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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Boeing_737_Next_Generation
|
|
gptkbp:average_temperature
|
up to 1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.4:1
|
|
gptkbp:certification
|
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:5
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
5.5 ft
61 in
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CFM56_family
CFM56-7 series
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:CFM56-7_B
CFM56-7 B1 variant
|
|
gptkbp:fan_art
|
wide-chord fan blades
|
|
gptkbp:fuel_capacity
|
1.68 m
2.9 m
1,700 kg
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:high-pressure_compressor
|
axial compressor
|
|
gptkbp:high-pressure_turbine
|
single-stage turbine
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-7 B1
|
|
gptkbp:length
|
9.5 ft
|
|
gptkbp:low-pressure_turbine
|
single-stage turbine
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:maximum_continuous_thrust
|
25,000 lbf
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:operational_range
|
up to 40,000 ft
|
|
gptkbp:original_run
|
gptkb:1997
|
|
gptkbp:produces
|
over 8,000 engines
|
|
gptkbp:propulsion
|
27,300 lbf
13.2:1
22,000 to 27,300 lbf
|
|
gptkbp:service_entry
|
gptkb:1998
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
3,800 lb
|
|
gptkbp:bfsParent
|
gptkb:CFM56-7_B_engine
|
|
gptkbp:bfsLayer
|
7
|