|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jet aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.4:1
|
|
gptkbp:certification
|
CAEP/6
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:5
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
3.0 ft
2.9 ft
|
|
gptkbp:engine
|
gptkb:CF34-10_series
gptkb:CF34
Brayton cycle
|
|
gptkbp:engine_configuration
|
twin-spool
high bypass ratio
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:CF34-10_A
gptkb:CF34-10_E
gptkb:CF34-8_C
gptkb:CF34-8_A
gptkb:CF34-8_E
gptkb:CF34-10_F
gptkb:CF34-10_G
gptkb:CF34-10_H
gptkb:CF34-10_I
gptkb:CF34-10_J
gptkb:CF34-10_K
gptkb:CF34-10_L
gptkb:CF34-10_M
gptkb:CF34-10_N
gptkb:CF34-10_O
gptkb:CF34-10_P
gptkb:CF34-10_Q
gptkb:CF34-10_R
gptkb:CF34-10_S
gptkb:CF34-10_T
gptkb:CF34-10_U
gptkb:CF34-10_V
gptkb:CF34-10_W
gptkb:CF34-10_X
gptkb:CF34-10_Y
gptkb:CF34-10_D
gptkb:CF34-10_Z
gptkb:CF34-8_B
|
|
gptkbp:fan_art
|
wide-chord fan blades
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
0.91 m
1.37 m
816 kg
|
|
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
|
CF34-10 B
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:notable_users
|
gptkb:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:propulsion
|
18,500 lbf
4,000 lbf
19,000 lbf
|
|
gptkbp:turbine_type
|
2
high-pressure turbine
low-pressure turbine
|
|
gptkbp:weight
|
1,800 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_CF34-10_E
|
|
gptkbp:bfsLayer
|
6
|