{
  "$type": "site.standard.document",
  "description": "A transition duct for a can combustor of a gas turbine assembly for power plant; the transition duct being a tubular assembly comprising a first end configured for being coupled to a combustion chamber of the can combustor and a second end configured for being coupled to a turbine of the gas…",
  "path": "/patents/1409829",
  "publishedAt": "2024-05-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "ANSALDO ENERGIA SWITZERLAND AG [CH]"
  ],
  "textContent": "A transition duct for a can combustor of a gas turbine assembly for power plant; the transition duct being a tubular assembly comprising a first end configured for being coupled to a combustion chamber of the can combustor and a second end configured for being coupled to a turbine of the gas turbine assembly; the transition duct comprising: an inner tubular body having an inner surface in contact with the hot gas and an outer surface; an outer tubular body having an inner surface and an outer surface in contact with cooling air; wherein a gap is present between the inner tubular body and the outer tubular body forming a cooling channel defined by the outer surface of the inner tubular body and the inner surface of the outer tubular body; wherein the outer tubular body is provided with a plurality of holes allowing cooling air to enter the cooling channel; wherein the outer surface of the inner tubular body is provided with a plurality of ribs.",
  "title": "TRANSITION DUCT FOR A GAS TURBINE CAN COMBUSTOR"
}