{
  "$type": "site.standard.document",
  "description": "This invention relates to a multi-spool gas turbine engine, comprising: a first generator for providing electrical power to an electrical system, the generator being driveably connected to a first spool; a second generator for providing electrical power to the electrical system, the generator being…",
  "path": "/patents/975160",
  "publishedAt": "2014-05-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D15/10",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "This invention relates to a multi-spool gas turbine engine, comprising: a first generator for providing electrical power to an electrical system, the generator being driveably connected to a first spool; a second generator for providing electrical power to the electrical system, the generator being driveably connected to a second spool; a disconnection device for disconnecting the second generator from the second spool; and, a controller configured to selectively operate the disconnection device under predetermined powered engine conditions.",
  "title": "An electrical generation arrangement for an aircraft"
}