{
  "$type": "site.standard.document",
  "description": "Turbojet engine comprising a compressor (1), a combustion chamber (2), and at least one turbine (6) receiving the combustion gases, characterized in that it comprises a precombustion chamber (3) comprising means for supplying an oxidizer and a fuel (4,5), and a means (7) for conveying the…",
  "path": "/patents/1108088",
  "publishedAt": "2001-12-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D1/24",
    "BREGENTZER DANIEL [BE]"
  ],
  "textContent": "Turbojet engine comprising a compressor (1), a combustion chamber (2), and at least one turbine (6) receiving the combustion gases, characterized in that it comprises a precombustion chamber (3) comprising means for supplying an oxidizer and a fuel (4,5), and a means (7) for conveying the combustion gases from the precombustion chamber into the combustion chamber, and in that it comprises a means (18) for directing at least a portion of the main flow (FP) of compressed air coming from the compressor (1) into the combustion chamber, said means (18) being arranged relative to the means (7) for conveying the combustion gases from the precombustion chamber (3) into the combustion chamber (2) in such a manner that at least a portion of the main flow (FP) creates a suction of the combustion gases from the precombustion chamber (3).",
  "title": "Gas turbine engine"
}