{
  "$type": "site.standard.document",
  "description": "The method involves activating an assisted piloting mode. A monitoring parameter e.g. gas ejection temperature, is maintained below a predetermined threshold when a limit indicator (10) is no longer in a position to display information. The monitoring parameter is maintained below a predetermined…",
  "path": "/patents/1014432",
  "publishedAt": "2011-03-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/04",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves activating an assisted piloting mode. A monitoring parameter e.g. gas ejection temperature, is maintained below a predetermined threshold when a limit indicator (10) is no longer in a position to display information. The monitoring parameter is maintained below a predetermined threshold by putting a ceiling on rate at which fuel is fed to engines (2, 3) e.g. turbine engines, where the engines have a free turbine and a gas generator. A pilot of the aircraft is informed when the assisted piloting mode is activated. An independent claim is also included for an assisted piloting device for a rotorcraft.",
  "title": "Method and device for aiding piloting an aircraft in case of failure of a first limitation indicator"
}