{
  "$type": "site.standard.document",
  "description": "The invention discloses a method for operating a gas turbine (10) with sequential combustion (14, 15, 17, 19), which gas turbine (10) comprises a compressor (13), a first combustor (14, 17) with a first combustion chamber (14) and first burners (17), which receives compressed air from the…",
  "path": "/patents/975752",
  "publishedAt": "2014-04-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/12",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The invention discloses a method for operating a gas turbine (10) with sequential combustion (14, 15, 17, 19), which gas turbine (10) comprises a compressor (13), a first combustor (14, 17) with a first combustion chamber (14) and first burners (17), which receives compressed air from the compressor (13), a second combustor (15, 19) with a second combustion chamber (15) and second burners (19), which receives hot gas from the first combustor (14, 17) with a predetermined second combustor inlet temperature, and a turbine (16), which receives hot gas from the second combustor (15, 19). The CO emission for part-load operation is reduced by reducing the second combustor inlet temperature for base-load operation of the gas turbine (10), and increasing the second combustor inlet temperature when decreasing the gas turbine load (RL GT ) from base-load to part-load.",
  "title": "Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method"
}