{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
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  "description": "The indicator (1) has a display unit (4) which presents on a visual display screen (5), a frame (6) which is graduated in percentage and whose maximum value represents a maximum thrust available for phase of a present flight. Characteristic signs (7, 8) have positions on the frame representing…",
  "path": "/patents/1082870",
  "publishedAt": "2004-10-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60L15/2045",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The indicator (1) has a display unit (4) which presents on a visual display screen (5), a frame (6) which is graduated in percentage and whose maximum value represents a maximum thrust available for phase of a present flight. Characteristic signs (7, 8) have positions on the frame representing respective controlled and effective thrusts which are expressed in percentage of the maximum thrust. An independent claim is also included for an aircraft with handling indicator.",
  "title": "Pilot display for an aircraft, for displaying the thrust generated by at least one of the engines"
}