{
  "$type": "site.standard.document",
  "description": "The intercooling method is for a gas turbine engine with first (1) and second (2) compressor stages and a combustion chamber (3) and turbine (4). The intercooler (9) is positioned between the two compressor stages. The intercooler is at least partially or largely isotropic. The cooling can occur at…",
  "path": "/patents/1090648",
  "publishedAt": "2004-01-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/143",
    "ALSTOM SWITZERLAND LTD [CH]"
  ],
  "textContent": "The intercooling method is for a gas turbine engine with first (1) and second (2) compressor stages and a combustion chamber (3) and turbine (4). The intercooler (9) is positioned between the two compressor stages. The intercooler is at least partially or largely isotropic. The cooling can occur at a flow point in the intercooler with a higher Mach number than the cooler inlet. Claims include a gas turbine using the method.",
  "title": "Intercooling process and intercooled gas turbine engine"
}