{
  "$type": "site.standard.document",
  "description": "Gas turbine aero engine provided with core flow bypass (74,66) between the HP and LP turbines, regulation valve (62) and an auxiliary turbine (60). When high trust is required, the valve (62) is open and auxiliary turbine (60) supply extra power to the compressor (32).",
  "path": "/patents/1000648",
  "publishedAt": "2012-07-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C1/007",
    "ROLLS ROYCE NAM TECH INC [US]"
  ],
  "textContent": "Gas turbine aero engine provided with core flow bypass (74,66) between the HP and LP turbines, regulation valve (62) and an auxiliary turbine (60). When high trust is required, the valve (62) is open and auxiliary turbine (60) supply extra power to the compressor (32).",
  "title": "Variable cycle gas turbine engine"
}