Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:compressor_type |
gptkb:10
axial |
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
2.5 m
3.0 ft |
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine |
gptkb:CF6
|
| gptkbp:engine_configuration |
twin spool
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-80 E1 A4
|
| gptkbp:length |
11.5 ft
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_users |
gptkb:Airbus
gptkb:Boeing |
| gptkbp:number_of_stages_in_low_pressure_compressor |
gptkb:6
|
| gptkbp:propulsion |
60,000 lbf
|
| gptkbp:service_ceiling |
40,000 ft
|
| gptkbp:turbine_type |
gptkb:4
2 high bypass ratio |
| gptkbp:weight |
4,000 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6-80_E1
|
| gptkbp:bfsLayer |
5
|