|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
1,200 mm
1,500 mm
|
|
gptkbp:elevation
|
37,000 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF34
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin spool
|
|
gptkbp:engine_type
|
gptkb:CF34-8
gptkb:CF34-8_C5
CF34-8 E5
CF34-8 B5
CF34-8 F5
CF34-8 L5 A
CF34-8 L5 B
CF34-8 L5 C
CF34-8 L5 D
CF34-8 L5 E
CF34-8 L5 F
CF34-8 L5 G
CF34-8 L5 H
CF34-8 L5 I
CF34-8 L5 J
CF34-8 L5 K
CF34-8 L5 L
CF34-8 L5 M
CF34-8 L5 N
CF34-8 L5 O
CF34-8 L5 P
CF34-8 L5 Q
CF34-8 L5 R
CF34-8 L5 S
CF34-8 L5 T
CF34-8 L5 U
CF34-8 L5 V
CF34-8 L5 W
CF34-8 L5 X
CF34-8 L5 Y
CF34-8 L5 Z
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
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 L5
|
|
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:number_of_engines
|
2
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:propulsion
|
18,500 lbf
15.4:1
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-8_L
|
|
gptkbp:bfsLayer
|
7
|