{
  "$type": "site.standard.document",
  "description": "A nozzle assembly, a combustor (100) using the same, and a gas turbine . The nozzle assembly is configured to inject fuel and compressed air into a combustion chamber of a combustor of a gas turbine, and includes a hollow nozzle frame (1410) , a mixture supply tube (1420) having a plurality of…",
  "path": "/patents/1391532",
  "publishedAt": "2026-04-22T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "DOOSAN ENERBILITY CO LTD [KR]"
  ],
  "textContent": "A nozzle assembly, a combustor (100) using the same, and a gas turbine . The nozzle assembly is configured to inject fuel and compressed air into a combustion chamber of a combustor of a gas turbine, and includes a hollow nozzle frame (1410) , a mixture supply tube (1420) having a plurality of tubes (1421) configured to supply a mixture of air and fuel to the combustion chamber, a fuel supply part (1440) configured to supply fuel to the mixture supply tube, an air supply part (1440) configured to supply air to the mixture supply tube, and a mixing part (1450) including an injection member (1451) formed in each of the tubes and configured to inject fuel supplied from the fuel supply part toward air passing through the tube, and a swirl vane (1452) formed on one side of the injection member and configured to mix fuel and air passing through the injection member.",
  "title": "NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE INCLUDING SAME"
}