{
  "$type": "site.standard.document",
  "description": "The network (10) has a three-phase power bus (11) conveying three-phase alternating current (AC) power generated by one direct current (DC)/AC converter (12) that is powered by a DC source of an aircraft. The DC/AC converter is fitted with a modulator unit for modulating the voltage and/or the…",
  "path": "/patents/1013665",
  "publishedAt": "2011-04-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C25/30",
    "MESSIER BUGATTI [FR]"
  ],
  "textContent": "The network (10) has a three-phase power bus (11) conveying three-phase alternating current (AC) power generated by one direct current (DC)/AC converter (12) that is powered by a DC source of an aircraft. The DC/AC converter is fitted with a modulator unit for modulating the voltage and/or the frequency of the three-phase power generated by the DC/AC converter. The DC/AC converter is of a linear amplification type. The power bus delivers AC voltage to a set of emergency unlocking actuators, where all of the actuators are connected to the three-phase power bus.",
  "title": "NETWORK FOR MANAGING MONO OR MULTI-ENGINE ACTUATORS, PARTICULARLY ADAPTED FOR AERONAUTICAL APPLICATIONS, SUCH AS THE POWER SUPPLY FOR THE MOTORS OF LATCHING BOXES"
}