{
  "$type": "site.standard.document",
  "description": "An aircraft (1) comprising a wing (3) having a spanwise lift distribution extending from a root (10) to a tip (12), the lift distribution defining an inboard region (14) defining a positive lift contribution, an outboard region (16) defining a negative lift contribution, and an intermediate region…",
  "path": "/patents/1414902",
  "publishedAt": "2024-10-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C11/46",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "An aircraft (1) comprising a wing (3) having a spanwise lift distribution extending from a root (10) to a tip (12), the lift distribution defining an inboard region (14) defining a positive lift contribution, an outboard region (16) defining a negative lift contribution, and an intermediate region (18) defining a neutral lift contribution, the neutral region (18) being spaced from the tip (12) and from the root (10). A propulsion system is provided, comprising a wing mounted propulsor (5). The wing mounted propulsor (5) has a rotational axis (x) positioned substantially at a span of the wing (3) where a value of δLift/δSpan is at a maximum for the span of the wing, and may be located at the intermediate region (18) along the span of the wing (3).",
  "title": "AIRCRAFT"
}