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gptkbp:instanceOf
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turbofan engine
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gptkbp:application
|
commercial aviation
|
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gptkbp:certifications
|
gptkb:FAA
Stage 4
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:compressionRatio
|
4:1
30:1
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gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
68 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:engine
|
gptkb:CF6-80C2B6F14
68 in
60 in
superalloy
single crystal superalloy
158 in
1,000 ft³
|
|
gptkbp:engineConfiguration
|
twin_spool
|
|
gptkbp:engineType
|
axial
high bypass ratio
|
|
gptkbp:fanEvents
|
composite
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B6F14
|
|
gptkbp:length
|
158 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
McDonnell Douglas MD-11
|
|
gptkbp:number_of_stages
|
fan: 3
high pressure compressor: 6
low pressure turbine: 2
high pressure turbine: 2
|
|
gptkbp:propulsion
|
60,000 lbf
cascade
|
|
gptkbp:related_engine
|
gptkb:CF6-80C2
CF6
|
|
gptkbp:weight
|
4,000 lb
|