{
  "$type": "site.standard.document",
  "description": "Wheeled aircraft landing gear typically includes a sleeve 10 arranged to protect the axle 9. Vibrations of the braking system and flexing of the axle can cause the axle 9 and sleeve 10 to rub and rotate relative to one another, elevating the temperature in this region and causing damage to the…",
  "path": "/patents/1405747",
  "publishedAt": "2025-10-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B29C65/56",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "Wheeled aircraft landing gear typically includes a sleeve 10 arranged to protect the axle 9. Vibrations of the braking system and flexing of the axle can cause the axle 9 and sleeve 10 to rub and rotate relative to one another, elevating the temperature in this region and causing damage to the sleeve and/or axle. The invention provides an axle sleeve 10 having a low friction wear surface 19 on, for example, a portion of the internal surface. The low friction wear surface 19 comprises a ring 20 of composite material, such as fibres in a polymer matrix.",
  "title": "AXLE SLEEVE"
}