{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
      "$link": "bafkreiarytredjexmfa7nig3hhi3pxl3yt3kh7xq4lcswjqkodyojcylau"
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    "mimeType": "image/png",
    "size": 100232
  },
  "description": "A wheel assembly is provided that includes a structure defining a wheel portion configured to receive a portion of a tire. The wheel assembly further includes a structure of the wheel portion defining an air channel from a face of the wheel portion to an area that receives the portion of the tire…",
  "path": "/patents/1365014",
  "publishedAt": "2024-06-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60C29/06",
    "Goodrich Corporation"
  ],
  "textContent": "A wheel assembly is provided that includes a structure defining a wheel portion configured to receive a portion of a tire. The wheel assembly further includes a structure of the wheel portion defining an air channel from a face of the wheel portion to an area that receives the portion of the tire, an end of the air channel proximate to the face being configured to receive a valve, where the structure is further configured to receive a corrosion mitigation device within the air channel.",
  "title": "CORROSION PROTECTION FOR AIRCRAFT WHEEL PNEUMATIC PORTS"
}