{
  "$type": "site.standard.document",
  "description": "A gas turbine (10) includes a plurality of combustion chambers (14); at least one fuel nozzle (16, 18, 20) for each of the combustion chambers; at least one fuel line (34, 36, 38) for each fuel nozzle in each of the combustion chambers; at least one heat exchanger (28, 30, 32) for each fuel line…",
  "path": "/patents/993808",
  "publishedAt": "2013-01-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/224",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine (10) includes a plurality of combustion chambers (14); at least one fuel nozzle (16, 18, 20) for each of the combustion chambers; at least one fuel line (34, 36, 38) for each fuel nozzle in each of the combustion chambers; at least one heat exchanger (28, 30, 32) for each fuel line configured to adjust a temperature of a fuel flow to each fuel nozzle; and a controller (50) configured to control each of the heat exchangers to reduce temperature variations amongst the combustion chambers.",
  "title": "Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation"
}