{
  "$type": "site.standard.document",
  "description": "A system for two-stage determination of a brakefail of an aircraft brake system includes an aircraft brake. The aircraft brake (106) is configured to receive a current command value, convert the current command value to a braking pressure and output a detected pressure value corresponding to the…",
  "path": "/patents/1420050",
  "publishedAt": "2024-04-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T13/74",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A system for two-stage determination of a brakefail of an aircraft brake system includes an aircraft brake. The aircraft brake (106) is configured to receive a current command value, convert the current command value to a braking pressure and output a detected pressure value corresponding to the braking pressure. The system also includes a brake control unit (BCU) (102) configured to determine a pressure command value, convert the pressure command value to the current command value and to determine whether a brakefail event has occurred based on the pressure command value, the current command value and the detected pressure value.",
  "title": "STAGED METHOD TO DETECT BRAKE FAIL CONDITIONS IN BRAKE CONTROL SYSTEMS"
}