{
  "$type": "site.standard.document",
  "description": "A system for measuring tire pressure on an aircraft includes a wheel (100; 150) with a tire pressure. A tire pressure sensor (108; 160; 214; 300; 506; 516) on the wheel (100; 150) may be configured to output an electronic measurement of the tire pressure. A transmission device (114; 166; 204) may…",
  "path": "/patents/953159",
  "publishedAt": "2016-02-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60C23/04",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A system for measuring tire pressure on an aircraft includes a wheel (100; 150) with a tire pressure. A tire pressure sensor (108; 160; 214; 300; 506; 516) on the wheel (100; 150) may be configured to output an electronic measurement of the tire pressure. A transmission device (114; 166; 204) may be electrically coupled to the first tire pressure sensor (108; 160; 214; 300; 506; 516) and configured to transmit the first electronic measurement. A hubcap (112; 164; 200; 504; 514) may be on the first wheel (100; 150) with the transmission device (114; 166; 204) mounted to the hubcap (112; 164; 200; 504; 514).",
  "title": "SYSTEM FOR EXTERNAL ANNUNCIATION OF TIRE PRESSURE"
}