|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:bypass_ratio
|
5.4:1
|
|
gptkbp:certification
|
gptkb:Certification
CAEP/6
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:5
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
1,000 mm
68 in
|
|
gptkbp:elevation
|
41,000 ft
|
|
gptkbp:engine
|
gptkb:CF34
bleed air
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:CF34-10_E5
turbofan
CF34-10 E5 A
CF34-10 E5 B
CF34-10 E5 E
CF34-10 E5 F
CF34-10 E5 G
CF34-10 E5 H
CF34-10 E5 I
CF34-10 E5 J
CF34-10 E5 K
CF34-10 E5 L
|
|
gptkbp:fan_art
|
wide-chord fan blades
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
1,000 mm
1,200 lb
1,800 mm
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
electronic fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-10 E5
|
|
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:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:operational_range
|
-40 to 50 ° C
|
|
gptkbp:propulsion
|
cascade
18,500 lbf
|
|
gptkbp:turbine_type
|
2
high-pressure turbine
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:GE_CF34-10_E
|
|
gptkbp:bfsLayer
|
7
|