{
  "$type": "site.standard.document",
  "description": "A full authority digital engine controller (FADEC) (16;116;316;416) controls an engine (12;112;312;412) attached to an airframe (14;114;314;414). The FADEC (16;116;316;416) includes an electronic engine controller (EEC) (20;120;320;420) attached to the engine (12;112;312;412), an airframe data…",
  "path": "/patents/1003265",
  "publishedAt": "2012-04-18T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F02C9/00",
    "HAMILTON SUNDSTRAND CORP [US]"
  ],
  "textContent": "A full authority digital engine controller (FADEC) (16;116;316;416) controls an engine (12;112;312;412) attached to an airframe (14;114;314;414). The FADEC (16;116;316;416) includes an electronic engine controller (EEC) (20;120;320;420) attached to the engine (12;112;312;412), an airframe data concentrator (ADC) (18;118;318,418) attached to the airframe (14;114;314;414), and a digital data bus (22;122;312;412) electrically connecting the ADC (18;118;318,418) to the EEC (20;120;320;420). The ADC (18;118;318,418) is electrically connected to a plurality of airframe sensors (26;126;326;426) to convert the airframe sensor signals to airframe sensor digital data. The digital bus (22;122;322;422) conducts the airframe sensor digital data to the EEC (20;120;320;420).",
  "title": "Distributed small engine FADEC"
}