{
  "$type": "site.standard.document",
  "description": "An exemplary aircraft (100) includes a turbine engine (102, 202) having a gas generator spool (204) and a power spool (206), the power spool operational to drive a rotor (107, 216), a first generator (218) coupled to the gas generator spool (204), and a controller (110) operable to increase a load…",
  "path": "/patents/1410448",
  "publishedAt": "2024-02-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/06",
    "TEXTRON INNOVATIONS INC [US]"
  ],
  "textContent": "An exemplary aircraft (100) includes a turbine engine (102, 202) having a gas generator spool (204) and a power spool (206), the power spool operational to drive a rotor (107, 216), a first generator (218) coupled to the gas generator spool (204), and a controller (110) operable to increase a load on the gas generator spool (204) when the gas generator spool is on a speed limit thereby increasing a speed limit margin in order to increase power available from the turbine engine (102, 202).",
  "title": "GAS GENERATOR SPEED LIMIT AND POWER RECOVERY"
}