|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:General_Electric
|
|
gptkbp:development
|
gptkb:CF6-50
|
|
gptkbp:diameter
|
68 inches
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:CF6_family
wide-body aircraft
|
|
gptkbp:engine_configuration
|
modular
twin-spool
|
|
gptkbp:engine_power
|
proven track record
optimized for long-haul flights
|
|
gptkbp:engine_type
|
multiple configurations
dual-rotor
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
68 in
11.5 ft
6.5 ft
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric CF6-80 A
|
|
gptkbp:introduced
|
gptkb:1980
|
|
gptkbp:investment
|
high
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market
|
global
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:propulsion
|
6.2
18,500 to 34,000 lbf
18,500 lbf
34,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:General_Electric_GEnx
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
2
|
|
gptkbp:type
|
high bypass turbofan engine
|
|
gptkbp:uses
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:variant
|
gptkb:CF6-80_A1
gptkb:CF6-80_E1
CF6-80 C2
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:Airbus
|
|
gptkbp:bfsLayer
|
4
|