{
  "$type": "site.standard.document",
  "description": "A method and an apparatus to monitor components of an aircraft landing system are disclosed herein. The method includes determining a first temperature of a wheel of an aircraft via a first temperature sensor, and determining a second temperature of a brake assembly operatively coupled to the wheel…",
  "path": "/patents/970003",
  "publishedAt": "2014-09-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T17/221",
    "BOEING CO [US]"
  ],
  "textContent": "A method and an apparatus to monitor components of an aircraft landing system are disclosed herein. The method includes determining a first temperature of a wheel of an aircraft via a first temperature sensor, and determining a second temperature of a brake assembly operatively coupled to the wheel via a second temperature sensor. The method further includes estimating a peak temperature of a fuse plug disposed on the wheel based on the first temperature and the second temperature.",
  "title": "METHOD TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM"
}