{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "It is disclosed an indicator for an aircraft capable of hovering, comprising a first indication (36) associated to the value of vertical speed of the aircraft itself; the indicator comprises a first area wherein a second indication can be displayed that is associated to a Vortex Ring State…",
  "path": "/patents/1409235",
  "publishedAt": "2023-03-01T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/006",
    "LEONARDO SPA [IT]"
  ],
  "textContent": "It is disclosed an indicator for an aircraft capable of hovering, comprising a first indication (36) associated to the value of vertical speed of the aircraft itself; the indicator comprises a first area wherein a second indication can be displayed that is associated to a Vortex Ring State condition being reached; the indicator comprises a second area wherein a third indication can be displayed that is associated to a Vortex Ring State condition approaching; wherein said second indication is overlapped to a first region of the first indication (35) corresponding to first values of a descent vertical speed and said third indication is overlapped to a second region of said first indication (35) corresponding to second values of said descent vertical speed, said first values being greater as an absolute value than said second values.",
  "title": "INDICATOR FOR AN AIRCRAFT CAPABLE OF HOVERING AND METHOD FOR ASSISTING PERFORMING A MANOEUVRE FOR THE AFORESAID AIRCRAFT"
}