CF34-8 L10

URI: https://gptkb.org/entity/CF34-8_L10
GPTKB entity
Statements (43)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Flight
gptkbp:average_temperature 1,600 ° F
gptkbp:bypass_ratio 5.5:1
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:control_system gptkb:FADEC
gptkbp:cooling_system air-cooled
gptkbp:design_features modular design
gptkbp:diameter 1,000 mm
gptkbp:emissions_standard CAEP/6
gptkbp:engine gptkb:CF34
air start
gptkbp:engine_configuration gptkb:CF34-8
twin spool
gptkbp:engine_type gptkb:CF34-8_L10
gptkb:CF34-8_L5
gptkb:CF34-8_C5
CF34-8 E5
CF34-8 A5
CF34-8 B5
CF34-8 L10 E
gptkbp:first_flight gptkb:1996
gptkbp:fuel_economy 0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label CF34-8 L10
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:noise_level Stage 4 compliant
gptkbp:notable_users gptkb:Bombardier_CRJ-900
gptkb:Embraer_ERJ-145
gptkbp:operational_range -40 to 50 ° C
gptkbp:power_output 14,000 to 18,500 lbf
gptkbp:propulsion clamshell
18,500 lbf
gptkbp:service_ceiling 37,000 ft
gptkbp:turbine_type high bypass ratio
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:CF34-8_L
gptkbp:bfsLayer 7