{
  "$type": "site.standard.document",
  "description": "A thermal shielding arrangement for a turbine probe (22) comprises a heat shield having first and second mating portions (40, 42) axially engaged in overlapping relationship around a probe (22) extending through an air cavity (34) between an exhaust case (15) and a turbine housing (24). The first…",
  "path": "/patents/1406037",
  "publishedAt": "2024-07-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/02",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A thermal shielding arrangement for a turbine probe (22) comprises a heat shield having first and second mating portions (40, 42) axially engaged in overlapping relationship around a probe (22) extending through an air cavity (34) between an exhaust case (15) and a turbine housing (24). The first mating portion (40) is provided on a radially outer surface of the turbine housing (24). The second mating portion (42) projects radially inwardly from a radially inner surface (30a) of the exhaust case (15).",
  "title": "THERMAL PROTECTION FOR A GAS TURBINE ENGINE PROBE"
}