Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional jets
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:combustor_type |
annular combustor
|
| gptkbp:compressor_type |
gptkb:5
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
34 inches
approximately 3.5 ft |
| gptkbp:engine_type |
turbofan
|
| gptkbp:first_flight |
gptkb:1982
|
| 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 |
CF34-3
|
| gptkbp:length |
approximately 10.5 ft
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:operational_range |
high bypass ratio
|
| gptkbp:propulsion |
up to 18,500 lbf
|
| gptkbp:service_entry |
gptkb:1983
|
| gptkbp:turbine_type |
2
|
| gptkbp:variant |
gptkb:CF34-8
|
| gptkbp:weight |
approximately 3,000 lb
|
| gptkbp:bfsParent |
gptkb:CF34_Engine
|
| gptkbp:bfsLayer |
6
|