{
  "$type": "site.standard.document",
  "description": "The gas turbine engine arrangement (10) comprises a compressor (11), a combustion chamber (12) and a turbine (13) connected one another. A casing (14) housing the compressor (11) has flanges (16) connectable to pipes (17) providing secondary air to the combustion chamber (12) and/or turbine (13)…",
  "path": "/patents/1005853",
  "publishedAt": "2012-01-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/243",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The gas turbine engine arrangement (10) comprises a compressor (11), a combustion chamber (12) and a turbine (13) connected one another. A casing (14) housing the compressor (11) has flanges (16) connectable to pipes (17) providing secondary air to the combustion chamber (12) and/or turbine (13). The flanges (16) define passages having an asymmetric cross section. A method for retrofitting a gas turbine engine arrangement (10) is also disclosed.",
  "title": "Gas turbine engine flange arrangement and method for retrofitting same"
}