{
  "$type": "site.standard.document",
  "description": "A fuel metering unit (FMU) (128;228;428) for an aircraft engine (112;212;412) includes an effector (132;232;432) and an electronic engine controller (EEC) (120;420). The effector (132;232;432) is electrically connected to the EEC (120;420) to adjust a rate of fuel flowing into the engine…",
  "path": "/patents/1003254",
  "publishedAt": "2012-04-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/263",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A fuel metering unit (FMU) (128;228;428) for an aircraft engine (112;212;412) includes an effector (132;232;432) and an electronic engine controller (EEC) (120;420). The effector (132;232;432) is electrically connected to the EEC (120;420) to adjust a rate of fuel flowing into the engine (112;212;412). The adjustment is in response to a control signal sent from the EEC (120;420). The control signal sent from the EEC (120;420) is responsive to an engine sensor signal and to airframe sensor information.",
  "title": "Electronic engine controler mounted on the fuel metering unit for small aircraft engine applications"
}