{
  "$type": "site.standard.document",
  "description": "The process involves determining static temperature at the level of an aircraft, using dynamic temperature outside the aircraft. A temperature value related to temperature at destination altitude is measured using the static temperature. A difference between the value and the destination altitude…",
  "path": "/patents/1075195",
  "publishedAt": "2005-08-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/00",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The process involves determining static temperature at the level of an aircraft, using dynamic temperature outside the aircraft. A temperature value related to temperature at destination altitude is measured using the static temperature. A difference between the value and the destination altitude temperature is found. An alarm signal is emitted by an alarm signal providing unit (10) when the difference is greater than a preset value. An independent claim is also included for an aircraft including a flight management system having a device for verification of a temperature value at a destination altitude of the aircraft.",
  "title": "Method and device for checking a temperature value at a destination altitude of an aircraft"
}