{
  "$type": "site.standard.document",
  "description": "The system (301) for mitigating an overspeeding condition of a turbine engine (113) can include a sensor (303) for measuring an actual speed (Ng) of a gas generator turbine (127) of the turbine engine and a processor (305) for deriving a delta (407), the delta being a comparison between the actual…",
  "path": "/patents/975186",
  "publishedAt": "2014-05-07T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D17/06",
    "BELL HELICOPTER TEXTRON INC [US]"
  ],
  "textContent": "The system (301) for mitigating an overspeeding condition of a turbine engine (113) can include a sensor (303) for measuring an actual speed (Ng) of a gas generator turbine (127) of the turbine engine and a processor (305) for deriving a delta (407), the delta being a comparison between the actual speed (Ng) of the gas generator turbine and a predicted gas generator turbine speed (405). The system is configured for detecting the overspeeding condition when delta (407) is higher than a predetermined threshold. A method of detecting an overspeeding condition during operation of a turbine engine (113) can include measuring an actual speed of a gas generator turbine (Ng), then evaluating a delta (407) between the actual speed of the gas generator turbine and a predicted speed (405) of the gas generator turbine, then comparing the delta (407) to a threshold value.",
  "title": "System for mitigating overspeeding of a turbine engine"
}