{
  "$type": "site.standard.document",
  "description": "A power generating apparatus for use with an aircraft gas turbine engine (10) has a low pressure spool assembly (12) which includes an electrical generator (34). The electrical generator (34) includes a generator stator (48) supported on a stationary structure of the engine and a generator rotor…",
  "path": "/patents/1001923",
  "publishedAt": "2012-05-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D41/00",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "A power generating apparatus for use with an aircraft gas turbine engine (10) has a low pressure spool assembly (12) which includes an electrical generator (34). The electrical generator (34) includes a generator stator (48) supported on a stationary structure of the engine and a generator rotor (58) rotatable around the generator stator (48) and mounted to the low pressure spool assembly (12).",
  "title": "Aircraft gas turbine engine comprising a generator"
}