{
  "$type": "site.standard.document",
  "description": "A method (300) for detecting a fault within a brake mechanism on an aircraft is disclosed. In various embodiments, the method includes activating (302), by a brake control unit, the brake mechanism; receiving (304), by the brake control unit, a wheel speed data for a wheel associated with the brake…",
  "path": "/patents/1415664",
  "publishedAt": "2023-02-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T17/221",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A method (300) for detecting a fault within a brake mechanism on an aircraft is disclosed. In various embodiments, the method includes activating (302), by a brake control unit, the brake mechanism; receiving (304), by the brake control unit, a wheel speed data for a wheel associated with the brake mechanism; determining (306), by the brake control unit, a wheel speed characteristic for the wheel associated with the brake mechanism; and detecting (308), by the brake control unit, whether the brake mechanism is faulty based on a comparison of the wheel speed characteristic and a wheel speed deceleration database.",
  "title": "DETECTION OF BRAKE FAILURE USING WHEEL SPEED DURING LANDING GEAR RETRACTION"
}