{
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  "description": "The gas turbine (1) comprises a compressor (2) that compresses an oxidiser containing flow and supplies it to at least a combustion chamber (3, 7), wherein a fuel is injected and a mixture formed; the mixture is then combusted generating a flue flow that is expanded in a turbine (8). The flue flow…",
  "path": "/patents/1015461",
  "publishedAt": "2011-02-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C1/08",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The gas turbine (1) comprises a compressor (2) that compresses an oxidiser containing flow and supplies it to at least a combustion chamber (3, 7), wherein a fuel is injected and a mixture formed; the mixture is then combusted generating a flue flow that is expanded in a turbine (8). The flue flow downstream of the a turbine (8) is diverted in a first flue flow (9) that is mixed with an air flow (12) to generate the oxidiser containing flow that is fed to the compressor (2), and a second flue flow (13) that is fed to a CO 2 capture unit (15). One or more combustion chambers (3, 7) have injectors (20) arranged to locally inject a pilot oxidiser in a zone of the combustion chamber (3, 7) where a flame (21) is housed. The present invention also refers to a method for operating a gas turbine.",
  "title": "Gas turbine and method for operating a gas turbine"
}