{
  "$type": "site.standard.document",
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  "description": "A combustor (108) for a gas turbine engine (100) includes a combustor liner (110), a fuel swirler (118) integral and conformal with the combustor liner (110) to provide an outlet (132) for fuel into the combustor (108), and a dilution chute (114) surrounding the fuel swirler outlet (132) and…",
  "path": "/patents/1418968",
  "publishedAt": "2024-07-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B22F5/009",
    "RTX CORP [US]"
  ],
  "textContent": "A combustor (108) for a gas turbine engine (100) includes a combustor liner (110), a fuel swirler (118) integral and conformal with the combustor liner (110) to provide an outlet (132) for fuel into the combustor (108), and a dilution chute (114) surrounding the fuel swirler outlet (132) and extending into the combustor (108) to provide a wetting surface for fuel exiting the fuel swirler (118).",
  "title": "GAS TURBINE COMBUSTOR WITH INTEGRATED FUEL SWIRLERS"
}