{
  "$type": "site.standard.document",
  "description": "A system (100) for controlling a flow rate of a compressed cooling medium between a compressor section (12) and a turbine section (16) of a gas turbine (100) includes a flow path (102) that is defined between the compressor section and the turbine section of the gas turbine and a thermally actuated…",
  "path": "/patents/973765",
  "publishedAt": "2014-06-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/141",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A system (100) for controlling a flow rate of a compressed cooling medium between a compressor section (12) and a turbine section (16) of a gas turbine (100) includes a flow path (102) that is defined between the compressor section and the turbine section of the gas turbine and a thermally actuated variable flow valve (104) disposed within the flow path. The variable flow valve defines an opening (120) that changes in size based on a temperature of the compressed cooling medium flowing therethrough.",
  "title": "A system for controlling a cooling flow from a compressor section of a gas turbine"
}