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gptkbp:instance_of
|
gptkb:turbofan_engine
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|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:bypass_ratio
|
5.1:1
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|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CFM56_family
|
|
gptkbp:engine_configuration
|
gptkb:CFM56-2_C
gptkb:CFM56-2_E
gptkb:CFM56-2_B
gptkb:CFM56-2_F
gptkb:CFM56-2_G
gptkb:CFM56-2_H
gptkb:CFM56-2_J
gptkb:CFM56-2_K
gptkb:CFM56-2_L
gptkb:CFM56-2_M
gptkb:CFM56-2_N
gptkb:CFM56-2_O
gptkb:CFM56-2_P
gptkb:CFM56-2_Q
gptkb:CFM56-2_R
gptkb:CFM56-2_S
gptkb:CFM56-2_T
gptkb:CFM56-2_U
gptkb:CFM56-2_V
gptkb:CFM56-2_W
gptkb:CFM56-2_X
gptkb:CFM56-2_Y
gptkb:CFM56-2_Z
gptkb:CFM56-2_I
twin spool
CFM56-2 D
|
|
gptkbp:engine_type
|
high bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_type
|
Jet A or Jet A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 I
|
|
gptkbp:length
|
3.3 m
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Boeing_737
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
up to 1,000 nautical miles
|
|
gptkbp:propulsion
|
22,000 to 34,000 lbf
18.3:1
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:total_time_between_overhauls
|
20,000 hours
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2_O
gptkb:CFM56-2_S
gptkb:CFM56-2_W
|
|
gptkbp:bfsLayer
|
7
|