{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) for an aircraft includes a turbine section (28) and an exhaust section (30) configured to receive an exhaust gas stream from the turbine section (28). The exhaust section (30) includes a monolithic catalyst structure configured to remove nitrogen oxides (NO) from the…",
  "path": "/patents/1399117",
  "publishedAt": "2025-04-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B01D53/56",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A gas turbine engine (20) for an aircraft includes a turbine section (28) and an exhaust section (30) configured to receive an exhaust gas stream from the turbine section (28). The exhaust section (30) includes a monolithic catalyst structure configured to remove nitrogen oxides (NO) from the exhaust gas stream.",
  "title": "EXHAUST SYSTEM FOR A GAS TURBINE ENGINE AND METHOD FOR USING SAME"
}