|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:Flight
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
68 in
34 in
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
modular design
advanced materials
|
|
gptkbp:engine_configuration
|
twin-spool
pylon-mounted
|
|
gptkbp:engine_power
|
high efficiency
20,000 hours
|
|
gptkbp:engine_test_stand
|
static test stand
|
|
gptkbp:engine_type
|
gptkb:CF34-10_E5
gptkb:CF34-8_C5
gptkb:CF34-10_K1
turbofan
CF34-10 A1
CF34-10 B1
|
|
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
|
CF34-10 K10
|
|
gptkbp:length
|
60 in
|
|
gptkbp:maintenance
|
4,000 hours
overhaulable
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
acoustic lining
|
|
gptkbp:notable_users
|
gptkb:Embraer_E-Jet_family
gptkb:Bombardier_CRJ-900
|
|
gptkbp:number_of_stages
|
5 stages
|
|
gptkbp:original_run
|
gptkb:1990
|
|
gptkbp:propulsion
|
no
10,000 lbf
|
|
gptkbp:service_ceiling
|
37,000 ft
|
|
gptkbp:starting_system
|
electric starter
|
|
gptkbp:turbine_inlet_temperature
|
1,600 ° F
|
|
gptkbp:turbine_type
|
high bypass turbofan
|
|
gptkbp:weight
|
1,800 lb
|
|
gptkbp:bfsParent
|
gptkb:CF34-10_K
|
|
gptkbp:bfsLayer
|
8
|