{
  "$type": "site.standard.document",
  "description": "A rigid electrical raft (200) is provided to a gas turbine engine via a fusible mount arrangement (400). The rigid electrical raft may be a part of an electrical system of the gas turbine engine, for example a part of the electrical harness. The fusible mount (400) is arranged to break when a…",
  "path": "/patents/969315",
  "publishedAt": "2014-10-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/045",
    "ROLLS ROYCE PLC [GB]"
  ],
  "textContent": "A rigid electrical raft (200) is provided to a gas turbine engine via a fusible mount arrangement (400). The rigid electrical raft may be a part of an electrical system of the gas turbine engine, for example a part of the electrical harness. The fusible mount (400) is arranged to break when a predetermined load is applied. The rigid electrical raft may be attached to a fan case of the engine, and the predetermined load may that which results from a fan blade being released from the hub. This ensures that the rigid electrical raft is protected from the load.",
  "title": "Mounting arrangement"
}