{
  "$type": "site.standard.document",
  "description": "A gas turbine engine exhaust system comprises an instrumented exhaust duct (30) including a set of exhaust temperature probes (50; 52) installed at the exhaust end (30b; 30c) of the duct (30) in an air space (G) between an engine outer case (18) and a surrounding engine nacelle (N). A shield (60)…",
  "path": "/patents/1406978",
  "publishedAt": "2024-09-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/085",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine exhaust system comprises an instrumented exhaust duct (30) including a set of exhaust temperature probes (50; 52) installed at the exhaust end (30b; 30c) of the duct (30) in an air space (G) between an engine outer case (18) and a surrounding engine nacelle (N). A shield (60) is removably installed at the end (30b; 30c) of the exhaust duct (30) to protect the probes (50; 52) and associated wiring in the air space (G).",
  "title": "INSTRUMENTED TURBINE EXHAUST DUCT"
}