Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:engine_control_system
|
| gptkbp:canBe |
single channel
dual channel |
| gptkbp:controls |
thrust
variable geometry ignition timing fuel flow engine start bleed valves |
| gptkbp:developedBy |
multiple aerospace companies
|
| gptkbp:enables |
diagnostics
engine health monitoring full digital control of engine parameters |
| gptkbp:improves |
engine reliability
engine efficiency engine safety |
| gptkbp:integratesWith |
aircraft avionics
|
| gptkbp:introducedIn |
1980s
|
| gptkbp:monitors |
engine sensors
|
| gptkbp:provides |
real-time engine data
automatic engine management |
| gptkbp:reduces |
pilot workload
|
| gptkbp:removes |
manual engine control levers
|
| gptkbp:replacedBy |
hydromechanical engine control
|
| gptkbp:requires |
electrical power
|
| gptkbp:standsFor |
Full Authority Digital Engine Control
|
| gptkbp:usedBy |
gptkb:aircraft
helicopters business jets |
| gptkbp:usedIn |
aircraft engines
|
| gptkbp:bfsParent |
gptkb:Pilatus_PC-12_NGX
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
FADEC engine control
|