{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "A gas turbine (10) includes a compressor (12), a combustor (14) downstream from the compressor (12) and a heat transfer system (30), wherein the heat transfer system (30) receives a compressed working fluid (22) from the compressor (12). A fluid coupling (34) between the heat transfer system (32)…",
  "path": "/patents/988877",
  "publishedAt": "2013-07-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C6/08",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A gas turbine (10) includes a compressor (12), a combustor (14) downstream from the compressor (12) and a heat transfer system (30), wherein the heat transfer system (30) receives a compressed working fluid (22) from the compressor (12). A fluid coupling (34) between the heat transfer system (32) and the combustor (14), wherein the fluid coupling (34) receives the compressed working fluid (22) from the heat transfer system (30). A conditioner (36) in fluid communication with the compressor (12) and a fluid coupling (34) between the heat transfer system (30) and the conditioner (36), wherein the fluid coupling (34) receives a cooling media from the heat transfer system. A method for operating the gas turbine (10) includes flowing a compressed working fluid (22) from the compressor (12) to the heat transfer system (30), transferring heat energy from the compressed working fluid (22) to the heat transfer system (30), flowing the compressed working fluid (22) from the heat transfer system (30) to a combustor (14), and flowing a cooling media from the heat transfer system (30) to a compressor inlet (20).",
  "title": "A method and apparatus for operating a gas turbine engine"
}