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gptkbp:instanceOf
|
turbofan engine
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|
gptkbp:application
|
commercial aviation
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|
gptkbp:certifications
|
gptkb:FAA
|
|
gptkbp:compressionRatio
|
5.5:1
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|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
68 in
|
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gptkbp:emissionsStandard
|
low emissions
|
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gptkbp:engine
|
gptkb:CF6-80C2
68 in
advanced technology
4,000 lb
high bypass ratio
wide-body aircraft
156 in
|
|
gptkbp:engineConfiguration
|
dual spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B4
gptkb:CF6-80C2B3
modular design
turbofan
axial
1,600 °F
CF6-80C2B1F2
B1F14
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
gptkbp:hasArea
|
gptkb:EASA
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B1F14
|
|
gptkbp:length
|
156 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
McDonnell Douglas MD-11
|
|
gptkbp:number_of_stages
|
compressor: 10
fan: 3
turbine: 2
|
|
gptkbp:performances
|
high reliability
high efficiency
|
|
gptkbp:propulsion
|
18,500 lbf
4.63
|
|
gptkbp:related_engine
|
gptkb:CF6-80
CF6
|
|
gptkbp:service_ceiling
|
42,000 ft
|
|
gptkbp:updates
|
performance upgrades
|
|
gptkbp:weight
|
4,000 lb
|