{
  "$type": "site.standard.document",
  "description": "An air inlet device (100) for an air inlet of an aircraft is described. The air inlet device (100) has a plurality of air guide arrangements (130). An air guide arrangement (130) has an inlet plate (131), an outlet plate (139), and a plurality of pivot plates (133, 135, 137) arranged therebetween…",
  "path": "/patents/1399956",
  "publishedAt": "2024-03-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/162",
    "AIRBUS DEFENCE & SPACE GMBH [DE]"
  ],
  "textContent": "An air inlet device (100) for an air inlet of an aircraft is described. The air inlet device (100) has a plurality of air guide arrangements (130). An air guide arrangement (130) has an inlet plate (131), an outlet plate (139), and a plurality of pivot plates (133, 135, 137) arranged therebetween. The outlet plate and the pivot plates can be rotated about a central axis of the air inlet device by adjustment rings, so that the air guide arrangement (130) is transitioned from a linear state to a curved state, and vice versa. The air inlet device allows for selective switching between a state with low radar signature and a state with high performance of an engine.",
  "title": "AIR INLET DEVICE FOR AN INLET DUCT TO AN ENGINE OF AN AIRCRAFT"
}