{
  "$type": "site.standard.document",
  "description": "The present invention relates to an aircraft (1) provided with a power plant (10) provided with at least one combustion engine (20) mechanically connected to a drive system (30), the drive system (30) comprising two electrical machines (35, 40) each connected by a kinematic chain (50) to the…",
  "path": "/patents/1392771",
  "publishedAt": "2024-12-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D27/02",
    "AIRBUS HELICOPTERS [FR]"
  ],
  "textContent": "The present invention relates to an aircraft (1) provided with a power plant (10) provided with at least one combustion engine (20) mechanically connected to a drive system (30), the drive system (30) comprising two electrical machines (35, 40) each connected by a kinematic chain (50) to the combustion engine (20), the two electrical machines (35, 40) being electrically connected to at least one electrical energy source (60). The aircraft (1) comprises a manager (70) controlling at least one mechanical power or engine torque delivered by each of the two electrical machines (35, 40) according to a current operating mode, said manager (70) being configured during a higher operating mode to control the two electrical machines (35, 40) so that the two electrical machines (35, 40) deliver different and unaffected mechanical powers or engine torques.",
  "title": "METHOD AND AIRCRAFT HAVING AT LEAST ONE COMBUSTION ENGINE AND A DRIVE SYSTEM HAVING AT LEAST TWO ELECTRIC MACHINES"
}