{
  "$type": "site.standard.document",
  "description": "The turbine has a blade (2) arranged downstream to a combustion chamber (9). A mini-heat shield (13) is fastened to a turbine carrier (4) and arranged at an upstream extension (4') of the turbine carrier or over a turbine carrier element at the turbine carrier upstream to the blade. The shield is…",
  "path": "/patents/1004366",
  "publishedAt": "2012-03-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D9/023",
    "ALSTOM TECHNOLOGY LTD [CH]"
  ],
  "textContent": "The turbine has a blade (2) arranged downstream to a combustion chamber (9). A mini-heat shield (13) is fastened to a turbine carrier (4) and arranged at an upstream extension (4') of the turbine carrier or over a turbine carrier element at the turbine carrier upstream to the blade. The shield is arranged adjacent to a vane platform (3) in a flow direction (10) of hot gas between a heat shield and the platform. The mini-heat shield forms a flow wall between the heat shield and the platform. An upstream small gap (17) is formed between the mini-heat shield and the heat shield.",
  "title": "Transitional Region for a Combustion Chamber of a Gas Turbine"
}