{
  "$type": "site.standard.document",
  "description": "A landing gear includes a wheel support portion connected to a fuselage of an aircraft, a wheel rotatably connected to the wheel support portion via a shaft, a stator mounted on the shaft, and a rotor mounted on the wheel spaced apart from the stator.",
  "path": "/patents/1377073",
  "publishedAt": "2025-11-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C25/405",
    "HYUNDAI MOTOR COMPANY"
  ],
  "textContent": "A landing gear includes a wheel support portion connected to a fuselage of an aircraft, a wheel rotatably connected to the wheel support portion via a shaft, a stator mounted on the shaft, and a rotor mounted on the wheel spaced apart from the stator.",
  "title": "LANDING GEAR OF AIRCRAFT AND METHOD FOR TAKEOFF AND LANDING USING LANDING GEAR"
}