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gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional jet aircraft
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:Delta_Air_Lines
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CF34_family
widely available
global support network
performance upgrades available
single crystal turbine blades
various regional jets
|
|
gptkbp:engine_configuration
|
modular design
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:CF34-10_E
gptkb:CF34-8_C
gptkb:CF34-8_E
high bypass ratio
multiple variants available
|
|
gptkbp:exhaust_system
|
variable area intake
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical fuel control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-10 N
|
|
gptkbp:is_tested_for
|
Peebles Test Operation
|
|
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:number_of_stages
|
gptkb:10
|
|
gptkbp:power_output
|
14,000 to 18,500 lbf
|
|
gptkbp:propulsion
|
18,500 lbf
cascade thrust reverser
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
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
|