{
  "$type": "site.standard.document",
  "description": "The assembly has a low pressure turbine with a flowpath and located aft of a high pressure spool (33). The low pressure turbine has counter rotatable low pressure inner and outer rotatable turbines. A single direction rotation booster has a row of booster blades connected to a low pressure outer…",
  "path": "/patents/1088481",
  "publishedAt": "2004-03-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D1/24",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "The assembly has a low pressure turbine with a flowpath and located aft of a high pressure spool (33). The low pressure turbine has counter rotatable low pressure inner and outer rotatable turbines. A single direction rotation booster has a row of booster blades connected to a low pressure outer shaft and axially located aft and downstream of a fan blade row (15).",
  "title": "Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and single direction of rotation booster aft of counter rotating fans"
}