{
  "$type": "site.standard.document",
  "description": "The present invention relates to a method for controlling a rotorcraft (1), said rotorcraft (1) comprising at least two combustion engines (2, 3), at least one control system (13) and a transmission system (4), said at least two engines (2, 3) being mechanically connected to said transmission…",
  "path": "/patents/1386550",
  "publishedAt": "2026-02-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/04",
    "AIRBUS HELICOPTERS [FR]"
  ],
  "textContent": "The present invention relates to a method for controlling a rotorcraft (1), said rotorcraft (1) comprising at least two combustion engines (2, 3), at least one control system (13) and a transmission system (4), said at least two engines (2, 3) being mechanically connected to said transmission system (4) respectively by at least two couplings (25, 26). Such a control method comprises at least an identification of an engine regulated in N2 (2), an identification of an engine not regulated in N2' (3) and a generation of a control setpoint limit of at least a first control system (12) of the engine regulated in N2 (2) and dependent on the rotation speed N2 of at least a first output shaft (5) of the engine regulated in N2 (2).",
  "title": "METHOD FOR CONTROLLING A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND COMPUTER PROGRAM",
  "updatedAt": "2026-06-11T15:50:56.555Z"
}