{
  "$type": "site.standard.document",
  "description": "The inlet has a dynamic inlet duct (30) provided with a grid (40) for protection against ingesting foreign bodies. The grid is moved in translation along a dynamic axis (AX1) relative to a front flow section of the duct. A lateral inlet is arranged in a side wall. A covering unit (41) covering the…",
  "path": "/patents/1012867",
  "publishedAt": "2011-05-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The inlet has a dynamic inlet duct (30) provided with a grid (40) for protection against ingesting foreign bodies. The grid is moved in translation along a dynamic axis (AX1) relative to a front flow section of the duct. A lateral inlet is arranged in a side wall. A covering unit (41) covering the lateral inlet is movable relative to the lateral inlet. A displacement unit (60) allows movement of the covering unit relative to the lateral inlet during movement in translation of the grid. An independent claim is also included for a method for optimizing operation of a turbine engine of an aircraft.",
  "title": "Air intake of a turbine aircraft engine, aircraft equipped with such air intake and method for optimizing the operation of a turbine aircraft engine with an air intake"
}