{
  "$type": "site.standard.document",
  "description": "A gas turbine engine 10 includes a first fan, a second fan spaced axially from the first fan, a turbine-driven fan shaft 26 and an epicyclic gear train 22 coupled to be driven by the turbine-driven fan shaft and coupled to drive the first fan and the second fan. The epicyclic gear train 22 includes…",
  "path": "/patents/984663",
  "publishedAt": "2013-07-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/107",
    "UNITED TECHNOLOGIES CORP [US]"
  ],
  "textContent": "A gas turbine engine 10 includes a first fan, a second fan spaced axially from the first fan, a turbine-driven fan shaft 26 and an epicyclic gear train 22 coupled to be driven by the turbine-driven fan shaft and coupled to drive the first fan and the second fan. The epicyclic gear train 22 includes a carrier 88 that supports star gears that mesh with a sun gear, and a ring gear that surrounds and meshes with the star gears. The star gears are supported on respective journal bearings.",
  "title": "Turbine engine"
}