{
  "$type": "site.standard.document",
  "description": "What is described is a tire pressure sensor (200) for use in a wheel (132, 134) of aircraft landing gear (110, 120, 130). The tire pressure sensor (200) includes a position sensor (208; 318) configured to detect a movement of the wheel (132, 134) and generate a wheel movement signal based on the…",
  "path": "/patents/943591",
  "publishedAt": "2016-05-04T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60C23/00",
    "GOODRICH CORP [US]"
  ],
  "textContent": "What is described is a tire pressure sensor (200) for use in a wheel (132, 134) of aircraft landing gear (110, 120, 130). The tire pressure sensor (200) includes a position sensor (208; 318) configured to detect a movement of the wheel (132, 134) and generate a wheel movement signal based on the movement. The tire pressure sensor (200) also includes a processor (310) coupled to the position sensor (208; 318). The processor (310) is configured to receive the wheel movement signal, determine a wheel rotational speed of the wheel (132, 134) based on the wheel movement signal and generate a wheel rotational speed signal based on the wheel rotational speed.",
  "title": "ENHANCED BRAKE CONTROL SYSTEM WITH WHEEL MOUNTED POSITION SENSOR"
}