{
  "$type": "site.standard.document",
  "description": "A method of startup control for a gas turbine system that is operating in a fired deceleration shutdown process mode (24) is provided. The method includes determining whether the combustor flame is in a lit state (26). Also included is increasing a fuel flow to the gas turbine system if the…",
  "path": "/patents/983916",
  "publishedAt": "2013-10-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/26",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method of startup control for a gas turbine system that is operating in a fired deceleration shutdown process mode (24) is provided. The method includes determining whether the combustor flame is in a lit state (26). Also included is increasing a fuel flow to the gas turbine system if the combustor is determined to be in the lit state (26). Further included is initiating (28) a starter system to the gas turbine system.",
  "title": "Method of startup control for a gas turbine system operating in a fired deceleration shutdown process mode"
}