{
  "$type": "site.standard.document",
  "description": "When a first generator (46a) is stopped, an electric motor control section (90) reduces the output power of a VTOL electric motor (20V) and a cruise electric motor (24C) that operate with electric power supplied from the first generator (46a), and increases the output power of a VTOL electric motor…",
  "path": "/patents/1396644",
  "publishedAt": "2024-11-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L50/60",
    "HONDA MOTOR CO LTD [JP]"
  ],
  "textContent": "When a first generator (46a) is stopped, an electric motor control section (90) reduces the output power of a VTOL electric motor (20V) and a cruise electric motor (24C) that operate with electric power supplied from the first generator (46a), and increases the output power of a VTOL electric motor (20V) and a cruise electric motor (24C) that operate with electric power supplied from a second generator (46b).",
  "title": "CONTROL DEVICE FOR AIRCRAFT"
}