|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
1,500 ° C
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
|
gptkbp:engine
|
gptkb:CF6
mass-produced
CF6-80 C2
|
|
gptkbp:engine_configuration
|
modular design
twin-spool
|
|
gptkbp:engine_power
|
high reliability
|
|
gptkbp:engine_type
|
gptkb:CF6-80_C2_B1_F1
gptkb:CF6-6
gptkb:CF6-80_E1
gptkb:CF6-50
gptkb:CF6-80_A
turbofan
CF6-80 C2
CF6-80 C2 B1 F
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
2.5 m
3.5 m
3,000 kg
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-50 C7
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Boeing
gptkb:Mc_Donnell_Douglas_DC-10
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:propulsion
|
50,000 lbf
16.67
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_707
gptkb:Airbus
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:water_requirement
|
2,000 lb/hr
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CF6-50_C
|
|
gptkbp:bfsLayer
|
7
|