{
  "$type": "site.standard.document",
  "description": "The invention relates to a premix burner (10) of the multi-cone type for a gas turbine, comprising a plurality of shells (16a-d), which are arranged around a central burner axis (11) and are parts of a virtual, axially extending common cone, which opens in a downstream direction, whereby said parts…",
  "path": "/patents/979604",
  "publishedAt": "2014-01-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/00",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The invention relates to a premix burner (10) of the multi-cone type for a gas turbine, comprising a plurality of shells (16a-d), which are arranged around a central burner axis (11) and are parts of a virtual, axially extending common cone, which opens in a downstream direction, whereby said parts are displaced perpendicular to said burner axis (11) such that a tangential slot (17) is defined between each pair of adjacent shells (16a-d). The flame front of such a burner (10) is stabilized by providing a virtual common cone with a cone angle, which varies in axial direction.",
  "title": "Premix burner of the multi-cone type for a gas turbine"
}