{
  "$type": "site.standard.document",
  "description": "A system includes a turbine fuel nozzle assembly (39). The turbine fuel nozzle assembly (39) includes a first fuel nozzle (12, 42, 44) including a first air inlet (62) and a second fuel nozzle (12, 42, 44) including a second air inlet (62). The turbine fuel nozzle assembly (39) also includes a…",
  "path": "/patents/993363",
  "publishedAt": "2013-01-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/2365",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A system includes a turbine fuel nozzle assembly (39). The turbine fuel nozzle assembly (39) includes a first fuel nozzle (12, 42, 44) including a first air inlet (62) and a second fuel nozzle (12, 42, 44) including a second air inlet (62). The turbine fuel nozzle assembly (39) also includes a first inlet flow conditioner (64) disposed adjacent the first air inlet (62) of the first fuel nozzle (12, 42, 44), wherein the first air inlet flow conditioner (64) extends only partially around the first fuel nozzle (12, 42, 44). The turbine fuel nozzle assembly (39) further includes a second inlet flow conditioner (64) disposed adjacent the second air inlet (62) of the second fuel nozzle (12, 42, 44), wherein the second air inlet flow conditioner (64) extends only partially around the second fuel nozzle (12, 42, 44), and the second inlet flow conditioner (64) is separate from the first inlet flow conditioner (64).",
  "title": "System for conditioning air flow into a multi-nozzle assembly"
}