{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (10) comprising a compressor (20), a combustion chamber (30) and a turbine (40) arranged in flow series, wherein the gas turbine engine further comprises: one or more combustion zones; a source of steam (60) configured to deliver steam to the combustion chamber; and a liquid…",
  "path": "/patents/996092",
  "publishedAt": "2012-11-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/305",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A gas turbine engine (10) comprising a compressor (20), a combustion chamber (30) and a turbine (40) arranged in flow series, wherein the gas turbine engine further comprises: one or more combustion zones; a source of steam (60) configured to deliver steam to the combustion chamber; and a liquid water delivery system (100) configured to selectively provide liquid water to one or more of the combustion zones after a start up period of the gas turbine engine. A method of generating power with a gas turbine engine (10), the gas turbine engine comprising a compressor (20), a combustion chamber (30) and a turbine (40) arranged in flow series, wherein the method comprises: selectively delivering steam from a source of steam (60) to the combustion chamber; and providing liquid water to one or more combustion zones after a start up period of the gas turbine engine.",
  "title": "A steam injected gas turbine engine"
}