|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:air_support
|
60 lb/s
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
up to 1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:5
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:customer_support
|
gptkb:Bombardier
|
|
gptkbp:diameter
|
1,200 mm
1,500 mm
|
|
gptkbp:engine
|
gptkb:CF34_family
gptkb:CF34_series
|
|
gptkbp:engine_configuration
|
high bypass ratio
flat rated
twin spool
|
|
gptkbp:engine_type
|
gptkb:CF34-8_C
gptkb:CF34-8
gptkb:CF34-8_A
gptkb:CF34-8_P
gptkb:CF34-8_Q
gptkb:CF34-8_R
gptkb:CF34-8_S
gptkb:CF34-8_T
gptkb:CF34-8_E
gptkb:CF34-8_B
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
gptkb:CF34-8_N
gptkb:CF34-8_O
turbofan
CF34-8 U
CF34-8 V
CF34-8 W
CF34-8 X
CF34-8 Y
CF34-8 Z
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
1,200 kg
1,200 mm
1,800 mm
|
|
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
|
CF34-8 I
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:notable_users
|
gptkb:Bombardier_CRJ-900
gptkb:Embraer_ERJ-145
|
|
gptkbp:propulsion
|
18,500 lbf
19,000 lbf
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:water_requirement
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-8_C
|
|
gptkbp:bfsLayer
|
6
|