{
  "$type": "site.standard.document",
  "description": "A power distribution system which may be provided in an aircraft for example is described. The power distribution system has a power distribution bus 110 and a plurality of localised voltage converters 120, each supplied by the power distribution bus 110. By providing a plurality of localised…",
  "path": "/patents/1004138",
  "publishedAt": "2012-03-21T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L1/00",
    "GE AVIAT SYSTEMS LTD [GB]"
  ],
  "textContent": "A power distribution system which may be provided in an aircraft for example is described. The power distribution system has a power distribution bus 110 and a plurality of localised voltage converters 120, each supplied by the power distribution bus 110. By providing a plurality of localised voltage converters 120, the power distribution system may use fewer, or just a single power distribution bus 110 at a particular voltage and convert to the desired voltage at or near to each of a plurality of pieces of electrical equipment being supplied.",
  "title": "Power distribution system for an aircraft"
}