{
  "$type": "site.standard.document",
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  "description": "A nozzle assembly (40) for a gas turbine engine (10), comprising: a nozzle (80) at a downstream end of the assembly (40) relative to fuel flow (50); a first and a second body (60, 70) upstream of the nozzle (80), the first body (60) defining a first passage (68) between a first inlet (68a)…",
  "path": "/patents/1409306",
  "publishedAt": "2025-11-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A nozzle assembly (40) for a gas turbine engine (10), comprising: a nozzle (80) at a downstream end of the assembly (40) relative to fuel flow (50); a first and a second body (60, 70) upstream of the nozzle (80), the first body (60) defining a first passage (68) between a first inlet (68a) connectable to a source and a first outlet (68b), and the second body (70) defining a second passage (78) between a second inlet (78a) and a second outlet (78b) in fluid communication with the nozzle (80), the first outlet and second inlet (68b, 72a) in fluid communication with each other; the bodies (60, 70) matingly engaged together along an axis (E), the first outlet and second inlet (68b, 72a) spaced apart relative to the axis (E) to define a gallery (52) having a depth in an axial direction and a width in a transverse direction; and a gap filler (100) within the gallery (52), compressible in at least one of the directions, having an uncompressed dimension greater than a corresponding dimension of the gallery (52) in the at least one of the directions.",
  "title": "FUEL NOZZLE ASSEMBLY WITH GAP FILLER"
}