{
  "$type": "site.standard.document",
  "description": "An aircraft (1) is described comprising a pilot cockpit (10); a windshield (11) delimiting the cockpit (10); a windscreen wiper (14, 15) comprising a plurality of nozzles (16, 17); a first tank (20) filled with a cleaning fluid and fluidically connected with the nozzles (16, 17); and a control unit…",
  "path": "/patents/1386212",
  "publishedAt": "2026-02-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60S1/482",
    "LEONARDO SPA [IT]"
  ],
  "textContent": "An aircraft (1) is described comprising a pilot cockpit (10); a windshield (11) delimiting the cockpit (10); a windscreen wiper (14, 15) comprising a plurality of nozzles (16, 17); a first tank (20) filled with a cleaning fluid and fluidically connected with the nozzles (16, 17); and a control unit (30) programmed to determine a flow of cleaning fluid from the first tank (20) towards the windshield (11) and through the nozzles (16, 17); the aircraft (1) further comprises a second tank (35) filled with an anti-icing/de-icing fluid and fluidically connected with the nozzles (16, 17); the control unit (30) determines a flow of anti-icing/de-icing fluid from the second tank (35) towards the windshield (11) and through the nozzles (16, 17).",
  "title": "AIRCRAFT AND METHOD FOR REMOVING ICE FROM THE RELATIVE WINDSHIELD OR FOR PREVENTING THE FORMATION OF ICE ON THE WINDSHIELD ITSELF"
}