{
  "$type": "site.standard.document",
  "description": "The turbine (10) has an exhaust gas diffuser (21) connected to a turbine unit (24). An inflow-side annular diffuser channel (33) is limited by a conical channel wall (40). Inward extending hollow support ribs (35) are provided at the channel for fastening a radial bearing (51). A blow line (47) for…",
  "path": "/patents/984140",
  "publishedAt": "2013-09-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/30",
    "SIEMENS AG [DE]"
  ],
  "textContent": "The turbine (10) has an exhaust gas diffuser (21) connected to a turbine unit (24). An inflow-side annular diffuser channel (33) is limited by a conical channel wall (40). Inward extending hollow support ribs (35) are provided at the channel for fastening a radial bearing (51). A blow line (47) for blow air, is led into the diffuser. An inflow side end of the blow line is connected with an axial-flow turbo compressor (18). An outflow-side end of the blow line is fluidically connected with a cavity of the ribs. The ribs comprise apertures (49) for blowing the blow air into the channel.",
  "title": "Gas turbine with an exhaust gas diffuser and support ribs"
}