{
  "$type": "site.standard.document",
  "description": "An apparatus for powering an aircraft by generating power from a pressure spool (26,28) of a turbine engine (10) includes a speed range reduction assembly (74,740) that reduces the higher speed ranges of a low pressure spool (28) to lower speed ranges within the tolerances of the same DC or VF…",
  "path": "/patents/986929",
  "publishedAt": "2013-09-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C7/32",
    "GE AVIAT SYSTEMS LLC [US]"
  ],
  "textContent": "An apparatus for powering an aircraft by generating power from a pressure spool (26,28) of a turbine engine (10) includes a speed range reduction assembly (74,740) that reduces the higher speed ranges of a low pressure spool (28) to lower speed ranges within the tolerances of the same DC or VF generators (58,580) used with the high pressure spool (26).",
  "title": "Apparatus for extracting input power from the low pressure spool of a turbine engine"
}