{
  "$type": "site.standard.document",
  "description": "The gas turbine (10) has compressors (12,14) for supplying compressed combustion air to a combustion chamber (20). The compressors are provided with intercooler (16) for precooling the supplied combustion air. A radiation-heat transfer agent is designed as an evaporation cooler. Fuel gas is…",
  "path": "/patents/1071392",
  "publishedAt": "2005-12-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01K21/047",
    "SIEMENS AG [DE]"
  ],
  "textContent": "The gas turbine (10) has compressors (12,14) for supplying compressed combustion air to a combustion chamber (20). The compressors are provided with intercooler (16) for precooling the supplied combustion air. A radiation-heat transfer agent is designed as an evaporation cooler. Fuel gas is supplied from the chamber to a turbine (22). A recuperator (18) preheats the combustion air using warm fuel gases.",
  "title": "Gasturbine with compressor and recuperator"
}