gptkbp:instance_of
|
gptkb:turbofan_engine
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gptkbp:application
|
commercial aviation
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gptkbp:average_temperature
|
1,500 ° F
|
gptkbp:bypass_ratio
|
5.5:1
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gptkbp:combustor_type
|
annular
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gptkbp:compressor_type
|
axial
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gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:diameter
|
2.5 m
2.4 m
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
gptkbp:engine
|
gptkb:CF6_family
modular design
Brayton cycle
air start
|
gptkbp:engine_configuration
|
takeoff rating
twin spool
|
gptkbp:engine_type
|
gptkb:CF6-50_C1
gptkb:CF6-50_C10
gptkb:CF6-50_C11
gptkb:CF6-50_C12
gptkb:CF6-50_C13
gptkb:CF6-50_C14
gptkb:CF6-50_C3
gptkb:CF6-50_C5
gptkb:CF6-50_C6
gptkb:CF6-50_C7
gptkb:CF6-50_C8
gptkb:CF6-50
gptkb:CF6-50_C2
high bypass turbofan
CF6-50 C15
CF6-50 C16
CF6-50 C17
CF6-50 C18
CF6-50 C19
CF6-50 C20
CF6-50 C4
CF6-50 C9
|
gptkbp:fan_art
|
wide chord fan
|
gptkbp:first_flight
|
gptkb:1971
|
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 C
|
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:Airbus
gptkb:Mc_Donnell_Douglas_DC-10
|
gptkbp:operational_range
|
long-haul flights
|
gptkbp:propulsion
|
50,000 lbf
16.67:1
|
gptkbp:service_ceiling
|
40,000 ft
|
gptkbp:status
|
in service
|
gptkbp:turbine_type
|
high bypass ratio
|
gptkbp:weight
|
3,000 kg
|
gptkbp:bfsParent
|
gptkb:General_Electric_CF6-50
|
gptkbp:bfsLayer
|
6
|