{
  "$type": "site.standard.document",
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  "description": "A method of operation of a gas turbine engine system and a gas turbine engine system (50,120,130,200) are provided that include a first gas turbine engine (52). The first gas turbine engine (52) has a first compressor (80) configured to intake air and to produce a first compressed air (14) and a…",
  "path": "/patents/1007524",
  "publishedAt": "2011-11-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/34",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method of operation of a gas turbine engine system and a gas turbine engine system (50,120,130,200) are provided that include a first gas turbine engine (52). The first gas turbine engine (52) has a first compressor (80) configured to intake air and to produce a first compressed air (14) and a first combustor (88) configured to combust a first mixture to produce a first combustion gas. The first mixture has a first fuel, at least a first portion of the first compressed air (14), and a second combustion gas (24) from a second gas turbine engine (10). The first gas turbine engine (52) also includes a first turbine (92) configured to extract work from the first combustion gas.",
  "title": "Gas turbine engine system and operation method for exhaust gas use in gas turbine engines"
}