|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
up to 1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
1,000 mm
68 inches
|
|
gptkbp:engine
|
gptkb:CF34
gptkb:CF34-10
Brayton cycle
|
|
gptkbp:engine_configuration
|
pylon-mounted
twin spool
|
|
gptkbp:engine_power
|
20,000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:CF34-10_A
gptkb:CF34-10_E
gptkb:CF34-10_F
gptkb:CF34-10_G
gptkb:CF34-10_H
gptkb:CF34-10_J
gptkb:CF34-10_K
gptkb:CF34-10_B
gptkb:CF34-10_C
gptkb:CF34-10_D
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-10 Y
|
|
gptkbp:launch_platform
|
electric 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:power_output
|
13,800 to 18,500 lbf
|
|
gptkbp:propulsion
|
18,500 lbf
cascade type
|
|
gptkbp:service_ceiling
|
37,000 feet
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:water_requirement
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-10_E
gptkb:CF34-10_B
|
|
gptkbp:bfsLayer
|
7
|