{
  "$type": "site.standard.document",
  "description": "A system includes a gas turbine system (10) including a compressor (16), a combustor (18), a turbine (22), and an exhaust section (24). The system also includes multiple sensors (40) coupled to components of the gas turbine system (10). The system further includes a controller (38) communicatively…",
  "path": "/patents/1401339",
  "publishedAt": "2024-11-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/20",
    "GENERAL ELECTRIC TECHNOLOGY GMBH [CH]"
  ],
  "textContent": "A system includes a gas turbine system (10) including a compressor (16), a combustor (18), a turbine (22), and an exhaust section (24). The system also includes multiple sensors (40) coupled to components of the gas turbine system (10). The system further includes a controller (38) communicatively coupled to the gas turbine system (10) and the multiple sensors (40) and configured to control operations of the gas turbine system (10), wherein the controller (3 8) is configured to calculate a surrogate value for turbine exit Mach number based on the feedback from the multiple sensors (40) and to utilize the surrogate value to derive a control action for the gas turbine system (10).",
  "title": "SYSTEM AND METHOD FOR NON-MODEL BASED CONTROL UTILIZING TURBINE EXIT MACH NUMBER SURROGATE"
}