{
  "$type": "site.standard.document",
  "description": "A method and apparatus for powering an aircraft by extracting power from both the high pressure and low pressure spools (26, 28) of a gas turbine engine. DC power (48) can be generated using the high pressure spool (26) and AC power (56) can be generated using the low pressure spool (28).",
  "path": "/patents/985645",
  "publishedAt": "2013-03-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D15/10",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A method and apparatus for powering an aircraft by extracting power from both the high pressure and low pressure spools (26, 28) of a gas turbine engine. DC power (48) can be generated using the high pressure spool (26) and AC power (56) can be generated using the low pressure spool (28).",
  "title": "Method and apparatus for extracting electrical power from a gas turbine engine"
}