{
  "$type": "site.standard.document",
  "description": "The method involves forming derivation of hot gas temperature at different areas of a gas turbine (10) over pressure measurements by pressure sensors (P1-P3). The pressure measurements are executed in a hot gas flow produced in a combustion chamber (13) of the turbine and directly before a blade…",
  "path": "/patents/1002799",
  "publishedAt": "2012-05-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/28",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The method involves forming derivation of hot gas temperature at different areas of a gas turbine (10) over pressure measurements by pressure sensors (P1-P3). The pressure measurements are executed in a hot gas flow produced in a combustion chamber (13) of the turbine and directly before a blade series of the turbine. A pressure drop is determined between measuring positions that lie downstream to fire (18) present in the chamber. A turbine flange (14) is arranged in the turbine at a transition between the chamber and the turbine. An independent claim is also included for a gas turbine for executing a regulation method.",
  "title": "Method for controlling a gas turbine and gas turbine for implementing the method"
}