{
  "$type": "site.standard.document",
  "description": "The gas turbine (1) has a bleed air system (4) for the compressor (2), a tap (5) on the housing (3) of the compressor and a bleed air outlet (6). A bleed-air chamber (7) is formed between the tap and the bleed air outlet. The bleed air system has a device, by which a part of the bleed air (L) is…",
  "path": "/patents/1009757",
  "publishedAt": "2011-08-31T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/105",
    "ROLLS ROYCE DEUTSCHLAND [DE]"
  ],
  "textContent": "The gas turbine (1) has a bleed air system (4) for the compressor (2), a tap (5) on the housing (3) of the compressor and a bleed air outlet (6). A bleed-air chamber (7) is formed between the tap and the bleed air outlet. The bleed air system has a device, by which a part of the bleed air (L) is passed out in partial mass flow from the tap.",
  "title": "Gas turbine with a bleed air device for the compressor"
}