{
  "$type": "site.standard.document",
  "description": "A gas turbine fuel control method and device controls a lift amount of a pressure control valve. Values such as a pressure for supplying fuel gas to a gas turbine, a pressure in a combustor casing of the gas turbine, an output of a generator connected to the gas turbine, and a controlled output for…",
  "path": "/patents/1096042",
  "publishedAt": "2003-05-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/28",
    "MITSUBISHI HEAVY IND LTD [JP]"
  ],
  "textContent": "A gas turbine fuel control method and device controls a lift amount of a pressure control valve. Values such as a pressure for supplying fuel gas to a gas turbine, a pressure in a combustor casing of the gas turbine, an output of a generator connected to the gas turbine, and a controlled output for a flow rate control valve are detected by sensors. The detected values are input into a control device. A differential pressure across the flow rate control valve and a target value of the differential pressure are also input into the control device. The control device performs a desired arithmetic operation based on these input values to output a lift instruction for the pressure control valve.",
  "title": "Method of and device for controlling fuel for gas turbine"
}