{
  "$type": "site.standard.document",
  "description": "The invention relates to an aircraft propulsion assembly equipped with a thrust reverser device (60) comprising: - at least one lateral opening (64), passing through the nacelle (48) of the propulsion assembly, configured to occupy an open state or a closed state, - at least one inflatable barrier…",
  "path": "/patents/1392871",
  "publishedAt": "2026-02-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/18",
    "AIRBUS OPERATIONS SAS [FR]"
  ],
  "textContent": "The invention relates to an aircraft propulsion assembly equipped with a thrust reverser device (60) comprising: - at least one lateral opening (64), passing through the nacelle (48) of the propulsion assembly, configured to occupy an open state or a closed state, - at least one inflatable barrier (66) configured to occupy a deflated state in which the barrier (66) does not protrude into an annular duct (50) channeling an air flow (52) and an inflated state in which the barrier (66), substantially rigid or semi-rigid, is deployed and extends across the annular duct (50) to deflect at least a portion of the air flow (52) toward the lateral opening (64). - at least one supply system (98) configured to supply fluid to the inflatable barrier (66). [0002] The invention also relates to an aircraft comprising at least one such propulsion assembly.",
  "title": "AIRCRAFT PROPULSION ASSEMBLY PROVIDED WITH A THRUST REVERSER DEVICE COMPRISING AT LEAST ONE INFLATABLE BARRIER, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY",
  "updatedAt": "2026-06-19T08:31:38.683Z"
}