{
  "$type": "site.standard.document",
  "description": "A land based gas turbine apparatus includes an integral compressor (110, 210); a turbine (114, 214) having a combustor (112, 212) to which air from the integral compressor and fuel are supplied; and a generator (132) operatively connected to the turbine for generating electricity; wherein hot gas…",
  "path": "/patents/1109023",
  "publishedAt": "2001-10-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A land based gas turbine apparatus includes an integral compressor (110, 210); a turbine (114, 214) having a combustor (112, 212) to which air from the integral compressor and fuel are supplied; and a generator (132) operatively connected to the turbine for generating electricity; wherein hot gas path component parts in the turbine are cooled entirely or at least partially by cooling air supplied by an external compressor (136, 236). A method is also provided which includes the steps of supplying at least a portion of the cooling air to the hot gas path parts in the turbine (114, 214) from the integral compressor (110, 210); and supplying a remaining portion of the cooling air from an external compressor (136, 236).",
  "title": "Combustion turbine cooling media supply system and related method"
}