{
  "$type": "site.standard.document",
  "description": "The turbofan gas assembly (10) has a low-pressure turbine with low-pressure turbine flowpath and located aft high-pressure spool. The turbine with counter rotatable low pressure inner and outer shaft turbines. A single direction of rotation booster (16) with rotatable row of booster blades…",
  "path": "/patents/1088504",
  "publishedAt": "2004-03-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/067",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The turbofan gas assembly (10) has a low-pressure turbine with low-pressure turbine flowpath and located aft high-pressure spool. The turbine with counter rotatable low pressure inner and outer shaft turbines. A single direction of rotation booster (16) with rotatable row of booster blades (116,117) is drivenly connected to low-pressure outer shaft and axially located aft and down stream of aft fan blade row (13,15).",
  "title": "Counter rotating fan aircraft gas turbine engine with aft booster"
}