{
  "$type": "site.standard.document",
  "description": "At least one main air compressor (12) makes a compressed ambient gas flow (26). The compressed ambient gas flow (26) is delivered to a turbine combustor (32) at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor (32) from a turbine…",
  "path": "/patents/992654",
  "publishedAt": "2013-02-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/34",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "At least one main air compressor (12) makes a compressed ambient gas flow (26). The compressed ambient gas flow (26) is delivered to a turbine combustor (32) at a pressure that is greater than or substantially equal to an output pressure delivered to the turbine combustor (32) from a turbine compressor (30) as at least a first portion of a recirculated gas flow (50). A fuel stream (28) is delivered to the turbine combustor (32), and a combustible mixture is formed and burned, forming the recirculated gas flow (50). A turbine power is produced that is substantially equal to at least a power required to rotate the turbine compressor (30). At least a portion of the recirculated gas flow (50) is recirculated through a recirculation loop (52). An excess portion of the recirculated gas flow (50) is vented or a portion of the turbine compressor exhaust (44) bypasses the turbine combustor (32) or both.",
  "title": "Method of operating a power plant"
}