{
  "$type": "site.standard.document",
  "description": "The invention relates to an aircraft comprising at least one air intake device (46) having an air inlet (48) opening at the level of an aerodynamic wall (50) and presenting a first end (48.1) positioned on a reference surface (Sr) of the aerodynamic wall (50) substantially parallel to an air flow…",
  "path": "/patents/1392132",
  "publishedAt": "2026-01-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D13/00",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to an aircraft comprising at least one air intake device (46) having an air inlet (48) opening at the level of an aerodynamic wall (50) and presenting a first end (48.1) positioned on a reference surface (Sr) of the aerodynamic wall (50) substantially parallel to an air flow (56) flowing along the aerodynamic wall (50) during operation. According to the invention, the air intake device (46) comprises at least one protuberance (70) projecting from the reference surface (Sr) and positioned upstream of the air inlet (48) according to the direction of flow of the air flow (56), in proximity to or at the same level as the first end (48.1) of the air inlet (48). This protuberance makes it possible to limit the appearance of aerodynamic noise.",
  "title": "AIRCRAFT COMPRISING AT LEAST ONE AIR INTAKE DEVICE CONFIGURED TO LIMIT THE OCCURRENCE OF AERODYNAMIC NOISE",
  "updatedAt": "2026-06-19T07:41:34.577Z"
}