Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jet aircraft
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine |
gptkb:CF34
|
| gptkbp:engine_configuration |
twin-spool
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF34-3 B21
|
| gptkbp:ignition_system |
dual spark plug
|
| gptkbp:length |
1,800 mm
|
| gptkbp:maintenance |
4,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:max_speed |
10,000 RPM
|
| gptkbp:notable_users |
gptkb:Bombardier_CRJ_series
|
| gptkbp:number_of_stages |
gptkb:5
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:turbine_type |
high bypass ratio
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF34-3_B
|
| gptkbp:bfsLayer |
7
|