{
  "$type": "site.standard.document",
  "description": "The present invention relates to an aircraft (1) equipped with an engine compartment (5), said aircraft (1) comprising a motor (10) housed at least partially in the engine compartment (5), the motor (10) comprising an ejection nozzle (20) for at least ejecting gases, said aircraft (1) comprising an…",
  "path": "/patents/1393182",
  "publishedAt": "2025-06-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C1/1453",
    "AIRBUS HELICOPTERS [FR]"
  ],
  "textContent": "The present invention relates to an aircraft (1) equipped with an engine compartment (5), said aircraft (1) comprising a motor (10) housed at least partially in the engine compartment (5), the motor (10) comprising an ejection nozzle (20) for at least ejecting gases, said aircraft (1) comprising an exhaust duct (30) disposed around the ejection nozzle (20), the exhaust duct (30) having an open end (35) opening into the engine compartment (5). The aircraft (1) comprises a drainage device (40) comprising a guide (45) cooperating with the exhaust duct (30) to collect a liquid (100) flowing along the exhaust duct (30) and escaping from the exhaust duct (30) through said end (35).",
  "title": "AIRCRAFT PROVIDED WITH AN ENGINE AND A DRAIN CONDUIT WHICH IS ARRANGED AROUND AN EXHAUST DUCT OF THE ENGINE",
  "updatedAt": "2026-06-19T10:31:06.232Z"
}