{
  "$type": "site.standard.document",
  "description": "When a difference in the SOC among respective batteries (50) is greater than or equal to a first prescribed value, an electric motor control section (90) reduces output power of a cruise electric motor (24C) that operates using electric power of a battery (50) with a low SOC and increases output…",
  "path": "/patents/1396649",
  "publishedAt": "2025-01-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L3/12",
    "HONDA MOTOR CO LTD [JP]"
  ],
  "textContent": "When a difference in the SOC among respective batteries (50) is greater than or equal to a first prescribed value, an electric motor control section (90) reduces output power of a cruise electric motor (24C) that operates using electric power of a battery (50) with a low SOC and increases output power of a cruise electric motor (24C) that operates using electric power of a battery (50) with a high SOC.",
  "title": "CONTROL APPARATUS FOR AIRCRAFT"
}