{
  "$type": "site.standard.document",
  "description": "An assembly (64) is provided for a gas turbine engine (20). This assembly (64) includes a fuel injector (62). The fuel injector (62) includes a nozzle (80) and a plurality of discrete fuel circuits (90). The discrete fuel circuits (90) include a first fuel circuit (90A), a second fuel circuit (90B)…",
  "path": "/patents/1393260",
  "publishedAt": "2025-05-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/263",
    "RTX CORP [US]"
  ],
  "textContent": "An assembly (64) is provided for a gas turbine engine (20). This assembly (64) includes a fuel injector (62). The fuel injector (62) includes a nozzle (80) and a plurality of discrete fuel circuits (90). The discrete fuel circuits (90) include a first fuel circuit (90A), a second fuel circuit (90B) and a third fuel circuit (90C). The nozzle (80) extends axially along an axis (84) to a nozzle tip (86). The first fuel circuit (90A) includes a first fuel outlet (94A) disposed at the nozzle tip (86). The second fuel circuit (90B) includes a plurality of second fuel outlets (94B) arranged circumferentially about the axis (84) at the nozzle tip (86) in a second fuel outlet array. The third fuel circuit (90C) includes a plurality of third fuel outlets (94C) arranged circumferentially about the axis (84) at the nozzle tip (86) in a third fuel outlet array.",
  "title": "GAS TURBINE ENGINE FUEL INJECTOR WITH MULTIPLE FUEL CIRCUITS"
}