{
  "$type": "site.standard.document",
  "description": "A fuel nozzle assembly (48) for a gas turbine engine (10) is provided, the fuel nozzle assembly (48) comprising a first shaft (84) including a first fluid passage (100); a flange (82) connected to the first shaft (84) and including a second fluid passage (102) fluidly coupled with the first fluid…",
  "path": "/patents/965282",
  "publishedAt": "2026-05-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "GE MARMARA TECH CENTER MUHENDISLIK HIZMETLERI LTD [TR]"
  ],
  "textContent": "A fuel nozzle assembly (48) for a gas turbine engine (10) is provided, the fuel nozzle assembly (48) comprising a first shaft (84) including a first fluid passage (100); a flange (82) connected to the first shaft (84) and including a second fluid passage (102) fluidly coupled with the first fluid passage (100); a nozzle tube (70) connected to the flange (82) and including a third fluid passage (104) fluidly coupled with the second fluid passage (102), the nozzle tube (70) disposed at a first side of the flange (82); and a second shaft (86) connected to the flange (82), the first shaft (84) disposed at least partially in the second shaft (86). The flange (82), the first shaft (84), and the second shaft (86) at least partially define a leak path (LP). The leak path (LP) includes a radial gap (212) between the first shaft (84) and the second shaft (86); and a leak channel (154) in an axial surface (156) of at least one of the first shaft (84) or the second shaft (86).",
  "title": "GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR"
}