Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jet aircraft
|
| gptkbp:bypass_ratio |
5.3:1
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:engine |
gptkb:CF34_family
|
| gptkbp:first_flight |
gptkb:1994
|
| gptkbp:fuel_economy |
0.5 lb/lbf/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF34-10 F-5
|
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notable_users |
gptkb:Bombardier_CRJ-900
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:turbine_type |
high bypass ratio turbine
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:CF34-10_F
|
| gptkbp:bfsLayer |
8
|