{
  "$type": "site.standard.document",
  "description": "The method involves determining (22) and displaying (24) a possible continuous utilization duration (DELTA-T) of a first power e.g. maximum takeoff power, when an engine e.g. turboshaft engine, of a power plant of an aircraft develops a second power greater than a third power e.g. maximum…",
  "path": "/patents/1004826",
  "publishedAt": "2012-02-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/14",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves determining (22) and displaying (24) a possible continuous utilization duration (DELTA-T) of a first power e.g. maximum takeoff power, when an engine e.g. turboshaft engine, of a power plant of an aircraft develops a second power greater than a third power e.g. maximum continuous power, and less than or equal to the first power, where the utilization duration passes at a variable speed depending on the second power. An alert is triggered when the utilization duration becomes shorter than a predetermined threshold. An independent claim is also included for a unit for controlling a power plant of an aircraft.",
  "title": "Method and device for optimising the use of a motor"
}