{
  "$type": "site.standard.document",
  "description": "A gas turbine engine has in flow series: a compressor section (10), a combustion chamber (12), and a turbine section (13). The engine further has a steam generator (16). The combustion chamber (12) has a steam reservoir (11) located at the upstream end thereof. The steam reservoir (11) receives…",
  "path": "/patents/985809",
  "publishedAt": "2013-03-06T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/30",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A gas turbine engine has in flow series: a compressor section (10), a combustion chamber (12), and a turbine section (13). The engine further has a steam generator (16). The combustion chamber (12) has a steam reservoir (11) located at the upstream end thereof. The steam reservoir (11) receives steam from the steam generator (16), and delivers the received steam into a combustion zone of the combustion chamber (12).",
  "title": "Steam injected gas turbine engine"
}