{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "The method involves defining two levels of performance of an aircraft (1), and determining a power margin based on a rotational speed of a gas generator (2'). Another power margin is determined based on a temperature of the gas. Each power margin is compared to a threshold to determine whether a…",
  "path": "/patents/987736",
  "publishedAt": "2013-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/04",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves defining two levels of performance of an aircraft (1), and determining a power margin based on a rotational speed of a gas generator (2'). Another power margin is determined based on a temperature of the gas. Each power margin is compared to a threshold to determine whether a target level of performance is equal to one of the levels of performance, and the target level of performance is displayed so that a pilot controls the aircraft depending on the target level of performance established before the flight. An independent claim is also included for a device for optimizing the performance of a rotary wing aircraft.",
  "title": "Method for optimising the performance of an aircraft, device and aircraft"
}