|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
1,200 lb/sec
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:bypass_ratio
|
5.5:1
|
|
gptkbp:certification
|
FAA certified
Stage 3
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:9
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
3.0 ft
60 in
|
|
gptkbp:engine
|
gptkb:CF6
gptkb:CF6_series
upgradable components
|
|
gptkbp:engine_configuration
|
modular design
twin-spool
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
gptkb:CF6-50
gptkb:CF6-50_C2
gptkb:CF6-50_A
gptkb:CF6-50_B
gptkb:CF6-50_E
high bypass turbofan
|
|
gptkbp:first_flight
|
gptkb:1971
|
|
gptkbp:fuel_capacity
|
3.8 m
1,360 kg
0.76 m
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C2
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
12.5 ft
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_users
|
gptkb:Airbus
gptkb:Boeing
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:propulsion
|
50,000 lbf
16.5:1
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:water_requirement
|
1,000 lb/hr
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Boeing_E-4_B
|
|
gptkbp:bfsLayer
|
6
|