{
  "$type": "site.standard.document",
  "description": "Liquid fuel assist ignition system (1) for providing a fuel-air mixture to a gas turbine in its start-up phase, comprising a high pressure tank (2), a vacuum pump (3) connected to the high pressure tank (2), a liquid fuel inlet (4) connected to the high pressure tank (2), an air inlet (5) connected…",
  "path": "/patents/999524",
  "publishedAt": "2012-08-08T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/24",
    "SIEMENS AG [DE]"
  ],
  "textContent": "Liquid fuel assist ignition system (1) for providing a fuel-air mixture to a gas turbine in its start-up phase, comprising a high pressure tank (2), a vacuum pump (3) connected to the high pressure tank (2), a liquid fuel inlet (4) connected to the high pressure tank (2), an air inlet (5) connected to the high pressure tank (2) and an outlet (6) connected to a burner of the gas turbine (20); and method to provide a fuel/air mixture to a gas turbine (20) in its start-up phase using a liquid fuel assist ignition system (1).",
  "title": "Liquid fuel assist ignition system of a gas turbine and method to provide a fuel/air mixture to a gas turbine"
}