|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.1:1
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
68 in
3.0 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CFM56
|
|
gptkbp:engine_configuration
|
twin spool
|
|
gptkbp:engine_type
|
gptkb:CFM56-2
gptkb:CFM56-2_P1
gptkb:CFM56-2_P2
gptkb:CFM56-2_P3
gptkb:CFM56-2_P4
gptkb:CFM56-2_P5
gptkb:CFM56-2_P6
gptkb:CFM56-2_P7
gptkb:CFM56-2_P8
gptkb:CFM56-2_P9
high bypass turbofan
CFM56-2 P10
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
3.5 m
0.76 m
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 P
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
11.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Boeing_737
|
|
gptkbp:number_of_compressor_stages
|
gptkb:5
|
|
gptkbp:number_of_fan_blades
|
gptkb:24
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:number_of_turbine_stages
|
2
|
|
gptkbp:operational_range
|
0 to 1,000 hours
|
|
gptkbp:propulsion
|
7.3:1
22,000 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
high bypass
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2
|
|
gptkbp:bfsLayer
|
6
|