|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
up to 1,500 ° F
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
1,000 mm
4.5:1
68 inches
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF34_family
gptkb:CF34_series
air start
|
|
gptkbp:engine_configuration
|
twin spool
|
|
gptkbp:engine_type
|
gptkb:CF34-8_C
gptkb:CF34-8_A
gptkb:CF34-8_E
gptkb:CF34-8_B
gptkb:CF34-8_D
gptkb:CF34-8_F
gptkb:CF34-8_G
gptkb:CF34-8_H
gptkb:CF34-8_J
gptkb:CF34-8_K
gptkb:CF34-8_L
gptkb:CF34-8_M
turbofan
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
1,000 mm
1,200 kg
1,800 mm
|
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-8 N
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:notable_users
|
gptkb:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:number_of_stages
|
gptkb:6
|
|
gptkbp:overall_pressure_ratio
|
25:1
|
|
gptkbp:power_output
|
13,800 to 18,500 lbf
|
|
gptkbp:propulsion
|
18,500 lbf
15.4:1
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-8_C
|
|
gptkbp:bfsLayer
|
6
|