{
  "$type": "site.standard.document",
  "description": "The device has a step-by-step motor (6) activated by a regulation unit (5) to actuate a fuel metering valve (7). The regulation unit evaluates fuel flow to be supplied to a turbine engine, during acceleration or deceleration of the engine, based on an optimal regulation rule. The rule is used for…",
  "path": "/patents/1072848",
  "publishedAt": "2005-11-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/28",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The device has a step-by-step motor (6) activated by a regulation unit (5) to actuate a fuel metering valve (7). The regulation unit evaluates fuel flow to be supplied to a turbine engine, during acceleration or deceleration of the engine, based on an optimal regulation rule. The rule is used for determining a main modulated flow according to modulated rotation speed of an engine combustor. An independent claim is also included for a method implemented by a device for limiting an increase of fuel flow of a turbine engine when a predetermined threshold is attained.",
  "title": "Method and device for fuel flow regulation of a turbomachine"
}