|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
FAA certified
ICAO CAEP/6 compliant
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:5
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
1,200 mm
68 inches
|
|
gptkbp:engine
|
gptkb:CF34
|
|
gptkbp:engine_configuration
|
twin spool
flat rated to 30° C
|
|
gptkbp:engine_type
|
gptkb:CF34-10_E
gptkb:CF34-8_C
gptkb:CF34-8_E
gptkb:CF34-8_F
gptkb:CF34-8_G
gptkb:CF34-8_H
gptkb:CF34-8_K
gptkb:CF34-8_L
gptkb:CF34-8_M
gptkb:CF34-8_N
high bypass turbofan
|
|
gptkbp:fan_art
|
wide chord fan
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
1,200 kg
1,200 mm
1,800 mm
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
electronic fuel control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-8 Q
|
|
gptkbp:launch_window
|
air starter
|
|
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:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:propulsion
|
18,500 lbf
|
|
gptkbp:turbine_type
|
2
high pressure turbine
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-8_C
|
|
gptkbp:bfsLayer
|
6
|