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:combustor_type
|
annular
|
gptkbp:compressor_type
|
axial
|
gptkbp:configuration
|
dual spool
|
gptkbp:control_system
|
gptkb:FADEC
digital electronic control
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:design
|
20,000 cycles
|
gptkbp:diameter
|
1.1 m
2.3 ft
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
gptkbp:engine
|
gptkb:CF34_family
|
gptkbp:engine_configuration
|
twin-engine
10,000 lbf
|
gptkbp:engine_type
|
gptkb:CF34-10_A
gptkb:CF34-10_E
gptkb:CF34-10_F
gptkb:CF34-10_G
gptkb:CF34-10_H
gptkb:CF34-10_I
gptkb:CF34-10_J
gptkb:CF34-10_K
gptkb:CF34-10_L
gptkb:CF34-10_M
gptkb:CF34-10_N
gptkb:CF34-10_O
gptkb:CF34-10_P
gptkb:CF34-10_Q
gptkb:CF34-10_R
gptkb:CF34-10_S
gptkb:CF34-10_T
gptkb:CF34-10_U
gptkb:CF34-10_V
gptkb:CF34-10_W
gptkb:CF34-10_X
gptkb:CF34-10_Y
gptkb:CF34-10_B
gptkb:CF34-10_C
gptkb:CF34-10_D
gptkb:CF34-10_Z
turbofan
|
gptkbp:first_flight
|
gptkb:1994
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF34-10 series
|
gptkbp:length
|
3.5 m
|
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:operational_range
|
high altitude
|
gptkbp:propulsion
|
up to 10,000 lbf
8.3:1
|
gptkbp:service_entry
|
gptkb:1994
|
gptkbp:turbine_type
|
high bypass ratio
|
gptkbp:weight
|
about 1,200 lb
|
gptkbp:bfsParent
|
gptkb:CF34-10_B
|
gptkbp:bfsLayer
|
7
|