{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (100) comprises a fan drive turbine (46) driving a shaft (108). The shaft (108) engages a gear reduction (105). The gear reduction (105) drives a fan rotor (102) at a speed that is less than the speed of the fan drive turbine (46). The gear reduction (105) is a non-epicyclic…",
  "path": "/patents/1423946",
  "publishedAt": "2024-02-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/107",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (100) comprises a fan drive turbine (46) driving a shaft (108). The shaft (108) engages a gear reduction (105). The gear reduction (105) drives a fan rotor (102) at a speed that is less than the speed of the fan drive turbine (46). The gear reduction (105) is a non-epicyclic gear reduction.",
  "title": "GEARED TURBOFAN WITH NON-EPICYCLIC GEAR REDUCTION SYSTEM"
}