{
  "$type": "site.standard.document",
  "description": "A low voltage DC power system for powering an aircraft brake actuator assembly (230). The brake actuator assembly (230) may comprise an electric actuator motor system with a park brake (232) and/or a hybrid electric hydraulic system with a park brake (332). The brake actuator assembly (230) may…",
  "path": "/patents/947036",
  "publishedAt": "2016-01-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60R16/03",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A low voltage DC power system for powering an aircraft brake actuator assembly (230). The brake actuator assembly (230) may comprise an electric actuator motor system with a park brake (232) and/or a hybrid electric hydraulic system with a park brake (332). The brake actuator assembly (230) may also comprise a load cell (234) and one or more sensors (236). The load cell (234) and sensors (334) may be configured to operate with low voltage DC power. Moreover, by employing a low voltage DC power system, the wiring of an aircraft brake system (200) may be reduced and/or simplified.",
  "title": "APPARATUS AND SYSTEM FOR POWER DISTRIBUTION TO BRAKE SYSTEMS"
}