Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:certification |
Stage 3
|
| gptkbp:compressor_type |
gptkb:5
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3.0 ft
60 in |
| gptkbp:engine |
gptkb:CF6
|
| gptkbp:first_flight |
gptkb:1970
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-50 C8
|
| gptkbp:introduced |
gptkb:1970
|
| gptkbp:length |
11.5 ft
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
Chapter 3
|
| gptkbp:notable_users |
gptkb:Boeing_707
gptkb:Airbus gptkb:Mc_Donnell_Douglas_DC-10 |
| gptkbp:propulsion |
50,000 lbf
|
| gptkbp:successor |
CF6-80 C2
|
| gptkbp:turbine_type |
2
|
| gptkbp:weight |
3,000 lb
|
| gptkbp:bfsParent |
gptkb:CF6-50_C
|
| gptkbp:bfsLayer |
7
|