type": "site.standard.document",
  "description": "An exemplary embodiment of a FLADE (fan on blade) counter-rotating fan aircraft gas turbine engine includes at least one row of FLADE fan blades (5) disposed radially outwardly of and drivingly connected to one of axially spaced-apart first and second counter-rotatable fans (130 and 132). A core…",
  "path": "/patents/1079678",
  "publishedAt": "2005-03-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02K3/072",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "An exemplary embodiment of a FLADE (fan on blade) counter-rotating fan aircraft gas turbine engine includes at least one row of FLADE fan blades (5) disposed radially outwardly of and drivingly connected to one of axially spaced-apart first and second counter-rotatable fans (130 and 132). A core engine (18) located downstream and axially aft of the first and second counter-rotatable fans (130 and 132) is circumscribed by a fan bypass duct (40) downstream and axially aft of the first and second counter-rotatable fans (130 and 132). The row of FLADE fan blades (5) radially extend across a FLADE duct (3) circumscribed about the first and second counter-rotatable fans (130 and 132) and the fan bypass duct (40). A second low pressure turbine (21) is drivingly connected to the first counter-rotatable fan (130) and a first low pressure turbine (19) is drivingly connected to the second counter-rotatable fan (132).",
  "title": "Gas turbine engine with counter-rotating fan blades"
}