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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Airbus
gptkb:Boeing_737
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:bypass_ratio
|
5.1:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:United_Airlines
|
|
gptkbp:diameter
|
1.5 m
1.9 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:CFM56_family
|
|
gptkbp:engine_configuration
|
pylon-mounted
twin spool
|
|
gptkbp:engine_power
|
up to 30,000 hours
|
|
gptkbp:engine_type
|
gptkb:CFM56-2_C
gptkb:CFM56-2_E
gptkb:CFM56-2_B
turbofan
CFM56-2 D
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 N2
|
|
gptkbp:ignition_system
|
dual spark plug
|
|
gptkbp:legal_principle
|
gptkb:jet_engine
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
4,000 hours
on-condition
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
up to 5,000 nautical miles
|
|
gptkbp:produces
|
over 8,000 units
|
|
gptkbp:propulsion
|
22,000 lbf
clamshell
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
high bypass turbofan
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2_N
|
|
gptkbp:bfsLayer
|
7
|