{
  "$type": "site.standard.document",
  "description": "A method (200) includes determining a current burn flow value of a turbine engine (205), measuring a fuel pressure of a metered fuel flow of liquid fuel to a combustor of the turbine engine at a measurement point in a fuel system upstream of the combustor (210) and determining a current burner…",
  "path": "/patents/1416579",
  "publishedAt": "2026-06-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/22",
    "RTX CORP [US]"
  ],
  "textContent": "A method (200) includes determining a current burn flow value of a turbine engine (205), measuring a fuel pressure of a metered fuel flow of liquid fuel to a combustor of the turbine engine at a measurement point in a fuel system upstream of the combustor (210) and determining a current burner pressure as a function of the measured fuel pressure and the current burn flow value (215).",
  "title": "BURNER PRESSURE SYNTHESIS FROM FUEL SYSTEM PRESSURE"
}