{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "An electric brake system (100) for an aircraft as described herein electrically actuates brake mechanisms (108) in a seamless manner when a power interrupt condition is experienced. While operating in a pedal braking mode and in response to a power interrupt condition, the electric brake system…",
  "path": "/patents/1016312",
  "publishedAt": "2011-01-26T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/1703",
    "BOEING CO [US]"
  ],
  "textContent": "An electric brake system (100) for an aircraft as described herein electrically actuates brake mechanisms (108) in a seamless manner when a power interrupt condition is experienced. While operating in a pedal braking mode and in response to a power interrupt condition, the electric brake system (100) discards the last brake actuation command generated from brake pedal interaction. After normal operating power is re-established, the brake pedal data is refreshed to generate a new brake actuation command. These procedures reduce lurching and unexpected brake actuation levels following a power interrupt in the electric brake system.",
  "title": "Power interrupt management for an aircraft electric brake system"
}