|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:bypass_ratio
|
5.1:1
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:common_applications
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Boeing_737
gptkb:Mc_Donnell_Douglas_MD-80
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:emissions_compliance
|
ICAO Chapter 4
|
|
gptkbp:engine_configuration
|
available
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
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_I
gptkb:CFM56-2_S1
gptkb:CFM56-2_S10
gptkb:CFM56-2_S2
gptkb:CFM56-2_S3
gptkb:CFM56-2_S4
gptkb:CFM56-2_S5
gptkb:CFM56-2_S6
gptkb:CFM56-2_S7
gptkb:CFM56-2_S8
gptkb:CFM56-2_S9
turbofan
CFM56-2 D
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 S
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
available
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:minimum_thrust
|
5,000 lbf
|
|
gptkbp:number_of_engines
|
over 8,000
|
|
gptkbp:number_of_stages
|
10 stages
|
|
gptkbp:propulsion
|
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1982
|
|
gptkbp:turbine_type
|
high bypass turbine
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2
|
|
gptkbp:bfsLayer
|
6
|