{
  "$type": "site.standard.document",
  "description": "The aircraft engine has one-or multi-stage compressor arrangement (V), downstream combustion chamber (BK), one or multi-stage turbine assembly (HT,NT), compressor heat exchanger arrangement (WV), turbine heat exchanger arrangement (WT) and by-pass unit (BY). The by-pass unit is provided for…",
  "path": "/patents/986670",
  "publishedAt": "2013-09-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C3/04",
    "MTU AERO ENGINES AG [DE]"
  ],
  "textContent": "The aircraft engine has one-or multi-stage compressor arrangement (V), downstream combustion chamber (BK), one or multi-stage turbine assembly (HT,NT), compressor heat exchanger arrangement (WV), turbine heat exchanger arrangement (WT) and by-pass unit (BY). The by-pass unit is provided for selectively by-passing or guiding the working medium with respect to turbine heat exchanger arrangement. An independent claim is included for method for operating aircraft engine.",
  "title": "Aircraft engine"
}