{
  "$type": "site.standard.document",
  "description": "A method for controlling a sequential combustor (10) of a gas turbine engine (2) includes the method comprising supplying the first combustor stage (12) of the sequential combustor (10) with a first air/fuel mixture (M1) and supplying a second combustor stage (13) of the sequential combustor (10)…",
  "path": "/patents/1391538",
  "publishedAt": "2025-08-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/26",
    "ANSALDO ENERGIA SWITZERLAND AG [CH]"
  ],
  "textContent": "A method for controlling a sequential combustor (10) of a gas turbine engine (2) includes the method comprising supplying the first combustor stage (12) of the sequential combustor (10) with a first air/fuel mixture (M1) and supplying a second combustor stage (13) of the sequential combustor (10) with a second air/fuel mixture (M2). The first air/fuel mixture (M1) contains ammonia and is stoichiometric or sub-stoichiometric.",
  "title": "METHOD FOR CONTROLLING A SEQUENTIAL COMBUSTOR OF A GAS TURBINE ENGINE AND GAS TURBINE POWER PLANT"
}