{
  "$type": "site.standard.document",
  "description": "A thermally actuated assembly (10) for a gas turbine assembly for a gas turbine system includes a heat transfer component (20) having a first portion (22) and a second portion (24), wherein the first portion (22) is disposed within a first cavity (14) having a first temperature and the second…",
  "path": "/patents/980758",
  "publishedAt": "2013-12-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/085",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A thermally actuated assembly (10) for a gas turbine assembly for a gas turbine system includes a heat transfer component (20) having a first portion (22) and a second portion (24), wherein the first portion (22) is disposed within a first cavity (14) having a first temperature and the second portion (24) is disposed in a second cavity (16) having a second temperature, wherein the heat transfer component (20) extends through a cavity wall, wherein the first temperature is greater than the second temperature. Also included is a temperature sensitive element (26) disposed within the second cavity (16) and in operable communication with the heat transfer component (20). Further included is a flow manipulating device (30,32) disposed within the second cavity (16) and configured to displace in response to a temperature change in the first cavity (14).",
  "title": "Thermally actuated assembly for a gas turbine system and method of controlling a cooling airflow path"
}