{
  "$type": "site.standard.document",
  "description": "The aircraft (30) can have a first engine (32) secured to a first wing (36) on a first side of a fuselage (42), and a second engine (34) secured to a second wing (44) on a second side of the fuselage (42), the second wing (44) having a proximal end (46) secured to the fuselage (42), and a distal…",
  "path": "/patents/1410665",
  "publishedAt": "2024-07-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C15/02",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "The aircraft (30) can have a first engine (32) secured to a first wing (36) on a first side of a fuselage (42), and a second engine (34) secured to a second wing (44) on a second side of the fuselage (42), the second wing (44) having a proximal end (46) secured to the fuselage (42), and a distal end (48) extending away from the fuselage (42). While operating the first engine (32), compressed gas can be conveyed from the first engine (32) to a thrust generating device (54) located at the distal end of the second wing (44).",
  "title": "AIRCRAFT AND METHOD OF OPERATING SAME"
}