{
  "$type": "site.standard.document",
  "description": "A thermal shielding arrangement for a turbine probe (22) extending through an exhaust case (15) and a turbine housing (24) of a gas turbine engine (10) comprises a sleeve (40) having a radially inner end fixedly mounted to the turbine housing (24) and a radially outer end floatingly received in a…",
  "path": "/patents/1405782",
  "publishedAt": "2024-02-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/003",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A thermal shielding arrangement for a turbine probe (22) extending through an exhaust case (15) and a turbine housing (24) of a gas turbine engine (10) comprises a sleeve (40) having a radially inner end fixedly mounted to the turbine housing (24) and a radially outer end floatingly received in a probe boss (32) on the exhaust case (15). The radially outer end of the sleeve (40) opens to an air cavity (G) between the exhaust case (15) and a surrounding engine nacelle (N) to allow for air circulation around the probe (22).",
  "title": "GAS TURBINE ENGINE INCLUDING A PROBE"
}