{
  "$type": "site.standard.document",
  "description": "The device has a protection cover (32) with a main portion (34) to seal an inlet (14) of a fan case ducting (12) when the device is assembled on an air inlet structure (6) of a jet engine. The cover has a secondary portion integrated with the main portion, where the secondary portion has…",
  "path": "/patents/1084371",
  "publishedAt": "2004-09-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64F1/005",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The device has a protection cover (32) with a main portion (34) to seal an inlet (14) of a fan case ducting (12) when the device is assembled on an air inlet structure (6) of a jet engine. The cover has a secondary portion integrated with the main portion, where the secondary portion has rigidifying unit and covers partially a hood (8) to seal a ventilation flap (20).",
  "title": "Protective device for the air intake of a jet engine"
}