{
  "$type": "site.standard.document",
  "description": "An electrically actuated braking system for an aircraft. The system includes: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a motor controller for generating a drive…",
  "path": "/patents/960244",
  "publishedAt": "2015-06-03T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T13/741",
    "AIRBUS OPERATIONS LTD [GB]"
  ],
  "textContent": "An electrically actuated braking system for an aircraft. The system includes: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a motor controller for generating a drive signal for the EMAbrake; a braking control unit (BCU) for generating a braking force command signal for the EMAC during a normal mode of operation; and an emergency braking control unit (eBCU) for generating a braking force command signal for the EMAC during an emergency operating mode. The eBCU is disposed together with the EMAC in a common line replaceable unit (LRU).",
  "title": "Aircraft electric braking system"
}