Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:Flight
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
gptkb:5
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
68 inches |
| gptkbp:engine_configuration |
dual spool
|
| gptkbp:engine_type |
turbofan
|
| gptkbp:first_flight |
gptkb:1996
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF34-8 L8
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_users |
gptkb:Bombardier_CRJ-900
gptkb:Embraer_ERJ-145 |
| gptkbp:operational_range |
high bypass ratio
|
| gptkbp:propulsion |
18,500 lbf
20,000 lbf |
| gptkbp:turbine_type |
2
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CF34-8_L
|
| gptkbp:bfsLayer |
7
|