{
  "$type": "site.standard.document",
  "description": "A method (200) of controlling an operating temperature of a first combustion zone (115) of a combustor (106) of a rotary machine (100) includes determining a current operating temperature and a target operating temperature of a first combustion zone (115) using a digital simulation. The method…",
  "path": "/patents/1414895",
  "publishedAt": "2023-12-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/222",
    "GENERAL ELECTRIC TECHNOLOGY GMBH [CH]"
  ],
  "textContent": "A method (200) of controlling an operating temperature of a first combustion zone (115) of a combustor (106) of a rotary machine (100) includes determining a current operating temperature and a target operating temperature of a first combustion zone (115) using a digital simulation. The method (200) further includes determining a derivative (408) of the current operating temperature with respect to a current fuel split using the digital simulation. The fuel split apportions a total flow of fuel to the combustor (106) between the first combustion zone (115) and a second combustion zone (117). The method (200) also includes calculating a calculated fuel split (410) that results in a calculated operating temperature approaching the target operating temperature. The method (200) further includes channeling a first flow of fuel to the first combustion zone (115) and a second flow of fuel to the second combustion zone (117).",
  "title": "SYSTEMS AND METHODS FOR DETERMINATION OF GAS TURBINE FUEL SPLIT FOR HEAD END TEMPERATURE CONTROL"
}