|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
CAEP/6
|
|
gptkbp:compressor_type
|
gptkb:10
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:engine
|
gptkb:CF6
gptkb:CF6_series
|
|
gptkbp:engine_configuration
|
pylon-mounted
twin spool
|
|
gptkbp:engine_type
|
gptkb:CF6-50
high bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
2.5 m
3,000 kg
3.8 m
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C3
|
|
gptkbp:launch_window
|
air start
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:maximum_continuous_thrust
|
52,000 lbf
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Boeing
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:number_of_stages_in_low_pressure_compressor
|
gptkb:6
|
|
gptkbp:oil_system_type
|
dry sump
|
|
gptkbp:propulsion
|
50,000 lbf
cascade
|
|
gptkbp:service_entry
|
gptkb:1971
|
|
gptkbp:turbine_type
|
gptkb:4
2
high bypass ratio
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|