{
  "$type": "site.standard.document",
  "description": "A method for operating a gas turbine engine (10) includes channeling compressed airflow (53) discharged from a first compressor (14) through an intercooler (50) having a cooling medium flowing therethrough, channeling a working fluid (72) through the intercooler to facilitate increasing an…",
  "path": "/patents/1072141",
  "publishedAt": "2005-11-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/305",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method for operating a gas turbine engine (10) includes channeling compressed airflow (53) discharged from a first compressor (14) through an intercooler (50) having a cooling medium flowing therethrough, channeling a working fluid (72) through the intercooler to facilitate increasing an operating temperature of the working fluid, and channeling the discharged working fluid to a combustor (18) to facilitate increasing an operating efficiency of the gas turbine engine.",
  "title": "Intercooler system for gas turbine engines"
}