{
  "$type": "site.standard.document",
  "description": "The method involves turning off a first engine (10) of an aircraft (1) by using a first control unit (13) when monitoring parameter of the first engine exceeds a first threshold value. A second engine (20) of the aircraft is turned off by a second control unit (23) when monitoring parameter of the…",
  "path": "/patents/985527",
  "publishedAt": "2013-03-20T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D21/02",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves turning off a first engine (10) of an aircraft (1) by using a first control unit (13) when monitoring parameter of the first engine exceeds a first threshold value. A second engine (20) of the aircraft is turned off by a second control unit (23) when monitoring parameter of the second engine exceeds a second threshold value, where the second value is greater than the first value, the parameters of the engines are number of revolutions of free turbines (10', 20') of the engines, and an external device indicates the values to-be implemented to the control units. Independent claims are also included for the following: (1) an over-speed safety system for an aircraft (2) an aircraft.",
  "title": "Control method for an overspeed safety system, associated system and aircraft"
}