{
  "$type": "site.standard.document",
  "description": "A gas turbine combustor system comprising plural combustors and plural fuel supply systems realizes a combustion of a lean and uniform pre-mixture in each of the combustors to thereby enable to reduce NOx generation. Flow regulating valves (29,30) are provided in fuel supply systems (23,24)…",
  "path": "/patents/1097970",
  "publishedAt": "2003-03-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/228",
    "MITSUBISHI HEAVY IND LTD [JP]"
  ],
  "textContent": "A gas turbine combustor system comprising plural combustors and plural fuel supply systems realizes a combustion of a lean and uniform pre-mixture in each of the combustors to thereby enable to reduce NOx generation. Flow regulating valves (29,30) are provided in fuel supply systems (23,24), respectively, that supply combustors (25,26) with fuel. Pressure gauges (31,32) are provided in the fuel supply systems (23,24), respectively, in front of inlets of the combustors (25,26). The flow regulating valves (29,30) are controlled so that pressures measured by the pressure gauges (31,32) become the same.",
  "title": "Gas turbine combustor system"
}