{
  "$type": "site.standard.document",
  "description": "The method involves acquiring a monitoring parameter of a turbine engine of an aircraft i.e. rotary wing aircraft, and determining whether the aircraft is flying in level with forward flight. A stability of the monitoring parameter is verified. A measurement signal (SIG) giving a measurement of a…",
  "path": "/patents/987697",
  "publishedAt": "2013-08-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64F5/00",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves acquiring a monitoring parameter of a turbine engine of an aircraft i.e. rotary wing aircraft, and determining whether the aircraft is flying in level with forward flight. A stability of the monitoring parameter is verified. A measurement signal (SIG) giving a measurement of a monitoring parameter in compliance with sampling defined by the manufacturer is acquired. The signal is filtered by a high-pass filter over a long duration (TPS1) and measuring amplitude (A1) of the signal that does not exceed a threshold. The parameter is acquired if the parameter is stable. An independent claim is also included for a healthcheck device.",
  "title": "Method and device for monitoring the health of a turbine engine of an aircraft provided with at least one turbine engine"
}