|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jets
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:certification
|
CAEP/6 compliant
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:date_enacted
|
gptkb:1994
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:engine
|
gptkb:CF34_family
air start
|
|
gptkbp:engine_configuration
|
twin spool
|
|
gptkbp:engine_type
|
gptkb:CF34-10_A
gptkb:CF34-10_E
gptkb:CF34-10_K1
gptkb:CF34-10_K10
gptkb:CF34-10_K2
gptkb:CF34-10_K3
gptkb:CF34-10_K4
gptkb:CF34-10_K5
gptkb:CF34-10_K6
gptkb:CF34-10_K7
gptkb:CF34-10_K8
gptkb:CF34-10_K9
gptkb:CF34-10_F
gptkb:CF34-10_G
gptkb:CF34-10_H
gptkb:CF34-10_J
gptkb:CF34-10_B
gptkb:CF34-10_D
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:history
|
derived from CF34-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-10 K
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notable_users
|
gptkb:Bombardier_CRJ-900
gptkb:Embraer_ERJ-145
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:operational_range
|
regional aircraft
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:power_output
|
13,000 to 18,500 lbf
|
|
gptkbp:propulsion
|
18,500 lbf
15.4:1
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CF34-10_E
gptkb:CF34-10_B
|
|
gptkbp:bfsLayer
|
7
|